1997L0068 — EN — 11.02.2003 — 002.001 — 1
This document is meant purely as a documentation tool and the institutions do not assume any liability for its contents
►B DIRECTIVE97/68/ECOFTHEEUROPEANPARLIAMENTANDOFTHECOUNCIL
of16December 1997
ontheapproximationofthelawsoftheMemberStatesrelatingtomeasuresagainsttheemission
ofgaseousandparticulatepollutantsfrominternalcombustionenginestobeinstalledinnon-road
mobilemachinery
(OJ L 59, 27.2.1998, p. 1)
Amended by:
Official Journal
No page date
►M1Commission Directive 2001/63/EC of 17 August 2001 L 227 41 23.8.2001
►M2Directive 2002/88/EC of the European Parliament and of the Council of
9 December 2002L 35 28 11.2.2003
▼B
DIRECTIVE 97/68/EC OF THE EUROPEAN PARLIAMENT
ANDOFTHECOUNCIL
of16December 1997
on the approximationof the lawsofthe Member States relating to
measuresagainsttheemissionofgaseousandparticulatepollutantsfrom internal combustion engines to be installed in non-road
mobilemachinery
THE EUROPEAN PARLIAMENT AND THE COUNCIL OF THE
EUROPEAN UNION,
Having regard to the Treaty establishing the European Community, and
in particular Article 100a thereof,
Having regard to the proposal from the Commission (1),
Having regard to the opinion of the Economic and Social
Committee (2),
Acting in accordance with the procedure laid down in Article 189b of
the Treaty (3), in the light of the joint text approved by the Conciliation
Committee on 11 November 1997,
(1)Whereasthe Community programme of policy and action inrelation to the environment and sustainable development (
4)
recognizes as a fundamental principle that all persons should be
effectively protected against recognized health risks from airpollution and that this necessitates in particular the control ofemissions of nitrogen dioxide (NO
2), particulates(PT) — black
smoke, and other pollutants such as carbon monoxide (CO);whereaswith regard to the prevention of tropos pheric ozone
(O
3) formation and its associated health and environmental
impact, the emissions of the precursors nitrogenoxides (NOx)
and hydrocarbons(HC) mus t be reduced; whereasthe environ-mental damage caused by acidification will also requirereductions inter alia on the emission of NO
xand HC;
(2)Whereasthe Community s igned the UN/ECE protocol on vola-
tile organic compound (VOC) reduction in April 1992 andadhered to the protocol on NO
xreduction in December 1993,
both of which are related to the 1979 Convention on Long-range
Transboundary Air Pollution which was approved in July 1982;
(3)Whereasthe objective of reducing the level of pollutant emis -
sions from non-road mobile machinery engines and theestablishment and operation of the internal market for engines
and machinery cannot be sufficiently achieved by individual
Member States, and can therefore be better achieved by theapproximation of the lawsof the Member Statesrelating tomeasures against air pollution by engines to be installed in non-road mobile machinery;
(4)Whereas recent investigations undertaken by the Commissionshow that the emissions from non-road mobile machineryengines constitute a significant proportion of the total man-made emissions of certain noxious atmospheric pollutants;whereas the category of compression ignition engines which
will be regulated by this Directive is responsible for a consider-
able share of air pollution by NO
xand PT, in particular when it
is compared with that coming from the road transport sector;1997L0068 — EN — 11.02.2003 — 002.001 — 2
(1) OJ C 328, 7.12.1995, p. 1.
(2) OJ C 153, 28.3.1996, p. 2.
(3) Opinion of the European Parliament of 25 October 1995 (OJ C 308,
20.11.1995, p. 29), Council common position of 20 January 1997 (OJ C
123, 21.4.1997, p. 1) and Decision of the European Parliament of 13 May1997, (OJ C 167, 2.7.1997, p. 22). Council Decision of 4 December 1997
and Decision of the European Parliament of 16 December 1997.
(
4) Resolution of the Council and the representatives of the Governments of the
Member States, meeting within the Council of 1 February 1993 (OJ C 138,
17.5.1993, p. 1).
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(5)Whereas emissions from non-road mobile machinery operating
on the ground equipped with compression ignition engines, and
in particular the emissions of NOxand PT, constitute a primary
cause of concern in this area; whereas these sources should beregulated in the first instance; whereas, however, it will also beappropriate subsequently to extend the scope of this Directive toinclude the control of emissions from other non-road mobile
machinery engines, including transportable generating sets, based
on appropriate test cycles, and in particular from gasolineengines; whereas a considerable reduction of the CO and HCemissions may be achievable with the envisaged enlargement ofthe scope of this Directive to include gasoline engines;
(6)Whereas emissions control legislation on agricultural andforestry tractor engines, ensuring a level of environmentalprotection equivalent to the level established pursuant to this
Directive, with standards and requirements fully consistent with
it, should be introduced as soon as possible;
(7)Whereas, in respect of certification procedures, that type-
approval approach hasbeen taken which, asa European method,
has stood the test of time for approvals of road vehicles and theircomponents; whereas, as a new element, the approval of a parentengine on behalf of a group of engines(engine family) builtusing similar components according to similar construction prin-
ciples, has been introduced;
(8)Whereasthe enginesproduced in compliance with the require-
mentsof thisDirective will have to be accordingly marked and
notified to the approval authorities; whereas, in order to keep
administrative burdens low, no direct control by the authority ofthe engine production datesrelevant for s trengthened require-mentshasbeen fores een; whereasthisfreedom for themanufacturersrequiresthem to facilitate the preparation of s potchecksby the authority and to make available relevant produc-
tion planning information at regular intervals; whereas absolute
compliance with notification made in accordance with thisprocedure isnot obligatory but a high degree of compliancewould facilitate the approval authorities' planning of assessmentsand contribute to a relationship of increased trust between manu-
facturersand type-approval authorities ;
(9)Whereasapprovalsgranted in accordance with Directive 88/77/
EEC (1) and with UN/ECE Regulation 49 Series02, aslis ted in
Annex IV, Appendix II to Directive 92/53/EEC (2) are recog-
nized asequivalent to thos e required by thisDirective in itsfirst stage;
(10)Whereasengineswhich are in compliance with the requirementsof this Directive and covered by its scope must be permitted tobe placed on the market in the Member States; whereas theseengines must not be subject to any other national emissionrequirement; whereasthe Member State granting approvalswill
take the necessary control measures;
(11)Whereas, in laying down the new test procedures and limit
values, it is necessary to take into account the specific usage
patterns of these types of engines;
(12)Whereas it is appropriate to introduce these new standards
according to the proven principle of a two-stage approach;1997L0068 — EN — 11.02.2003 — 002.001 — 3
(1) Council Directive 88/77/EEC of 3 December 1987 on the approximation of
the laws of the Member States relating to the measures to be taken against
the emission of gaseous pollutants from diesel engines for use in vehicles
(OJ L 36, 9.2.1988, p. 33). Directive aslas t amended by Directive 96/1/EC(OJ L 40, 17.2.1996, p. 1).
(
2) Council Directive 92/53/EEC of 18 June 1992 amending Directive 70/156/
EEC on the approximation of the lawsof the Member Statesrelating to the
type-approval of motor vehiclesand their trailers(OJ L 225, 10.8.1992, p.
1).
▼B
(13)Whereas, for engines with higher power output, the achievement
of substantial emission reduction seems to be easier, as existing
technology that hasbeen developed for enginesof road vehiclescan be used; whereas, taking this into account a staggered imple-mentation of the requirementshasbeen fores een, beginning withthe highest of three powerbands for stage I; whereas this prin-ciple hasbeen retained for s tage II with the exception of a new
fourth powerband not covered by stage I;
(14)Whereasfor thiss ector of non-road mobile machinery applica-
tions , which isnow regulated and isthe mos t important one
besides agricultural tractors if compared with emissions coming
from road transport, a considerable reduction of emissions canbe expected by the implementation of thisDirective; whereasdue to, in general, very good performance of diesel engineswith respect to CO and HC emissions, the margin for improve-
ment in respect of the total amount emitted is very small;
(15)Whereas, in order to make provision for the case of exceptional
technical or economic circumstances, procedures have been inte-
grated which could exempt manufacturersfrom the obligations
arising from this Directive;
(16)Whereas, in order to ensure ‘conformity of production’ (COP)
once an approval isgranted for an engine, manufacturerswill
be required to provide corresponding arrangements; whereasprovisions have been made for the case of discovered non-conformity which lay down information procedures, correctiveactionsand a cooperation procedure which will allow the s ettlingof possible differences of opinion between Member States in
respect of conformity of certified engines;
(17)Whereasthe entitlement of Member Statesto lay down require-ments ensuring that workers are protected when using non-road
mobile machinery shall not be affected by this Directive;
(18)Whereasthe technical provis ionsin certain Annexesto this
Directive should be supplemented and, as necessary, adapted to
technical progress according to a committee procedure;
(19)Whereas provisions should be laid down to ensure testing of the
enginesin compliance with the rulesof good laboratory practice;
(20)Whereasthere isa need to promote global trade in thiss ector by
harmonizing, as far as possible, emission standards in the
Community with those applied or planned in third countries;
(21)Whereas it is therefore necessary to envisage the possibility of
reconsidering the situation on the basis of the availability and
the economic feasibility of new technologies and taking account
of progress achieved in the implementation of the second stage;
(22)Whereasan agreement on a modusvivendi between the
European Parliament, the Council and the Commission
concerning the implementing measures for acts adopted in accor-dance with the procedure laid down in Article 189b of the Treatywasreached on 20 December 1994 (
1),
HAVE ADOPTED THIS DIRECTIVE:
Article 1
Objectives
ThisDirective aimsat approximating the lawsof the Member States
relating to emission standards and type-approval procedures for enginesto be installed in non-road mobile machinery. It will contribute to thesmooth functioning of the internal market, while protecting humanhealth and the environment.1997L0068 — EN — 11.02.2003 — 002.001 — 4
(1) OJ C 102, 4.4.1996, p. 1.
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Article 2
Definitions
For the purposes of this Directive:
—non-road mobile machinery shall mean any mobile machine, trans-
portable industrial equipment or vehicle with or without body work,not intended for the use of passenger- or goods-transport on theroad, in which an internal combustion engine as specified in AnnexI section 1 is installed,
—type-approval shall mean the procedure whereby a Member State
certifiesthat an internal combus tion engine type or engine familywith regard to the level of emission of gaseous and particulatepollutants by the engine(s), satisfies the relevant technical require-
mentsof thisDirective,
—engine type shall mean a category of engines which do not differ in
such essential engine characteristics as specified in Annex II,Appendix 1,
—engine family shall mean a manufacturer's grouping of engines
which, through their design, are expected to have similar exhaustemission characteristics and which comply with the requirementsof thisDirective,
—parent engine shall mean an engine selected from an engine family
in such a way that it complies with the requirements set out insections 6 and 7 of Annex I,
—engine power output shall mean net power as specified in section
2.4 of Annex I,
—engine production date shall mean the date when the engine passes
the final check after it hasleft the production line. At thiss tage the
engine isready to be delivered or to be put on s tock,
—placing on the market shall mean the action of making an engine
available for the first time on the market, for payment or free ofcharge, with a view to distribution and/or use in the Community,
—manufacturer shall mean the person or body who is responsible to
the approval authority for all aspects of the type-approval processand for ensuring conformity of production. It is not essential thatthe person or body is directly involved in all stages of the construc-tion of the engine,
—approval authority shall mean a Member State's competent
authority or authorities responsible for all aspects of type-approvalof an engine or of an engine family, for issuing and withdrawingapproval certificates, for serving as the contact point with the
approval authoritiesof the other Member States , and for verifying
the manufacturer'sconformity of production arrangements ,
—technical service shall mean the organization(s) or body(ies) that
has(have) been appointed as a testing laboratory to carry out tests
or inspections on behalf of the approval authority of a Member
State. Thisfunction may als o be carried out by the approvalauthority itself,
—information document shall mean the document set out in Annex II
that prescribes the information to be supplied by an applicant,
—information folder shall mean the total folder or file of data, draw-
ings, photographs, etc. supplied by the applicant to the technicalservice or the approval authority as prescribed in the information
document,
—information package shall mean the information folder plus any test
reportsor other documentsthat the technical s ervice or the approvalauthority have added to the information folder in the course of
carrying out their functions,
—index to the information package shall mean the document in which
the contentsof the information package, s uitably numbered orotherwise marked to clearly identify all pages, are listed,1997L0068 — EN — 11.02.2003 — 002.001 — 5
▼M2
▼B
▼M2
—replacement engines shall mean a newly built engine to replace an
engine in a machine, and which has been supplied for this purposeonly,
—hand-held engine shall mean an engine that meets at least one of
the following requirements:
(a) the engine must be used in a piece of equipment that is carried
by the operator throughout the performance of itsintendedfunction(s);
(b) the engine must be used in a piece of equipment that must
operate multipositionally, such as upside down or sideways, tocomplete itsintended function(s );
(c) the engine must be used in a piece of equipment for which the
combined engine and equipment dry weight isunder 20 kilo-
grams and at least one of the following attributes is alsopresent:
(i) the operator must alternatively provide support or carry the
equipment throughout the performance of itsintended
function(s);
(ii) the operator must provide support or attitudinal control for
the equipment throughout the performance of itsintendedfunction(s);
(iii) the engine must be used in a generator or a pump,
—non-hand-held engine shall mean an engine which does not fall
under the definition of a hand-held engine,
—professional use multipositional hand-held engine shall mean a
hand-held engine which meetsthe requirementsof both (a) and (b)of the hand-held engine definition and in relation to which the
engine manufacturer has satisfied an approval authority that a Cate-
gory 3 Emissions Durability Period (according to section 2.1 ofAppendix 4 to Annex IV) would be applicable to the engine,
—emission durability period shall mean the number of hours indicated
in Annex IV, Appendix 4, used to determine the deteriorationfactors,
—small volume engine family shall mean a spark-ignition (SI) engine
family with a total yearly production of fewer than 5 000 units,
—small volume engine manufacturer of SIengines shall mean a
manufacturer with a total yearly production of fewer than 25 000units.
Article 3
Applicationfortype-approval
1. Application for engine or engine family type-approval shall be
submitted by the manufacturer to the approval authority of a MemberState. An application shall be accompanied by an information folder,the contentsof which are given in the information document in AnnexII. An engine conforming to the engine type characteristics described inAnnex II, Appendix 1, shall be submitted to the technical service
responsible for conducting the approval tests.
2. In the case of an application for type-approval of an engine
family, if the approval authority determinesthat, with regard to theselected parent engine, the submitted application does not fully repre-sent the engine family described in Annex II, Appendix 2, analternative and, if necessary, an additional parent engine which is deter-
mined by the approval authority shall be provided for approval
according to paragraph 1.
3. No application in respect of one engine type or engine family
may be submitted to more than one Member State. A separate applica-tion shall be submitted for each engine type or engine family to beapproved.1997L0068 — EN — 11.02.2003 — 002.001 — 6
▼B
▼B
Article 4
Type-approvalprocedure
1. The Member State receiving the application shall grant type-
approval to all engine typesor engine familieswhich conform to the
particularsin the information folder and which meet the requirementsof thisDirective.
2. The Member State shall complete all applicable sections of the
type-approval certificate, the model being given in ►
M2Annex
VII◄, for each engine type or engine family which it approvesand
shall compile or verify the contents of the index to the informationpackage. Type-approval certificatess hall be numbered in accordance
with the method described in ►
M2Annex VIII ◄. The completed
type-approval certificate and itsattachmentss hall be delivered to theapplicant.
3. Where the engine to be approved fulfilsitsfunction or offersa
specific feature only in conjunction with other parts of the non-roadmobile machinery, and for thisreas on compliance with one or morerequirementscan be verified only when the engine to be approvedoperatesin conjunction with other machinery parts , whether real or
simulated, the scope of the type-approval of the engine(s) must be
restricted accordingly. The type-approval certificate for an engine typeor engine family shall then include any restrictions on its use and shallindicate any conditionsfor fitting it.
4. The approval authority of each Member State shall:
(a) send monthly to the approval authorities of the other Member
States a list (containing the particulars shown in ►
M2Annex
IX◄) of the engine and engine family type-approvalsit has
granted, refused to grant or withdrawn during that month;
(b) on receiving a request from the approval authority of another
Member State, send forthwith:
— a copy of the engine or engine family type-approval certificate
with/without information package for each engine type or
engine family which it hasapproved or refus ed to approve or
withdrawn, and/or
— the list of engines produced according to type-approvals
granted, asdes cribed in Article 6(3), containing the particulars
shown in ►M2Annex X ◄, and/or
— a copy of the declaration described in Article 6(4).
5. The approval authority of each Member State shall yearly, or in
addition on receiving a corresponding application, send the Commis-sion a copy of the data sheet as shown in ►
M2Annex XI ◄related
to the engines approved since the last notification was made.
Article 5
Amendmentstoapprovals
1. The Member State which hasgranted type-approval mus t take the
necessary measures to ensure that it is informed of any change in the
particularsappearing in the information package.
2. The application for the amendment or extension of a type-
approval shall be submitted exclusively to the approval authority of
the Member State which granted the original type-approval.
3. If particularsappearing in the information package have changed,
the approval authority of the Member State in question shall:
— issue revised page(s) of the information package as necessary,
marking each revised page to show clearly the nature of the changeand the date of re-issue. Wherever revised pages are issued theindex to the information package (which isattached to the type-approval certificate) shall also be amended to show the latest datesof revised pages, and1997L0068 — EN — 11.02.2003 — 002.001 — 7
▼B
— issue a revised type-approval certificate (denoted by an extension
number) if any information on it (excluding itsattachments ) haschanged or if the standards of this Directive have changed since
the date currently on the approval. The revised certificate shall
show clearly the reason for revision and the date of re-issue.
If the approval authority of the Member State in question finds that an
amendment to an information package warrants fresh tests or checks, it
shall inform the manufacturer thereof and issue the documents
mentioned above only after the conduct of successful fresh tests orchecks.
Article 6
Conformity
1. The manufacturer shall affix to each unit manufactured in confor-
mity with the approved type the markingsasdefined in s ection 3 ofAnnex I, including the type-approval number.
2. Where the type-approval certificate, in accordance with Article
4(3), includes restrictions on use, the manufacturer shall deliver with
each unit manufactured, detailed information on these restrictions and
shall indicate any conditions for fitting it. Where a series of enginetypes is delivered to one single manufacturer of machinery, it is suffi-cient that he will be provided with only one such informationdocument, at the latest on the delivery date of the first engine, which
additionally lists the relevant engine identification numbers.
3. The manufacturer shall send on demand to the approval authority
which granted the type-approval, within 45 daysafter the end of eachcalendar year, and without delay after each application date when therequirementsof thisDirective change, and immediately following
each additional date the authority may stipulate, a list which contains
the range of identification numbersfor each engine type produced inaccordance with the requirements of this Directive since the lastreporting wasmade, or s ince the requirementsof thisDirective werefirst applicable. Where not clarified by the engine coding system, thislist must specify correlations of the identification numbers to the corre-
sponding engine types or engine families and to the type-approval
numbers. Additionally, this list must contain particular information ifthe manufacturer ceases to produce an approved engine type or enginefamily. Where this list is not required to be regularly sent to theapproval authority, the manufacturer must maintain these records for a
minimum period of 20 years.
4. The manufacturer shall send to the approval authority which
granted the type-approval, within 45 daysafter the end of eachcalendar year and at each application date referred to in Article 9, adeclaration specifying the engine types and engine families together
with the relevant engine identification codesfor thos e engineshe
intendsto produce from thisdate on.
Article 7
Acceptanceofequivalentapprovals
1. The European Parliament and the Council, acting on a proposal
from the Commission, may acknowledge the equivalence between the
conditions and provisions for type-approval of engines established bythis Directive and the procedures established by international regula-tionsor regulationsof third countries , in the framework of multilateralor bilateral agreementsbetween the Community and third countries .
2. Member Statess hall accept type-approvalsand, where applicable,
the pertaining approval markslis ted in Annex XII asbeing in confor-mity with thisDirective.1997L0068 — EN — 11.02.2003 — 002.001 — 8
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Article 8
Registrationandplacingonthemarket
1. Member States may not refuse registration, where applicable, or
placing on the market of new engines, whether or not already installedin machinery, which meet the requirementsof thisDirective.
2. Member States shall only permit registration, where applicable, or
placing on the market of new engines, whether or not already installedin machinery, which meet the requirementsof thisDirective.
3. The approval authority of a Member State granting a type-
approval shall take the necessary measures in relation to that approval
to register and control, if need be in cooperation with the approvalauthoritiesof the other Member States , the identification numbersofthose engines produced in conformity with the requirements of thisDirective.
4. An additional control of the identification numbersmay take
place in conjunction with the control of conformity of production asdescribed in Article 11.
5. With regard to the control of the identification numbers, the
manufacturer or his agents established in the Community shall withoutdelay give, on request, to the responsible approval authority all theinformation needed related to his/their purchasers together with theidentification numbersof the enginesreported asproduced in accor-dance with Article 6(3). Where enginesare s old to a manufacturer of
machinery, further information isnot required.
6. If, at the request of the approval authority, the manufacturer is not
able to verify the requirementsass pecified in Article 6 particularly inconjunction with paragraph 5 of thisArticle, the approval granted in
respect of the corresponding engine type or family pursuant to this
Directive may be withdrawn. The information procedure shall then becarried out asdes cribed in Article 12(4).
Article 9
Timetable-compression ignitionengines
1. GRANT OF TYPE-APPROVALS
After 30 June 1998, Member Statesmay not refus e to grant type-
approval for an engine type or engine family or to issue the document
asdes cribed in ►
M2Annex VII ◄, and may not impose any other
type-approval requirements with regard to air-polluting emissions fornon-road mobile machinery in which an engine isins talled, if theengine meetsthe requirementss pecified in thisDirective asregards
the emissions of gaseous and particulate pollutants.
2. TYPE-APPROVALS STAGE I
(ENGINE CATEGORIES A/B/C)
Member States shall refuse to grant type-approval for an engine type or
engine family and to issue the document as described in ►
M2Annex
VII◄, and shall refuse to grant any other type-approval for non-road
mobile machinery in which an engine isins talled:
after 30 June 1998 for enginesof a power output:
— A: 130 kW ≤P≤560 kW,
—B : 7 5k W ≤P < 130 kW,
—C : 3 7k W ≤P < 75 kW,
if the engine failsto meet the requirementss pecified in thisDirective
and where the emissions of gaseous and particulate pollutants from theengine do not comply with the limit valuesass et out in the table in►
M2section 4.1.2.1 of Annex I ◄.1997L0068 — EN — 11.02.2003 — 002.001 — 9
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▼B
▼B
3. TYPE-APPROVALS STAGE II
(ENGINE CATEGORIES: D, E, F, G)
Member States shall refuse to grant type-approval for an engine type or
engine family and to issue the document as described in ►M2Annex
VII◄, and shall refuse to grant any other type-approval for non-road
mobile machinery in which an engine isins talled:
— D: after 31 December 1999 for enginesof a power output: 18
kW≤P < 37 kW,
— E: after 31 December 2000 for enginesof a power output: 130
kW≤P≤560 kW,
— F: after 31 December 2001 for enginesof a power output: 75
kW≤P < 130 kW,
— G: after 31 December 2002 for enginesof a power output: 37
kW≤P < 75 kW,
if the engine failsto meet the requirementss pecified in thisDirective
and where the emissions of gaseous and particulate pollutants from the
engine do not comply with the limit valuesass et out in the table in►
M2section 4.1.2.3 of Annex I ◄.
4. REGISTRATION AND PLACING ON THE MARKET: ENGINE
PRODUCTION DATES
After the datesreferred to hereafter, with the exception of machineryand engines intended for export to third countries, Member States shallpermit the registration, where applicable, and ►
M2placing on the
market of engines ◄, whether or not already installed in machinery,
only if they meet the requirementsof thisDirective, and only if the
engine isapproved in compliance with one of the categoriesasdefinedin paragraphs2 and 3.
Stage I
— category A: 31 December 1998
— category B: 31 December 1998— category C: 31 March 1999
Stage II
— category D: 31 December 2000
— category E: 31 December 2001
— category F: 31 December 2002
— category G: 31 December 2003
Nevertheless, for each category, Member States may postpone each
date mentioned in the above requirement for two yearsin res pect ofengineswith a production date prior to the s aid date.
The permission granted for stage I-engines shall be terminated with
effect from the mandatory implementation of stage II.
Article 9a
Timetable—Sparkignitionengines
1. DIVIDING INTO CLASSES
For the purpose of this Directive, spark-ignition engines shall be
divided into the following classes.
Main class S: small engines with a net power ≤19 kW
The main class S shall be divided into two categories:H: enginesfor hand-held machinery
N: enginesfor non-hand-held machinery1997L0068 — EN — 11.02.2003 — 002.001 — 10
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Class/category Displacement (cubic cm)
Hand-held engines
Class SH:1 < 20
Class SH:2 ≥20
<5 0
Class SH:3 ≥50
Non-hand-held engines
Class SN:1 < 66
Class SN:2 ≥66
< 100
Class SN:3 ≥100
< 225
Class SN:4 ≥225
2. GRANT OF TYPE APPROVALS
After 11 August 2004, Member States may not refuse to grant type-
approval for an SI engine type or engine family or to issue the docu-ment as described in Annex VII, and may not impose any other type-
approval requirements with regard to air-polluting emissions for non-
road mobile machinery in which an engine isins talled, if the enginemeets the requirements specified in this Directive as regards the emis-sions of gaseous pollutants.
3. TYPE-APPROVALS STAGE 1
Member States shall refuse to grant type-approval for an engine type or
engine family and to issue the documents as described in Annex VII,and shall refuse to grant any other type-approval for non-road mobilemachinery in which an engine is installed after 11 August 2004 if theengine failsto meet the requirementss pecified in thisDirective and
where the emissions of gaseous pollutants from the engine do not
comply with the limit values as set out in the table in section 4.2.2.1of Annex I.
4. TYPE-APPROVALS STAGE II
Member States shall refuse to grant type-approval for an engine type or
engine family and to issue the documents as described in Annex VII,and shall refuse to grant any other type-approval for non-road mobilemachinery in which an engine isins talled:
after 1 August 2004 for engine classes SN:1 and SN:2
after 1 August 2006 for engine class SN:4after 1 August 2007 for engine classes SH:1, SH:2 and SN:3
after 1 August 2008 for engine class SH:3,
if the engine failsto meet the requirementss pecified in thisDirective
and where the emissions of gaseous pollutants from the engine do notcomply with the limit values as set out in the table in section 4.2.2.2 ofAnnex I.
5. PLACING ON THE MARKET: ENGINE PRODUCTION DATES
Six monthsafter the datesfor the relevant category of engine in para-
graphs3 and 4, with the exception of machinery and enginesintendedfor export to third countries, Member States shall permit placing on themarket of engines, whether or not already installed in machinery, onlyif they meet the requirementsof thisDirective.1997L0068 — EN — 11.02.2003 — 002.001 — 11
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6. LABELLING OF EARLY COMPLIANCE WITH STAGE II
For engine typesor engine familiesmeeting the limit valuess et out in
the table in section 4.2.2.2 of Annex I, before the dates laid down inpoint 4 of this Article, Member States shall allow special labelling
and marking to show that the equipment concerned meets the required
limit valuesbefore the dateslaid down.
7. EXEMPTIONSThe following machinery shall be exempted from the implementation
dates of stage II emission limit requirements for a period of three yearsafter the entry into force of those emission limit requirements. Forthose three years, the stage I emission limit requirements shall continueto apply:
— hand-held chainsaw: a hand-held device designed to cut wood with
a saw chain, designed to be supported with two hands and having
an engine capacity in excess of 45 cm
3, according to EN ISO
11681-1,
— top handle machine (i.e., hand-held drillsand tree s ervice chain-
saws): a hand-held device with the handle on top of the machine
designed to drill holes or to cut wood with a saw chain (accordingto ISO 11681-2),
— hand-held brush cutter with an internal combustion engine: a hand-
held device with a rotating blade made of metal or plastic intended
to cut weeds, brush, small trees and similar vegetation. It must be
designed according to EN ISO 11806 to operate multi-positionally,such as horizontally or upside down, and have an engine capacityin excess of 40 cm
3;
— hand-held hedge trimmer: a hand-held device designed for trim-
ming hedgesand bus hesby meansof one or more reciprocatingcutter blades, according to EN 774,
— hand-held power cutter with an internal combustion engine: a
hand-held device intended for cutting hard materials such as stone,
asphalt, concrete or steel by means of a rotating metal blade with a
displacement in excess of 50 cm
3, according to EN 1454, and
— non-hand-held, horizontal shaft class SN:3 engine: only those class
SN:3 non-hand-held engineswith a horizontal s haft that producepower equal to or less than 2,5 kW and are used mainly for select,
industrial purposes, including tillers, reel cutters, lawn aerators and
generators.
8. OPTIONAL IMPLEMENTATION DELAYNevertheless, for each category, Member States may postpone the dates
in paragraphs3, 4 and 5 for two yearsin res pect of engineswith aproduction date prior to those dates.
Article 10
Exemptionsandalternativeprocedures
1. The requirementsof Article 8(1) and (2), Article 9(4) and Article
9a (5) shall not apply to:
— engines for use by the armed services,
— enginesexempted in accordance with paragraphs1a and 2.
1a. A replacement engine shall comply with the limit values that the
engine to be replaced had to meet when originally placed on the
market. The text ‘REPLACEMENT ENGINE’ shall be attached to alabel on the engine or inserted into the owner's manual.
2. Each Member State may, at the request of the manufacturer,
exempt end-of-series engines which are still in stock, or stocks ofnon-road mobile machinery in respect of their engines, from the time1997L0068 — EN — 11.02.2003 — 002.001 — 12
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limit(s) for placing on the market set out in Article 9(4) in accordance
with the following conditions:
— the manufacturer must submit an application to the approval autho-
ritiesof that Member State which approved the corres pondingengine type(s) or engine family(ies) before the entry into force ofthe time limit(s),
— the application of the manufacturer must include a list as defined in
Article 6(3) of those new engines which are not placed on themarket within the time limit(s); in the case of engines covered bythis Directive for the first time, he must submit his application to
the type-approval authority of that Member State where the engines
are stored,
— the request must specify the technical and/or economic reasons on
which it isbas ed,
— the enginesmus t conform to a type or family for which the type-
approval isno longer valid, or which did not need a type-approval
before, but which have been produced according to the timelimit(s),
— the engines must have been physically stored within the Commu-
nity within the time limit(s),
— the maximum number of new enginesof one or more typesplaced
on the market in each Member State by the application of thisexemption must not exceed 10 % of the new engines of all typesconcerned placed on the market in that Member State during thepreviousyear,
— if the request is accepted by the Member State, the latter must,
within one month, send the approval authorities of the otherMember Statesparticularsof, and reas onsfor, the exemptions
granted to the manufacturer,
— the Member State granting exemptionsaccording to thisArticle
shall be responsible for ensuring that the manufacturer complies
with all corresponding obligations,
— the approval authority shall release for each engine in question a
certificate of conformity on which a special entry has been made.If applicable a consolidated document that contains all engine iden-tification numbers in question may be used,
— Member States shall each year send the Commission a list of
exemptions granted specifying the reasons.
Thisoption s hall be limited to a period of 12 monthsasfrom the date
on which the engines for the first time were subject to the time limit(s)for placing on the market.
3. The requirements of Article 9a(4) and (5) shall be postponed by
three years for small volume engine manufacturers.
4. The requirementsof Article 9a(4) and (5) s hall be replaced by the
corresponding stage I requirements for a small volume engine family toa maximum of 25 000 unitsproviding that the variousengine familiesinvolved all have different cylinder displacements.
Article 11
Conformityofproductionarrangements
1. The Member State granting a type-approval shall take the neces-
sary measures to verify, with regard to the specifications laid down insection 5 of Annex I, if need be in cooperation with the approvalauthoritiesof the other Member States , that adequate arrangements
have been made to ensure effective control of the conformity of
production before it grantstype-approval.
2. The Member State which hasgranted a type-approval s hall take
the necessary measures to verify, with regard to the specifications laiddown in section 5 of Annex I, if need be in cooperation with theapproval authoritiesof the other Member States , that the arrangementsreferred to in paragraph 1 continue to be adequate and that each1997L0068 — EN — 11.02.2003 — 002.001 — 13
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production engine bearing a type-approval number pursuant to this
Directive continuesto conform to the des cription asgiven in theapproval certificate and itsAnnexesfor the approved engine type or
family.
Article 12
Non-conformitywiththeapprovedtypeorfamily
1. There shall be failure to conform to the approved type or family
where deviationsfrom the particularsin the type-approval certificateand/or the information package are found to exist and where these
deviationshave not been authorized, purs uant to Article 5(3), by the
Member State which granted the type-approval.
2. If a Member State which hasgranted type-approval findsthat
enginesaccompanied by a certificate of conformity or bearing anapproval mark do not conform to the type or family it hasapproved,it shall take the necessary measures to ensure that the engines inproduction again conform to the approved type or family. The approval
authorities of that Member State shall advise those of the other
Member States of the measures taken which may, where necessary,extend to withdrawal of type-approval.
3. If a Member State demonstrates that engines bearing a type-
approval number do not conform to the approved type or family itmay request the Member State which granted the type-approval toverify that enginesin production conform to the approved type or
family. Such action shall be taken within six months of the date of
the request.
4. The approval authoritiesof the Member Statess hall inform each
other within one month of any withdrawal of type-approval and of thereasons for such measure.
5. If the Member State which granted type-approval disputes the
failure to conform notified to it, the Member Statesconcerned s hallendeavour to settle the dispute. The Commission shall be keptinformed and shall, where necessary, hold appropriate consultations
for the purpose of reaching a settlement.
Article 13
Workerprotectionrequirements
The provisions of this Directive shall not affect Member States' entitle-
ment to lay down, in due observance of the Treaty, such requirementsas they may deem necessary to ensure that workers are protected when
using the machinery referred to in this Directive, provided that this
doesnot affect the placing on the market of the enginesin ques tion.
Article 14
Adaptationtotechnical progress
Any amendments which are necessary in order to adapt the Annexes to
thisDirective, with the exception of the requirementss pecified in
section 1, sections 2.1 to 2.8 and section 4 of Annex I, to take account
of technical progress shall be adopted by the Commission in accor-dance with the procedure referred to in Article 15(2).
Article 14a
Procedure forderogations
The Commission shall study possible technical difficulties in
complying with the stage II requirements for certain uses of the
engines, in particular mobile machinery in which engines of classesSH:2 and SH:3 are installed. If the Commission studies conclude thatfor technical reasons certain mobile machinery, in particular, profes-sional use, multi-positional, hand-held engines, cannot meet thesedeadlines, it shall submit, by 31 December 2003, a report accompanied1997L0068 — EN — 11.02.2003 — 002.001 — 14
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by appropriate proposals for extensions of the period referred to in
Article 9a(7) and/or further derogations, not exceeding five years,unless in exceptional circumstances, for such machinery, under the
procedure laid down in Article 15(2).
Article 15
Committee
1. The Commission shall be assisted by the Committee on Adapta-
tion to Technical Progress of the Directives on the Removal of
Technical Barriersto Trade in the Motor Vehicle Sector (hereinafterreferred to as‘the Committee’).
2. Where reference ismade to thisparagraph, Articles5 and 7 of
Decision 1999/468/EC (
1) shall apply, having regard to the provisions
of Article 8 thereof.
The period laid down in Article 5(6) of Decision 1999/468/EC shall be
set at three months.
3. The Committee shall adopt its Rules of Procedure.
Article 16
Approvalauthoritiesandtechnical services
The Member States shall notify to the Commission and to the other
Member States the names and addresses of the approval authorities
and technical services that are responsible for the purposes of this
Directive. The notified services must satisfy the requirements as laiddown in Article 14 of Directive 92/53/EEC.
Article 17
Transposalintonationallaw
1. Member States shall bring into force the laws, regulations and
administrative provisions necessary to comply with this Directive notlater than 30 June 1998. They shall forthwith inform the Commissionthereof.
When Member States adopt these measures, they shall contain a refer-
ence to this Directive or shall be accompanied by such reference on theoccasion of their official publication. The methods of making such a
reference shall be laid down by Member States.
2. Member States shall communicate to the Commission the texts of
the provisions of national law which they adopt in the field governedby thisDirective.
Article 18
Entryintoforce
ThisDirective s hall enter into force on the 20th day following its
publication in the Official Journal of the European Communities .
Article 19
Furtherreductioninemissionlimit values
The European Parliament and the Council shall decide, by the end of
the year 2000 on a proposal which the Commission will submit before
the end of 1999, on a further reduction in emission limit values, takinginto account the global availability of techniquesfor controlling air-polluting emissions from compression ignition engines and the airquality situation.1997L0068 — EN — 11.02.2003 — 002.001 — 15
(1) OJ L 184, 17.7.1999, p. 23.▼B
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Article 20
Addressees
This Directive is addressed to the Member States.1997L0068 — EN — 11.02.2003 — 002.001 — 16
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List of Annexes
ANNEX I Scope, definitions, symbols and abbreviations, engine
markings, specifications and tests, specification of confor-
mity of production assessments, parameters defining the
engine family, choice of the parent engine
ANNEX II Information documents
Appendix 1 Essential characteristics of the (parent) engine
Appendix 2 Essential characteristics of the engine familyAppendix 3 Essential characteristics of engine type within family
ANNEX III Test procedure for CI Engines
Appendix 1 Measurement and sampling proceduresAppendix 2 Calibration of the analytical instruments
Appendix 3 Data evaluation and calculations
ANNEX IV Test procedure — Spark ignition enginesAppendix 1 Measurement and sampling procedures
Appendix 2 Calibration of the analytical instruments
Appendix 3 Data evaluation and calculationsAppendix 4 Deterioration factors
ANNEX V Technical characteristics of reference fuel prescribed for
approval tests and to verify conformity of production
Non-road mobile machinery reference fuel for CI engines
ANNEX VI Analytical and sampling systemANNEX VII Type approval certificate
Appendix 1 Test result for CI engines
Appendix 2 Test result for SI enginesAppendix 3 Equipment and auxiliaries to be installed for the test to
determine engine power
ANNEX VIII Approval certificate numbering systemANNEX IX List of engine/engine family type-approvals issued
ANNEX X List of engines produced
ANNEX XI Data sheet of type approved enginesANNEX XII Recognition of alternative type approvals1997L0068 — EN — 11.02.2003 — 002.001 — 17
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ANNEX I
SCOPE, DEFINITIONS, SYMBOLS AND ABBREVIATIONS, ENGINE
MARKINGS, SPECIFICATIONS AND TESTS, SPECIFICATION OF
CONFORMITY OF PRODUCTION ASSESSMENTS, PARAMETERS
DEFINING THE ENGINE FAMILY, CHOICE OF THE PARENT
ENGINE
1. SCOPE
ThisDirective appliesto all enginesto be ins talled in non-road mobile
machinery and to secondary engines fitted into vehicles intended for
passenger or goods transport on the road.
ThisDirective doesnot apply to enginesfor the propuls ion of:
— vehiclesasdefined by Directive 70/156/EEC (1), and by Directive
92/61/EEC (2),
— agricultural tractorsasdefined by Directive 74/150/EEC (3).
Additionally, in order to be covered by thisDirective, the engineshave
to be installed in machinery which meets the following specific require-
ments:
A.intendedandsuited,tomove,ortobemovedontheground,
with o rwithoutroad,andwitheither
(i)aCIenginehavinganetpowerinaccordancewithsection2.4
thatishigherthan18kWbutnotmorethan560kW(4)and
thatisoperatedunderintermittentspeedratherthanasingleconstantspeed.
Machinery,theengines ofwhicharecoveredunderthisde-
finition,includesbutisnotlimitedto:
—industrialdrillingrigs,compressors,etc.,
—constructionequipmentincludingwheelloaders,bulldozers,
crawlertractors,crawlerloaders,truck-typeloaders,off-
highwaytrucks,hydraulicexcavators,etc.,
—agriculturalequipment,rotarytillers,
—forestryequipment,—self-propelledagriculturalvehicles(excepttractorsas
definedabove),
—materialhandlingequipment,
—fork-lifttrucks,
—roadmaintenanceequipment(motorgraders,roadrollers,
asphaltfinishers),
—snow-ploughequipment,—groundsupportequipmentinairports,
—aeriallifts,
—mobilecranes.
or
(ii)aCIenginehavinganetpowerinaccordancewithsection2.4
thatishigherthan18kWbutnotmorethan560kWandthat
isoperatedunderconstantspeed.Limitsonlyapplyfrom31
December2006.
Machinery,theenginesofwhicharecoveredunderthisdefini-
tion,includesbutisnotlimitedto:
—gascompressors,1997L0068—EN—11.02.2003—002.001—18
(1)OJL42,23.2.1970,p.1.DirectiveaslastamendedbyDirective93/81/EEC(OJL264,
23.10.1993,p.49).
(2)OJL225,10.8.1992,p.72.
(3)OJL84,28.3.1974,p.10.DirectiveaslastamendedbyDirective88/297/EEC(OJL
126,20.5.1988,p.52).
(4)AnapprovalgrantedinaccordancewithRegulation49oftheEconomicCommission
forEurope,seriesofamendments02,corrigenda1/2shallbedeemedtobeequivalent
toanapprovalgrantedinaccordancewithDirective88/77/EEC(seeDirective92/53/
EEC,AnnexIV,sectionII).▼M2
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— generating sets with intermittent load including refriger-
ating units and welding sets,
— water pumps,
— turf care, chippers, snow removal equipment, sweepers;or
(iii) a petrol fuelled SI engine having a net power in accordance
with section 2.4 of not more than 19 kW.Machinery, the enginesof which are covered under thisdefini-
tion, includesbut isnot limited to:
—lawnmowers,
—chainsaws,—generators,—waterpumps,—bushcutters.
TheDirectiveisnotapplicableforthefollowingapplications:
B.ships;
C.railwaylocomotives;
D.aircraft;
E.recreationalvehicles,e.g.
—snowmobiles,
—offroadmotorcycles,
—all-terrainvehicles
2.DEFINITIONS,SYMBOLSANDABBREVIATIONS
ForthepurposeofthisDirective,
2.1. compression ignition (C.I.) engine shall mean an engine which works
on the compression-ignition principle (e.g. diesel engine);
2.2. gaseous pollutants shall mean carbon monoxide, hydrocarbons
(assuming a ratio of C
1:H1.85and oxidesof nitrogen, the las t named
being expressed in nitrogen dioxide (NO2equivalent;
2.3. particulate pollutants shall mean any material collected on a specified
filter medium after diluting C.I. engine exhaust gas with clean filtered
air so that the temperature does not exceed 325 K (52 ºC);
2.4. net power shall mean the power in ‘EEC kW’ obtained on the test
bench at the end of the crankshaft, or its equivalent, measured in accor-dance with the EEC method of measuring the power of internal
combustion engines for road vehicles as set out in Directive 80/1269/
EEC (
1), except that the power of the engine cooling fan isexcluded (2)
and the test conditions and reference fuel specified in this Directive areadhered to;
2.5. rated speed shall mean the maximum full load speed allowed by the
governor ass pecified by the manufacturer;
2.6. per cent load shall mean the fraction of the maximum available torque
at an engine speed;
2.7. maximum torque speed shall mean the engine speed at which the
maximum torque isobtained from the engine, ass pecified by the manu-facturer;
2.8. intermediate speed shall mean that engine speed which meets one of the
following requirements:
— for engines which are designed to operate over a speed range on a
full load torque curve, the intermediate speed shall be the declared
maximum torque speed if it occurs between 60 % and 75 % of rated
speed,1997L0068 — EN — 11.02.2003 — 002.001 — 19
(1) OJ L 375, 31.12.1980, p. 46. Directive aslas t amended by Directive 89/491/EEC (OJ L
238, 15.8.1989, p. 43).
(2) Thismeansthat, contrary to the requirementsof s ection 5.1.1.1 of Annex I to Directive
80/1269/EEC, the engine cooling fan must not be installed during the test for the check
of the engine net power; if on the contrary the manufacturer carriesout the tes t with thefan installed on the engine, the power absorbed by the fan itself must be summed up tothe power so measured ►
M2, except for cooling fansof air cooled enginesdirectly
fitted on the crankshaft (see Appendix 3 of Annex VII) ◄.◄
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— if the declared maximum torque speed is less than 60 % of rated
speed, then the intermediate speed shall be 60 % of the rated speed,
— if the declared maximum torque speed is greater than 75 % of the
rated speed then the intermediate speed shall be 75 % of rated
speed,
— for engines to be tested on cycle G1, the intermediate speed shall be
85 % of the maximum rated speed (see section 3.5.1.2 of Annex
IV);
2.9. adjustable parameter shall mean any physically adjustable device,
system or element of design which may affect emission or engine
performance during emission testing or normal operation;
2.10. after-treatment shall mean the passage of exhaust gases through a
device or system whose purpose is chemically or physically to alter
the gases prior to release to the atmosphere;
2.11. spark ignition (SI) engine shall mean an engine which works on the
spark-ignition principle;
2.12. auxiliary emission control device shall mean any device that senses
engine operation parameters for the purpose of adjusting the operation
of any part of the emission control system;
2.13. emission control system shall mean any device, system or element of
design which controls or reduces emissions;
2.14. fuel system shall mean all components involved in the metering and
mixture of the fuel;
2.15. secondary engine shall mean an engine installed in or on a motor
vehicle, but not providing motive power to the vehicle;
2.16. mode length meansthe time between leaving the s peed and/or torque of
the previousmode or the preconditioning phas e and the beginning of
the following mode. It includesthe time during which s peed and/or
torque are changed and the stabilisation at the beginning of each mode;
►M22.17.◄Symbolsandabbreviations
►M22.17.1.◄Symbols for test parameters
Symbol Unit Term
Apm2Cross sectional area of the isokinetic
sampling probe
ATm2Cross sectional area of the exhaust pipe
aver Weighted average valuesfor:
m3/h — volume flow
kg/h — mass flow
C1 — Carbon 1 equivalent hydrocarbon
conc ppm
Vol %Concentration (with suffix of the component
nominating)
conccppm
Vol %Background corrected concentration
concdppm
Vol %Concentration of dilution air
DF — Dilution factor
fa— Laboratory atmospheric factor
FFH— Fuel specific factor used for the calculations
of wet concentrationsfrom dry concentra-
tionshydrogen to carbon ratio
GAIRWkg/h Intake air mass flow rate on wet basis
GAIRDkg/h Intake air mass flow rate on dry basis
GDILWkg/h Dilution air mass flow rate on wet basis
GEDFWkg/h Equivalent diluted exhaust gas mass flow
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GEXHWkg/h Exhaust gas mass flow rate on wet basis
GFUELkg/h Fuel mass flow rate
GTOTWkg/h Diluted exhaust gas mass flow rate on wet
basis
HREFg/kg Reference value of absolute humidity
10,71 g/kg for calculation of NOxand parti-
culate humidity correction factors
Hag/kg Absolute humidity of the intake air
Hdg/kg Absolute humidity of the dilution air
i — Subscript denoting an individual mode
KH— Humidity correction factor for NOx
Kp— Humidity correction factor for particulate
KW,a— Dry to wet correction factor for the intake
air
KW,d— Dry to wet correction factor for the dilution
air
KW,e— Dry to wet correction factor for the diluted
exhaust gas
KW,r— Dry to wet correction factor for the raw
exhaust gas
L % Percent torque related to the maximum
torque for the test speed
mass g/h Subscript denoting emissions mass flow rate
MDILkg Mass of the dilution air sample passed
through the particulate sampling filters
MSAMkg Mass of the diluted exhaust sample passed
through the particulate sampling filters
Mdmg Particulate sample mass of the dilution air
collected
Mfmg Particulate sample mass collected
PakPa Saturation vapour pressure of the engine
intake air (ISO 3046: psy= PSY test
ambient)
pBkPa Total barometric pressure (ISO 3046:
Px= PX Site ambient total pressure
Py= PY Test ambient total pressure)
pdkPa Saturation vapour pressure of the dilution
air
pskPa Dry atmospheric pressure
P kW Power, brake uncorrected
PAEkW Declared total power absorbed by auxiliaries
fitted for the test which are not required by
paragraph 2.4. of thisAnnex
PMkW Maximum measured power at the test speed
under test conditions (see Annex VI,
Appendix 1)
PmkW Power measured at the different test modes
q — Dilution ratio
r — Ratio of cross sectional areas of isokinetic
probe and exhaust pipe
Ra% Relative humidity of the intake air
Rd% Relative humidity of the dilution air
Rf— FID response factor
S kW Dynamometer setting1997L0068 — EN — 11.02.2003 — 002.001 — 21
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TaK Absolute temperature of the intake air
TDK Absolute dewpoint temperature
TrefK Reference temperature (of combustion air:
298 K)
VAIRDm3/h Intake air volume flow rate on dry basis
VAIRWm3/h Intake air volume flow rate on wet basis
VDILm3Volume of the dilution air sample passed
through the particulate sample filters
VDILWm3/h Dilution air volume flow rate on wet basis
VEDFWm3/h Equivalent diluted exhaust gas volume flow
rate on wet basis
VEXHDm3/h Exhaust gas volume flow rate on dry basis
VEXHWm3/h Exhaust gas volume flow rate on wet basis
VSAMm3Volume of sample through particulate
sampling filters
VTOTWm3/h Diluted exhaust gas volume flow rate on
wet basis
WF — Weighting factor
WFE— Effective weighting factor
►M22.17.2.◄Symbols for the chemical components
CO Carbon monoxide
CO2Carbon dioxide
HC Hydrocarbons
NOxOxidesof nitrogen
NO Nitric oxideNO
2Nitrogen dioxide
O2Oxygen
C2H6Ethane
PT Particulate
DOP Di-octylphthalate
CH4Methane
C3H8Propane
H2O Water
PTFE Polytetrafluoroethylene
►M22.17.3.◄Abbreviations
FID Flame ionization detector
HFID Heated flame ionization detectorNDIR Non-dispersive infrared analyser
CLD Chemiluminescent detector
HCLD Heated chemiluminescent detectorPDP Positive displacement pump
CFV Critical flow venturi
3. ENGINE MARKINGS
3.1. Compression ignition engines approved in accordance with this Direc-
tive must bear:1997L0068 — EN — 11.02.2003 — 002.001 — 22
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3.1.1. the trade mark or trade name of the manufacturer of the engine;
3.1.2. the engine type, engine family (if applicable), and a unique engine
identification number;
3.1.3. the EC type-approval number asdes cribed in ►M2Annex VIII ◄.
3.2. Spark-ignition enginesapproved in accordance with thisDirective mus t
bear:
3.2.1. the trade mark or trade name of the manufacturer of the engine;3.2.2. the EC type-approval number asdefined in Annex VIII.
►
M23.3.◄These marks must be durable for the useful life of the engine
and mus t be clearly legible and indelible. If labelsor platesare us ed,
they must be attached in such a manner that in addition the fixing is
durable for the useful life of the engine, and the labels/plates cannot
be removed without destroying or defacing them.
►M23.4.◄These marks must be secured to an engine part necessary for
normal engine operation and not normally requiring replacement during
engine life.
►M23.4.1.◄These marks must be located so as to be readily visible to the
average person after the engine has been completed with all the auxili-
aries necessary for engine operation.
►M23.4.2.◄Each engine must be provided with a supplementary movable
plate in a durable material, which must bear all data indicated under
section 3.1, to be positioned, if necessary, in order to make the marks
referred to under section 3.1 readily visible to the average person and
easily accessible when the engine is installed in a machine.
►M23.5.◄The coding of the enginesin context with the identification
numbers must be such that it allows for the indubitable determination
of the sequence of production.
►M23.6.◄Before leaving the production line the enginesmus t bear all
markings.
►M23.7.◄The exact location of the engine markingss hall be declared in
►M2Annex VII ◄, Section 1.
4. SPECIFICATIONS AND TESTS
4.1.CIengines
►M24.1.1.◄General
The components liable to affect the emission of gaseous and particulate
pollutants shall be so designed, constructed and assembled as to enable
the engine, in normal use, despite the vibrations to which it may be
subjected, to comply with the provisions of this Directive.
The technical measures taken by the manufacturer must be such as to
ensure that the mentioned emissions are effectively limited, pursuant
to thisDirective, throughout the normal life of the engine and under
normal conditions of use. These provisions are deemed to be met if
the provisions of sections ►M24.1.2.1◄,►M24.1.2.3◄and
5.3.2.1 are respectively complied with.
If a catalytic converter and/or a particulatestrap isus ed the manufac-
turer must prove by durability tests, which he himself may carry out
in accordance with good engineering practice, and by corresponding
records, that these after-treatment devices can be expected to function
properly for the lifetime of the engine. The recordsmus t be producedin compliance with the requirementsof s ection 5.2 and in particular
with section 5.2.3. A corresponding warranty must be guaranteed to
the customer. Systematic replacement of the device, after a certain
running time of the engine, is permissible. Any adjustment, repair,
disassembly, cleaning, or replacement of engine components or systems
which isperformed on a periodic bas isto prevent malfunction of the
engine in context with the after-treatment device, shall only be done to
the extent that is technologically necessary toassure proper functioning
of the emission control system. Accordingly scheduled maintenance
requirements must be included in the customer's manual, and be
covered by the warranty provisions mentioned above, and be approved1997L0068 — EN — 11.02.2003 — 002.001 — 23
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before an approval isgranted. The corres ponding extract from the
manual with respect to maintenance/replacements of the treatment
device(s), and to the warranty conditions, must be included in the infor-
mation document ass et out in Annex II to thisDirective.
►M24.1.2.◄Specifications concerning the emissions of pollutants
The gaseous and particulate components emitted by the engine
submitted for testing shall be measured by the methods described in
►M2Annex VI ◄.
Other systems or analysers may be accepted if they yield equivalent
results to the following reference systems:
— for gaseous emissions measured in the raw exhaust, the system
shown in Figure 2 of ►M2Annex VI ◄,
— for gaseous emissions measured in the dilute exhaust of a full flow
dilution system, the system shown in Figure 3 of ►M2Annex
VI◄,
— for particulate emissions, the full flow dilution system, operating
either with a separate filter for each mode or with the single filter
method, shown in Figure 13 of ►M2Annex VI ◄.
The determination of system equivalency shall be based on a seven-test
cycle (or larger) correlation study between the system under considera-
tion and one or more of the above reference systems.
The equivalency criterion isdefined asa ± 5 % agreement of the
averages of the weighted cycle emissions values. The cycle to be used
shall be that given in Annex III, section 3.6.1.
For introduction of a new system into the Directive the determination of
equivalency shall be based upon the calculation of repeatability and
reproducibility, asdes cribed in ISO 5725.
►M24.1.2.1.◄The emissions of the carbon monoxide, the emissions of
hydrocarbons, the emissions of the oxides of nitrogen and the emissions
of particulates obtained shall for stage I not exceed the amount shown
in the table below:
Net power
(P)
(kW)Carbon monoxide
(CO)
(g/kWh)Hydrocarbons
(HC)
(g/kWh)Oxidesof
nitrogen
(NOx)
(g/kWh)Particulates
(PT)
(g/kWh)
130≤P≤560 5,0 1,3 9,2 0,54
75≤P < 130 5,0 1,3 9,2 0,70
37≤P < 75 6,5 1,3 9,2 0,85
►M24.1.2.2.◄The emission limits given in point ►M24.1.2.1◄are
engine-out limits and shall be achieved before any exhaust after-treat-
ment device.
►M24.1.2.3.◄The emissions of the carbon monoxide, the emissions of
hydrocarbons, the emissions of the oxides of nitrogen and the emissions
of particulates obtained shall for stage II not exceed amounts shown in
the table below:
Net power
(P)
(kW)Carbon monoxide
(CO)
(g/kWh)Hydrocarbons
(HC)
(g/kWh)Oxidesof
nitrogen
(NOx)
(g/kWh)Particulates
(PT)
(g/kWh)
130≤P≤560 3,5 1,0 6,0 0,2
75≤P < 130 5,0 1,0 6,0 0,3
37≤P < 75 5,0 1,3 7,0 0,4
18≤P < 37 5,5 1,5 8,0 0,81997L0068 — EN — 11.02.2003 — 002.001 — 24
▼B
►M24.1.2.4.◄Where, asdefined according to Section 6 in conjunction with
Annex II, Appendix 2, one engine family coversmore than one power
band, the emission values of the parent engine (type approval) and of
all engine types within the same family (COP) must meet the more
stringent requirements of the higher power band. The applicant has the
free choice to restrict the definition of engine families to single power
bands, and to correspondingly apply for certification.
4.2.SIengines
4.2.1. General
The components liable to affect the emission of gaseous pollutants shall
be so designed, constructed and assembled as to enable the engine, in
normal use, despite the vibrations to which it may be subjected, to
comply with the provisions of this Directive.
The technical measures taken by the manufacturer must be such as to
ensure that the mentioned emissions are effectively limited, pursuant
to thisDirective, throughout the normal life of the engine and under
normal conditionsof us e in accordance with Annex IV, Appendix 4.
4.2.2. Specifications concerning the emissions of pollutants.
The gaseous components emitted by the engine submitted for testing
shall be measured by the methods described in Annex VI (and shall
include any after-treatment device).
Other systems or analysers may be accepted if they yield equivalent
results to the following reference systems:
— for gaseous emissions measured in the raw exhaust, the system
shown in Figure 2 of Annex VI,
— for gaseous emissions measured in the dilute exhaust of a full flow
dilution system, the system shown in figure 3 of Annex VI.
4.2.2.1. The emissions of carbon monoxide, the emissions of hydrocarbons, the
emissions of oxides of nitrogen and the sum of hydrocarbons and
oxides of nitrogen obtained shall for stage I not exceed the amount
shown in the table below:
Stage I
ClassCarbon monoxide
(CO) (g/kWh)Hydrocarbons
(HC) (g/kWh)Oxidesof
nitrogen (NOx) (g/
kWh)Sum of hydrocar-
bonsand oxides
of nitrogen (g/
kWh)
HC + NOx
SH:1 805 295 5,36
SH:2 805 241 5,36SH:3 603 161 5,36SN:1 519 50SN:2 519 40
SN:3 519 16,1
SN:4 519 13,4
4.2.2.2. The emissions of carbon monoxide and the emissions of the sum of
hydrocarbons and oxides of nitrogen obtained shall for stage II not
exceed the amount shown in the table below:
Stage II (*)
ClassCarbon monoxide (CO)
(g/kWh)Sum of hydrocarbonsand oxidesof
nitrogen (g/kWh)
HC + NOx
SH:1 805 501997L0068 — EN — 11.02.2003 — 002.001 — 25
▼M2
▼M2
ClassCarbon monoxide (CO)
(g/kWh)Sum of hydrocarbonsand oxidesof
nitrogen (g/kWh)
HC + NOx
SH:2 805 50
SH:3 603 72SN:1 610 50,0SN:2 610 40,0
SN:3 610 16,1
SN:4 610 12,1
(*) See Annex 4, Appendix 4: deterioration factorsincluded.
The NOxemissions for all engine classes must not exceed 10 g/kWh.
4.2.2.3. Notwithstanding the definition of ‘hand-held engine’ in Article 2 of this
Directive two-stroke engines used to power snowthrowers only have to
meet SH:1, SH:2 or SH:3 standards.
4.3.Installationonthemobilemachinery
The engine installation on the mobile machinery shall comply with the
restrictions set out in the scope of the type-approval. Additionally the
following characteristics in respect to the approval of the engine always
must be met:
4.3.1. intake depression shall not exceed that specified for the approved
engine in Annex II, Appendix 1 or 3 respectively;
4.3.2. exhaust back pressure shall not exceed that specified for the approved
engine in Annex II, Appendix 1 or 3 respectively.
5. SPECIFICATION OF CONFORMITY OF PRODUCTION ASSESS-
MENTS
5.1. With regard to the verification of the existence of satisfactory arrange-
mentsand proceduresfor ens uring effective control of production
conformity before granting type-approval, the approval authority must
also accept the manufacturer's registration to harmonized standard EN
29002 (whose scope covers the engines concerned) or an equivalent
accreditation standard as satisfying the requirements. The manufacturer
must provide details of the registration and undertake to inform the
approval authority of any revisions to its validity or scope. In order to
verify that the requirements of section 4.2 are continuously met,
suitable controls of the production shall be carried out.
5.2. The holder of the approval shall in particular:5.2.1. ensure existence of procedures for the effective control of the quality of
the product;
5.2.2. have access to the control equipment necessary for checking the confor-
mity to each approved type;
5.2.3. ensure that data of test results are recorded and that annexed documents
shall remain available for a period to be determined in accordance with
the approval authority;
5.2.4. analyse the results of each type of test, in order to verify and ensure the
stability of the engine characteristics, making allowance for variations
in the industrial production process;
5.2.5. ensure that any sampling of engines or components giving evidence of
non-conformity with the type of test considered shall give rise to
another sampling and another test. All the necessary steps shall be
taken to re-establish the conformity of the corresponding production.1997L0068 — EN — 11.02.2003 — 002.001 — 26
▼B
▼B
5.3. The competent authority which hasgranted approval may at any time
verify the conformity control methodsapplicable to each production
unit.
5.3.1. In every inspection, the test books and production survey record shall
be presented to the visiting inspector.
5.3.2. When the quality level appears unsatisfactory or when it seems neces-
sary to verify the validity of the data presented in application of section
4.2, the following procedure isadopted:
5.3.2.1. an engine is taken from the series and subjected to the test described in
Annex III. The emissions of the carbon monoxide, the emissions of the
hydrocarbons, the emissions of the oxides of nitrogen and the emissions
of particulates obtained shall not exceed the amounts shown in the table
in section 4.2.1, subject to the requirements of section 4.2.2, or those
shown in the table in section 4.2.3 respectively;
5.3.2.2. if the engine taken from the series does not satisfy the requirements of
section 5.3.2.1 the manufacturer may ask for measurements to be
performed on a sample of engines of the same specification taken
from the series and including the engine originally taken. The manufac-
turershall determine the size n of the sample in agreement with the
technical service. Engines other than the engine originally taken shall
be subjected to a test. The arithmetical mean ( /C22xx) of the results obtained
with the sample shall then be determined for each pollutant. The
production of the series shall then be deemed to confirm if the
following condition ismet:
/C22xxþk/C1St/C20L(1)
where:
L isthe limit value laid down in s ection 4.2.1/4.2.3 for each pollutant
considered,
k is a statistical factor depending on n and given in the following table:
n23456789 1 0
k 0,973 0,613 0,489 0,421 0,376 0,342 0,317 0,296 0,279
n 1 11 21 31 41 51 61 71 81 9
k 0,265 0,253 0,242 0,233 0,224 0,216 0,210 0,203 0,198
if n≥20, k ¼0;860ﬃﬃﬃnp
5.3.3. The approval authority or the technical service responsible for verifying
the conformity of production shall carry out tests on engines which
have been run-in partially or completely, according to the manufac-
turer's specifications.
5.3.4. The normal frequency of inspections authorized by the competent
authority shall be one per year. If the requirements of section 5.3.2 are
not met, the competent authority shall ensure that all necessary steps
are taken to re-establish the conformity of production as rapidly as
possible.
6. PARAMETERS DEFINING THE ENGINE FAMILY
The engine family may be defined by basic design parameters which
must be common to engines within the family. In some cases there
may be interaction of parameters. These effects must also be taken
into consideration to ensure that only engines with similar exhaust
emission characteristics are included within an engine family.
In order that engines may be considered to belong to the same engine
family, the following list of basic parameters must be common:1997L0068 — EN — 11.02.2003 — 002.001 — 27
(1)S2
t¼Xx/C0/C22xxðÞ2
n/C01where x is any one of the individual results obtained with the sample
n.
▼B
6.1. Combustion cycle:
— 2 cycle
— 4 cycle
6.2. Cooling medium:
— air
— water— oil
6.3. Individual cylinder displacement, within 85 % and 100 % of the largest
displacement within the engine family
6.4. Method of air aspiration6.5. Fuel type
— Diesel
— Petrol.
6.6. Combustion chamber type/design
6.7. Valve and porting — configurations, size and number6.8. Fuel system
For diesel:
— pump-line injector
— in-line pump— distributor pump
— single element
— unit injector.
For petrol:
— carburettor
— port fuel injection— direct injection.
6.9. Miscellaneous features
— Exhaust gas recirculation
— Water injection/emulsion— Air injection— Charge cooling system— Ignition type (compression, spark).
6.10. Exhaust after-treatment
— Oxidation catalyst
— Reduction catalyst
— Three way catalyst— Thermal reactor— Particulate trap
7. CHOICE OF THE PARENT ENGINE
7.1. The parent engine of the family shall be selected using the primary
criteria of the highest fuel delivery per stroke at the declared maximum
torque speed. In the event that two or more engines share this primary
criteria, the parent engine shall be selected using the secondary criteria
of highest fuel delivery per stroke at rated speed. Under certain circum-
stances, the approval authority may conclude that the worst case
emission rate of the family can best be characterized by testing a
second engine. Thus, the approval authority may select an additional
engine for test based upon features which indicate that it may have the
highest emission levels of the engines within that family.
7.2. If engineswithin the family incorporate other variable featureswhich
could be considered to affect exhaust emissions, these features must
also be identified and taken into account in the selection of the parent
engine.1997L0068 — EN — 11.02.2003 — 002.001 — 28
▼M2
▼B
▼B
ANNEX II
INFORMATIONDOCUMENTNo.…
relatingtotype-approvalandreferringtomeasuresagainsttheemissionofgaseousandparticu-
latepollutantsfrominternalcombustionenginestobeinstalledinnon-roadmobilemachinery
(Directive 97/68/EC as last amended by Directive ../…/EC)
1997L0068 — EN — 11.02.2003 — 002.001 — 29
▼B
Appendix 1
1997L0068 — EN — 11.02.2003 — 002.001 — 30
▼B
1997L0068 — EN — 11.02.2003 — 002.001 — 31
▼B
1997L0068 — EN — 11.02.2003 — 002.001 — 32
▼B
Appendix 2
►(1)M21997L0068 — EN — 11.02.2003 — 002.001 — 33
▼B
Appendix 3
1997L0068 — EN — 11.02.2003 — 002.001 — 34
▼B
►(1)M21997L0068 — EN — 11.02.2003 — 002.001 — 35
▼B
►(1) (2) (3) (4) (5) (6)M21997L0068 — EN — 11.02.2003 — 002.001 — 36
▼B
ANNEX III
TESTPROCEDUREFORC.I.ENGINES
1. INTRODUCTION
1.1. This Annex describes the method of determining emissions of gaseous
and particulate pollutantsfrom the enginesto be tes ted.
1.2. The test shall be carried out with the engine mounted on a test bench
and connected to a dynamometer.
2. TEST CONDITIONS
2.1.Generalrequirements
All volumesand volumetric flow ratess hall be related to 273 K (0 ºC)
and 101,3 kPa.
2.2.Enginetestconditions
2.2.1. The absolute temperature Taof the engine intake air expressed in
Kelvin, and the dry atmospheric pressure ps, expressed in kPa, shall be
measured, and the parameter fashall be determined according to the
following provisions:
Naturally aspirated and mechanically supercharged engines:
fa¼99
ps/C18/C19T
298/C18/C190;7
Turbocharged engine with or without cooling of the intake air:
fa¼99
ps/C18/C190;7
/C2T
298/C18/C191;5
2.2.2. Test validity
For a test to be recognized as valid, the parameter fashall be such that:
0,96≤fa≤1,06
2.2.3. Engines with charge air cooling
The temperature of the cooling medium and the temperature of the
charge air have to be recorded.
2.3.Engineairinletsystem
The test engine shall be equipped with an air inlet system presenting an
air inlet restriction at the upper limit specified by the manufacturer for a
clean air cleaner at the engine operating conditionsass pecified by the
manufacturer which result in maximum air flow.
A test shop system may be used, provided it duplicates actual engine
operating conditions.
2.4.Engineexhaustsystem
The test engine shall be equipped with an exhaust system presenting an
exhaust back pressure at the upper limit specified by the manufacturer
for the engine operating conditionswhich res ult in maximum declared
power.1997L0068 — EN — 11.02.2003 — 002.001 — 37
▼M2
▼B
▼M1
▼B
▼B
2.5.Coolingsystem
An engine cooling system with sufficient capacity to maintain the
engine at normal operating temperaturespres cribed by the manufac-
turer.
2.6.Lubricatingoil
Specifications of the lubricating oil used for the test shall be recorded
and presented with the results of the test.
2.7.Testfuel
The fuel shall be the reference fuel specified in ►M2Annex V ◄.
The cetane number and the sulphur content of the reference fuel used
for test shall be recorded at sections 1.1.1 and 1.1.2 respectively of
►M2Annex VII ◄, Appendix 1.
The fuel temperature at the injection pump inlet shall be 306-316 K
(33-43 ºC).
2.8.Determinationofdynamometersettings
The settings of inlet restriction and exhaust pipe backpressure shall be
adjusted to the manufacturer's upper limits, in accordance with sections
2.3 and 2.4.
The maximum torque values at the specified test speeds shall be deter-
mined by experimentation in order to calculate the torque valuesfor the
specified test modes. For engines which are not designed to operate
over a speed range on a full load torque curve, the maximum torque at
the test speeds shall be declared by the manufacturer.
The engine setting for each test mode shall be calculated using the
formula:
S¼PMþPAE ðÞ /C2L
100/C18/C19
/C0PAE
If the ratio,
PAE
PM/C210;03
the value of PAEmay be verified by the technical authority granting type
approval.
3. TEST RUN
3.1.Preparationofthesamplingfilters
At least one hour before the test, each filter (pair) shall be placed in a
closed, but unsealed, petri dish and placed in a weighing chamber for
stabilization. At the end of the stabilization period, each filter (pair)
shall be weighed and the tare weight shall be recorded. The filter
(pair) shall then be stored in a closed petri dish or filter holder until
needed for testing. If the filter (pair) is not used within eight hours of
itsremoval from the weighing chamber, it mus t be reweighed before
use.
3.2.Installationofthemeasuringequipment
The instrumentation and sample probes shall be installed as required.
When using a full flow dilution system for exhaust gas dilution, the
tailpipe shall be connected to the system.
3.3.Startingthedilutionsystemandengine
The dilution system and the engine shall be started and warmed up until
all temperatures and pressures have stabilized at full load and rated
speed (section 3.6.2).1997L0068 — EN — 11.02.2003 — 002.001 — 38
▼B
3.4.Adjustmentofthedilutionratio
The particulate sampling system shall be started and running on bypass
for the single filter method (optional for the multiple filter method).
The particulate background level of the dilution air may be determined
by passing dilution air through the particulate filters. If filtered dilution
air is used, one measurement may be done at any time prior to, during,
or after the test. If the dilution air is not filtered, measurements at a
minimum of three points, after the starting, before the stopping, and at
a point near the middle of the cycle, are required, and the valuesaver-
aged.
The dilution air shall be set to obtain a maximum filter face tempera-
ture of 325 K (52 ºC) or less at each mode. The total dilution ratio shall
not be less than four.
For the single filter method, the sample mass flow rate through the
filter shall be maintained at a constant proportion of the dilute exhaust
mass flow rate for full flow systems for all modes. This mass ratio shall
be within ± 5 %, except for the first 10 seconds of each mode for
systems withoutbypass capability. For partial flow dilution systems
with single filter method, the mass flow rate through the filter shall be
constant within ± 5 % during each mode, except for the first 10 seconds
of each mode for systems without bypass capability.
For CO2or NOxconcentration controlled systems, the CO2or NOxcontent of the dilution air must be measured at the beginning and at
the end of each test. The pre and post test background CO2or NOxconcentration measurements of the dilution air must be within 100 ppmor 5 ppm of each other, respectively.
When using a dilute exhaust gas analysis system, the relevant back-
ground concentrations shall be determined by sampling dilution air
into a sampling bag over the complete test sequence.
Continuous(non bag) background concentration may be taken at the
minimum of three points, at the beginning, at the end, and a point
near the middle of the cycle and averaged. At the manufacturer's
request background measurements may be omitted.
3.5.Checkingtheanalysers
The emission analysers shall be set at zero and spanned.
3.6.Testcycle
3.6.1. Equipment specifications according to section 1(A) of Annex I:
3.6.1.1. Specification A: For enginescovered by Section 1(A)(i) of Annex I, the
following eight-mode cycle (
1) shall be followed in dynamometer opera-
tion on the test engine:
Mode
numberEngine speed Load (%)Weighting
factor
1 Rated 100 0,15
2 Rated 75 0,153 Rated 50 0,154 Rated 10 0,1
5 Intermediate 100 0,1
6 Intermediate 75 0,17 Intermediate 50 0,18 Idle — 0,151997L0068 — EN — 11.02.2003 — 002.001 — 39
(1) Identical with C1 cycle of the draft ISO 8178-4 standard.▼M2
▼B
▼M2
3.6.1.2. Specification B. For enginescovered by Sections1(A)(ii), the following
five-mode cycle (1) shall be followed in dynamometer operation on the
test engine:
Mode
numberEngine speed Load % Weighting factor
1 Rated 100 0,05
2 Rated 75 0,253 Rated 50 0,3
4 Rated 25 0,3
5 Rated 10 0,1
The load figuresare percentage valuesof the torque corres ponding to
the prime power rating defined asthe maximum power available during
a variable power sequence, which may be run for an unlimited number
of hoursper year, between s tated maintenance intervalsand under the
stated ambient conditions, the maintenance being carried out as
prescribed by the manufacturer. (
2).
3.6.2. Conditioning of the engine
Warming up of the engine and the system shall be at maximum speed
and torque in order to stabilize the engine parameters according to the
recommendationsof the manufacturer.
Note:The conditioning period should also prevent the influence of
deposits from a former test in the exhaust system. There is also
a required period of stabilization between test points which has
been included to minimise point to point influences.
►M23.6.3. Test sequence
The test sequence shall be started. The test shall be performed in
ascending order of mode numbers as set out above for the test cycles.
During each mode of the given test cycle ◄after the initial transition
period, the specified speed shall be held to within ± 1 % of rated speed
or ± 3 min−1whichever isgreater except for low idle which s hall be
within the tolerancesdeclared by the manufacturer. The s pecified
torque shall be held so that the average over the period during which
the measurements are being taken is within ± 2 % of the maximum
torque at the test speed.
For each measuring point a minimum time of 10 minutes is necessary.
If for the testing of an engine, longer sampling times are required for
reasons of obtaining sufficient particulate mass on the measuring filter
the test mode period can be extended as necessary.
The mode length shall be recorded and reported.
The gaseous exhaust emission concentration values shall be measured
and recorded during the last three minutes of the mode.
The particulate sampling and the gaseous emission measurement should
not commence before engine stabilization, as defined by the manufac-
turer, hasbeen achieved and their completion mus t be coincident.
The fuel temperature shall be measured at the inlet to the fuel injection
pump or as specified by the manufacturer, and the location of measure-
ment recorded.
3.6.4. Analyser response
The output of the analysers shall be recorded on a strip chart recorder
or measured with an equivalent data acquisition system with the
exhaust gas flowing through the analysers at least during the last three1997L0068 — EN — 11.02.2003 — 002.001 — 40
(1) Identical with D2 cycle of the ISO 8178-4: 1996(E) standard.
(2) For a better illustration of the prime power definition, see figure 2 of ISO 8528-1:
1993(E) standard.▼B
▼B
minutesof each mode. If bag s ampling isapplied for the diluted CO
and CO2measurement (see Appendix 1, section 1.4.4), a sample shall
be bagged during the last three minutes of each mode, and the bag
sample analysed and recorded.
3.6.5. Particulate sampling
The particulate sampling can be done either with the single filter
method or with the multiple filter method (Appendix 1, section 1.5).
Since the results of the methods may differ slightly, the method used
must be declared with the results.
For the single filter method the modal weighting factors specified in the
test cycle procedure shall be taken into account during sampling by
adjusting sample flow rate and/or sampling time, accordingly.
Sampling must be conducted as late as possible within each mode. The
sampling time per mode must be at least 20 seconds for the single filter
method and at least 60 seconds for the multi-filter method. For systems
without bypass capability, the sampling time per mode must be a least
60 seconds for single and multiple filter methods.
3.6.6. Engine conditions
The engine speed and load, intake air temperatur, fuel flow and air or
exhaust gas flow shall be measured for each mode once the engine has
been stabilized.
If the measurement of the exhaust gas flow or the measurement of
combustion air and fuel consumption is not possible, it can be calcu-
lated using the carbon and oxygen balance method (see Appendix 1,
section 1.2.3).
Any additional data required for calculation shall be recorded (see
Appendix 3, sections 1.1 and 1.2).
3.7.Re-checkingtheanalysers
After the emission test a zero gas and the same span gas will be used
for re-checking. The test will be considered acceptable if the difference
between the two measuring results is less than 2 %.1997L0068 — EN — 11.02.2003 — 002.001 — 41
▼B
Appendix 1
1. MEASUREMENT AND SAMPLING PROCEDURES
Gaseous and particulate components emitted by the engine submitted
for testing shall be measured by the methods described in
►M2Annex VI ◄. The methodsof ►M2Annex VI ◄describe
the recommended analytical systems for the gaseous emissions (section
1.1) and the recommended particulate dilution and sampling systems
(section 1.2).
1.1.Dynamometerspecification
An engine dynamometer with adequate characteristics to perform the
test cycle described in Annex III, section 3.6.1 shall be used. The
instrumentation for torque and speed measurement shall allow the
measurement of the shaft power within the given limits. Additional
calculations may be necessary.
The accuracy of the measuring equipment must be such that the
maximum tolerancesof the figuresgiven in point 1.3 are not exceeded.
1.2.Exhaustgasflow
The exhaust gas flow shall be determined by one of the methods
mentioned in sections 1.2.1 to 1.2.4.
1.2.1. Direct measurement method
Direct measurement of the exhaust flow by flow nozzle or equivalent
metering system (for detail see ISO 5167).
Note:Direct gaseous flow measurement is a difficult task. Precautions
must be taken to avoid measurement errors which will impact
emission value errors.
1.2.2. Air and fuel measurement method
Measurement of the air flow and the fuel flow.
Air flow-metersand fuel flow-meterswith an accuracy defined in
section 1.3 shall be used.
The calculation of the exhaust gas flow is as follows:
GEXHW=GAIRW+GFUEL
(for wet exhaust mass)
or
VEXHD=VAIRD− 0,766 × GFUEL
(for dry exhaust volume)
or
VEXHW=VAIRW+ 0,746 × GFUEL
(for wet exhaust volume)
1.2.3. Carbon balance method
Exhaust mass calculation from fuel consumption and exhaust gas
concentrations using the carbon balance method (see Annex III,
Appendix 3).
1.2.4. Total dilute exhaust gas flow
When using a full flow dilution system, the total flow of the dilute
exhaust (GTOTW,VTOTW) shall be measured with a PDP or CFV — Annex
V, section 1.2.1.2. The accuracy shall confom to the provisions of
Annex III, Appendix 2, section 2.2.1997L0068 — EN — 11.02.2003 — 002.001 — 42
▼B
1.3.Accuracy
The calibration of all measurement instruments shall be traceable to
national (international) standards and comply with the following
requirements:
Number ItemPermissible devia-
tion
(± valuesbas ed on
enginesmaximum
values)Permissible devia-
tion
(± values
according to ISO
3046)Calibration inter-
vals
(months)
1 Engine speed 2 % 2 % 3
2 Torque 2 % 2 % 33 Power 2 % (
1) 3 % not applicable
4 Fuel consumption 2 % (1)3 % 6
5 Specific fuel
consumptionnot applicable 3 % not applicable
6 Air consumption 2 % (1)5 % 6
7 Exhaust gas flow 4 % (1) not applicable 6
8 Coolant temperature 2 K 2 K 39 Lubricant tempera-
ture2K 2K 3
10 Exhaust gas pressure 5 % of
maximum5% 3
11 Inlet manifold
depressions5%o f
maximum5% 3
12 Exhaust gas tempera-
ture15 K 15 K 3
13 Air inlet temperature
(combustion air)2K 2K 3
14 Atmospheric pressure 0,5 % of reading 0,5 % 3
15 Intake air humidity
(Relative)3 % not applicable 1
16 Fuel temperature 2 K 5 K 3
17 Dilution tunnel
temperatures1,5 K not applicable 3
18 Dilution air humidity 3 % not applicable 1
19 Diluted exhaust gas
flow2 % of reading not applicable 24 (partial flow)
(full flow) (
2)
(1) The calculations of the exhaust emissions as described in this Directive are, in some cases, based on
different measurement and/or calculation methods. Because of limited total tolerances for the exhaust
emission calculation, the allowable values for some items, used in the appropriate equations, must besmaller than the allowed tolerances given in ISO 3046-3.
(
2) Full flow systems — the CVS positive displacement pump or critical flow Venturi shall be calibrated
following initial installation, major maintenance or as necessary when indicated by the CVS system
verification described in Annex V.1997L0068 — EN — 11.02.2003 — 002.001 — 43
▼B
1.4.Determinationofthegaseouscomponents
1.4.1. General analyser specifications
The analysers shall have a measuring range appropriate for the accuracy
required to measure the concentrations of the exhaust gas components
(section 1.4.1.1). It is recommended that the analysers be operated
such that the measured concentration falls between 15 % and 100 %
of full scale.
If the full scale value is 155 ppm (or ppm C) or less or if read-out
systems (computers, data loggers) that provide sufficient accuracy and
resolution below 15 % of full scale are used concentrations below
15 % of full scale are also acceptable. In this case, additional calibra-
tionsare to be made to ens ure the accuracy of the calibration curves—
Annex III, Appendix 2, section 1.5.5.2.
The electromagnetic compatibility (EMC) of the equipment shall be on
a level asto minimize additional errors .
1.4.1.1. Measurement error
The total measurement error, including the cross sensitivity to other
gases — see Annex III, Appendix 2, point 1.9 shall not exceed ± 5 %
of the reading or 3,5 % of full scale, whichever is smaller. For concen-
trations of less than 100 ppm the measurement error shall not
exceed ± 4 ppm.
1.4.1.2. Repeatability
The repeatability, defined as2,5 timesthe s tandard deviation of 10
repetitive responses to a given calibration or span gas, must be no
greater than ± 1 % of full scale concentration for each range used above
155 ppm (or ppm C) or ± 2 % of each range used below 155 ppm (or
ppm C).
1.4.1.3. Noise
The analyser peak-to-peak response to zero and calibration or span
gases over any 10-second period shall not exceed 2 % of full scale on
all rangesus ed.
1.4.1.4. Zero drift
The zero drift during a one-hour period shall be less than 2 % of full
scale on the lowest range used. The zero response is defined as the
mean response, including noise, to a zero gas during a 30-seconds
time interval.
1.4.1.5. Span drift
The span drift during a one hour period shall be less than 2 % of full
scale on the lowest range used. Span is defined as the difference
between the span response and the zero response. The span response is
defined as the mean response, including noise, to a span gas during a
30-seconds time interval.
1.4.2. Gas drying
The optional gasdrying device mus t have a minimal effect on the
concentration of the measured gases. Chemical dryers are not an accep-
table method of removing water from the sample.
1.4.3. Analysers
Sections 1.4.3.1 to 1.4.3.5 of this Appendix describe the measurement
principles to be used. A detailed description of the measurement
systems is given in ►M2Annex VI ◄.
The gases to be measured shall be analysed with the following instru-
ments. For non-linear analysers, the use of linearizing circuits ispermitted.
1.4.3.1. Carbon m onoxide (CO) analysis
The carbon monoxide analyser shall be of the non-dispersive infra-red
(NDIR) absorption type.
1.4.3.2. Carbon dioxide (CO
2)a n a l y si s
The carbon dioxide analyser shall be of the non-dispersive infra-red
(NDIR) absorption type.1997L0068 — EN — 11.02.2003 — 002.001 — 44
▼B
1.4.3.3. Hydrocarbon (HC) analysis
The hydrocarbon analyser shall be of the heated flame ionization
detector (HFID) type with detector, valves, pipework, etc, heated so as
to maintain a gastemperature of 463 K (190 ºC) ± 10 K.
1.4.3.4. Oxidesof nitrogen (NOx)a n a l y si s
The oxides of nitrogen analyser shall be of the chemiluminescent
detector (CLD) or heated chemiluminescent detector (HCLD) type
with a NO2/NO converter, if measured on a dry basis. If measured on
a wet basis, a HCLD with converter maintained above 333 K (60 ºC)
shall be used, provided the water quench check (Annex III, Appendix
2, section 1.9.2.2) is satisfied.
1.4.4. Sampling for gaseous emissions
The gaseous emissions sampling probes must be fitted at least 0,5 m or
three timesthe diameter of the exhaus t pipe — whichever isthe larger
— upstream of the exit of the exhaust gas system as far as applicable
and sufficiently close to the engine as to ensure an exhaust gas
temperature of at least 343 K (70 ºC) at the probe.
In the case of a multicylinder engine with a branched exhaust manifold,
the inlet of the probe shall be located sufficiently far downstream so as
to ensure that the sample is representative of the average exhaust emis-
sions from all cylinders. In multicylinder engines having distinct groups
of manifolds, such as in a ‘V’-engine configuration, it is permissible to
acquire a sample from each group individually and calculate an average
exhaust emission. Other methods which have been shown to correlate
with the above methods may be used. For exhaust emissions calculation
the total exhaust mass flow of the engine must be used.
If the composition of the exhaust gas is influenced by any exhaust after-
treatment system, the exhaust sample must be taken upstream of this
device in the tests of stage I and downstream of this device in the tests
of stage II. When a full flow dilution system is used for the determina-
tion of the particulates, the gaseous emissions may also be determined
in the diluted exhaust gas. The sampling probes shall be close to the
particulate sampling probe in the dilution tunnel (Annex V, section
1.2.1.2, DT and section 1.2.2, PSP). CO and CO2may optionally be
determined by sampling into a bag and subsequent measurement of the
concentration in the sampling bag.
1.5.Determinationoftheparticulates
The determination of the particulates requires a dilution system. Dilu-
tion may be accomplished by a partial flow dilution system or a full
flow dilution system. The flow capacity of the dilution system shall belarge enough to completely eliminate water condensation in the dilution
and sampling systems, and maintain the temperature of the diluted
exhaust gas at or below 325 K (52 ºC) immediately upstream of the
filter holders. De-humidifying the dilution air before entering the dilu-
tion system is permitted, if the air humidity is high. Dilution air pre-
heating above the temperature limit of 303 K (30 ºC) isrecommended,
if the ambient temperature isbelow 293 K (20 ºC). However, the
diluted air temperature must not exceed 325 K (52 ºC) prior to the
introduction of the exhaust in the dilution tunnel.
For a partial flow dilution system, the particulate sampling probe must
be fitted close to and upstream of the gaseous probe as defined in
section 4.4 and in accordance with Annex V, section 1.2.1.1, figures
4-12 EP and SP.
The partial flow dilution system has to be designed to split the exhaust
stream into two fractions, the smaller one being diluted with air and
subsequently used for particulate measurement. From that it is essential
that the dilution ratio be determined very accurately. Different splitting
methods can be applied, whereby the type of splitting used dictates to a
significant degree the sampling hardware and procedures to be used
(Annex V, section 1.2.1.1).
To determine the mass of the particulates, a particulate sampling
system, particulate sampling filters, a microgram balance and a
temperature and humidity controlled weighing chamber are required.
For particulate sampling, two methods may be applied:
—the single filter method uses one pair of filters (see section 1.5.1.3
of this Appendix) for all modes of the test cycle. Considerable
attention must be paid to sampling times and flows during the1997L0068 — EN — 11.02.2003 — 002.001 — 45
▼B
sampling phase of the test. However, only one pair of filters will be
required for the test cycle,
—the multiple filter method dictates that one pair of filters (see section
1.5.1.3 of thisAppendix) isus ed for each of the individual modesof
the test cycle. This method allows more lenient sample procedures
but uses more filters.
1.5.1. Particulate sampling filters
1.5.1.1. Filter specification
Fluorocarbon coated glass fibre filters or fluorocarbon based membrane
filters are required for certification tests. For special applications
different filter materials may be used. All filter types shall have a
0,3 µm DOP (di-octylphthalate) collection efficiency of at least 95 %
at a gasface velocity between 35 and 80 cm/s . When performing corre-
lation tests between laboratories or between a manufacturer and an
approval authority, filters of identical quality must be used.
1.5.1.2. Filter size
Particulate filtersmus t have a minimum diameter of 47 mm (37 mm
stain diameter). Larger diameter filters are acceptable (section 1.5.1.5).
1.5.1.3. Primary and back-up filters
The diluted exhaust shall be sampled by a pair of filters placed in series
(one primary and one back-up filter) during the test sequence. The
back-up filter shall be located no more than 100 mm downstream of,
and shall not be in contact with the primary filter. The filters may be
weighed separately or as a pair with the filters placed stain side to stain
side.
1.5.1.4. Filter face velocity
A gasface velocity through the filter of 35 to 80 cm/ss hall be
achieved. The pressure drop increase between the beginning and the
end of the test shall be no more than 25 kPa.
1.5.1.5. Filter loading
The recommended minimum filter loading shall be 0,5 mg/1 075 mm2
stain area for the single filter method. For the most common filter size
the valuesare asfollows :
Filter diameter
(mm)Recommended stain
diameter
(mm)Recommended
minimum loading
(mg)
47 37 0,5
70 60 1,390 80 2,3
110 100 3,6
For the multiple filter method, the recommended minimum filter
loading for the sum of all filters shall be the product of the appropriate
value above and the square root of the total number of modes.
1.5.2. Weighing chamber and analytical balance specifications
1.5.2.1. Weighing chamber conditions
The temperature of the chamber (or room) in which the particulate
filtersare conditioned and weighed s hall be maintained to within
295 K (22 ºC) ± 3 K during all filter conditioning and weighing. The
humidity shall be maintained to a dewpoint of 282,5 (9,5 ºC) ± 3 K
and a relative humidity of 45 ± 8 %.
1.5.2.2. Reference filter weighing
The chamber (or room) environment shall be free of any ambient
contaminants (such as dust) that would settle on the particulate filters
during their stabilisation. Disturbances to weighing room specifications
asoutlined in s ection 1.5.2.1 will be allowed if the duration of the
disturbances does not exceed 30 minutes. The weighing room should
meet the required specifications prior to personnel entrance into the
weighing room. At least two unused reference filters or reference filter1997L0068 — EN — 11.02.2003 — 002.001 — 46
▼B
pairs shall be weighed within four hours of, but preferably at the same
time as the sample filter (pair) weighing. They shall be the same size
and material as the sample filters.
If the average weight of the reference filters(reference filter pairs )
changesbetween s ample filter weighing by more than ± 5 % (± 7,5 %
for the filter pair) of the recommended minimum filter loading (section
1.5.1.5), then all sample filters shall be discarded and the emissions test
repeated.
If the weighing room stability criteria outlined in section 1.5.2.1 is not
met, but the reference filter (pair) weighing meet the above criteria, the
engine manufacturer hasthe option of accepting the s ample filter
weights or voiding the tests, fixing the weighing room control system
and re-running the test.
1.5.2.3. Analytical balance
The analytical balance used to determine the weights of all filters shall
have a precision (standard deviation) of 20 µg and a resolution of 10 µg
(1 digit = 10 µg). For filters less than 70 mm diameter, the precision
and resolution shall be 2 µg and 1 µg, respectively.
1.5.2.4. Elimination of static electricity effects
To eliminate the effects of static electricity, the filters shall be neutra-
lized prior to weighing, for example, by a Polonium neutralizer or a
device of similar effect.
1.5.3. Additional specifications for particulate measurement
All parts of the dilution system and the sampling system from the
exhaust pipe up to the filter holder, which are in contact with raw and
diluted exhaust gas, must be designed to minimize deposition or altera-
tion of the particulates. All parts must be made of electrically
conductive materials that do not react with exhaust gas components,
and must be electrically grounded to prevent electrostatic effects.1997L0068 — EN — 11.02.2003 — 002.001 — 47
▼B
Appendix 2
1. CALIBRATION OF THE ANALYTICAL INSTRUMENTS
1.1.Introduction
Each analyzer shall be calibrated as often as necessary to fulfil the
accuracy requirementsof thiss tandard. The calibration method that
shall be used is described in this paragraph for the analysers indicated
in Appendix 1, section 1.4.3.
1.2.Calibrationgases
The shelf life of all calibration gases must be respected.The expiry date of the calibration gases stated by the manufacturer shall
be recorded.
1.2.1. Pure gases
The required purity of the gases is defined by the contamination limits
given below. The following gases must be available for operation:
— purified nitrogen
(contamination ≤1 ppm C, ≤1 ppm CO, ≤400 ppm CO
2,
≤0,1 ppm NO)
— purified oxygen
(purity > 99,5 % vol O2)
— hydrogen-helium mixture
(40 ± 2 % hydrogen, balance helium)
(contamination ≤1 ppm C, ≤400 ppm ►M1CO2◄)
— purified synthetic air
(contamination ≤1 ppm C, ≤1 ppm CO, ≤400 ppm CO2,
≤0,1 ppm NO)
(oxygen content between 18—21 % vol)
1.2.2. Calibration and span gases
Mixture of gases having the following chemical compositions shall be
available:
—C3H8and purified synthetic air (see section 1.2.1)
— CO and purified nitrogen
— NO and purified nitrogen (the amount of NO2contained in thiscali-
bration gasmus t not exceed 5 % of the NO content)
—O2and purified nitrogen
—C O2and purified nitrogen
—C H4and purified synthetic air
—C2H6and purified synthetic air
Note:other gascombinationsare allowed provided the gas esdo not
react with one another.
The true concentration of a calibration and span gas must be within ± 2 %
of the nominal value. All concentrationsof calibration gass hall be
given on a volume basis (volume percent or volume ppm).
The gases used for calibration and span may also be obtained by means
of a gasdivider, diluting with purified N2or with purified synthetic air.
The accuracy of the mixing device must be such that the concentration
of the diluted calibration gases may be determined to within ± 2 %.
1.3.Operatingprocedureforanalysersandsamplingsystem
The operating procedure for analysers shall follow the start-up and
operating instructions of the instrument manufacturer. The minimum
requirements given in sections 1.4 to 1.9 shall be included.
1.4.Leakagetest
A system leakage test shall be performed. The probe shall be discon-
nected from the exhaust system and the end plugged. The analyser
pump shall be switched on. After an initial stabilization period all
flow meters should read zero. If not, the sampling lines shall be
checked and the fault corrected. The maximum allowable leakage rate
on the vacuum side shall be 0,5 % of the in-use flow rate for the1997L0068 — EN — 11.02.2003 — 002.001 — 48
▼B
portion of the system being checked. The analyser flows and bypass
flows may be used to estimate the in-use flow rates.
Another method isthe introduction of a concentration s tep change at
the beginning of the sampling line by switching from zero to span gas.
If after an adequate period of time the reading shows a lower concen-
tration compared to the introduced concentration, thispointsto
calibration or leakage problems.
1.5.Calibrationprocedure
1.5.1. Instrument assembly
The instrument assembly shall be calibrated and calibration curves
checked against standard gases. The same gas flow rates shall be used
as when sampling exhaust.
1.5.2. Warming-up time
The warming-up time should be according to the recommendations of
the manufacturer. If not specified, a minimum of two Hours is recom-
mended for warming-up the analysers.
1.5.3. NDIR and HFID analyser
The NDIR analyser shall be tuned, as necessary, and the combustion
flame of the HFID analyser shall be optimized (section 1.8.1).
1.5.4. Calibration
Each normally used operating range shall be calibrated.Using purified synthetic air (or nitrogen), the CO, CO
2,N ox, HC and O2analysers shall be set at zero.The appropriate calibration gases shall be introduced to the analysers,
the values recorded, and the calibration curve established according to
section 1.5.6.
The zero setting shall be re-checked and the calibration procedure
repeated, if necessary.
1.5.5. Establishment of the calibration curve
1.5.5.1. General guidelines
The analyser calibration curve is established by at least five calibration
points (excluding zero) spaced as uniformly as possible. The highest
nominal concentration must be equal to or higher than 90 % of full
scale.
The calibration curve is calculated by the method of least squares. If the
resulting polynomial degree is greater than three, the number of calibra-
tion points (zero included) must be at least equal to this polynomial
degree plustwo.
The calibration curve must not differ by more than ± 2 % from the
nominal value of each calibration point and by more than ± 1 % of
full scale at zero.
From the calibration curve and the calibration points, it is possible to
verify that the calibration hasbeen carried out correctly. The different
characteristic parameters of the analyser must be indicated, particularly:
— the measuring range,
— the sensitivity,— the date of carrying out the calibration.
1.5.5.2. Calibration below 15 % of full scale
The analyser calibration curve is established by at least ten calibration
points (excluding zero) spaced so that 50 % of the calibration points is
below 10 % of full scale.
The calibration curve is calculated by the method of least squares.
The calibration curve must not differ by more than ± 4 % from the
nominal value of each calibration point and by more than ± 1 % of
full scale at zero.1997L0068 — EN — 11.02.2003 — 002.001 — 49
▼B
1.5.5.3. Alternative methods
If it can be shown that alternative technology (e.g. computer, electroni-
cally controlled range switch, etc.) can give equivalent accuracy, then
these alternatives may be used.
1.6.Verificationofthecalibration
Each normally used operating range shall be checked prior to each
analysis in accordance with the following procedure.
The calibration is checked by using a zero gas and a span gas whose
nominal value is more than 80 % of full scale of the measuring range.
If, for the two pointscons idered, the value found doesnot differ by
more than ± 4 % of full scale from the declared reference value, the
adjustment parameters may be modified. Should this not be the case, a
new calibration curve shall be established in accordance with section
1.5.4.
1.7.Efficiency testoftheNOxconverter
The efficiency of the converter used for the conversion of NO2into NO
is tested as given in sections 1.7.1 to 1.7.8 (Figure 1).
1.7.1. Test set-up
Using the test set-up as shown in Figure 1 (see also Appendix 1, section
1.4.3.5) and the procedure below, the efficiency of converterscan be
tested by means of an ozonator.1997L0068 — EN — 11.02.2003 — 002.001 — 50
▼B
Figure 1
SchematicofNO2converter efficiency device
1.7.2. Calibration
The CLD and the HCLD shall be calibrated in the most common oper-
ating range following the manufacturer's specifications using zero and
span gas (the NO content of which must amount to about 80 % of the
operating range and the NO2concentration of the gasmixture to les s
than 5 % of the NO concentration). The NOxanalyser must be in the
NO mode so that the span gas does not pass through the converter.
The indicated concentration hasto be recorded.
1.7.3. Calculation
The efficiency of the NOxconverter iscalculated asfollows :
Efficiency % ðÞ ¼ 1þa/C0b
c/C0d/C18/C19
/C2100
(a) NOxconcentration according to section 1.7.6;
(b) NOxconcentration according to section 1.7.7;
(c) NO concentration according to section 1.7.4;(d) NO concentration according to section 1.7.5.
1.7.4. Adding of oxygen
Via a T-fitting, oxygen or zero air isadded continuous ly to the gasflow
until the concentration indicated isabout 20 % les sthan the indicated
calibration concentration given in section 1.7.2. (The analyser is in the
NO mode.)
The indicated concentration (c) shall be recorded. The ozonator is kept
de-activated throughout the process.1997L0068 — EN — 11.02.2003 — 002.001 — 51
▼B
1.7.5. Activation of the ozonator
The ozonator isnow activated to generate enough ozone to bring the
NO concentration down to about 20 % (minimum 10 %) of the calibra-
tion concentration given in section 1.7.2. The indicated concentration
(d) shall be recorded. (The analyser is in the NO mode.)
1.7.6. NOxmode
The NO analyser is then switched to the NOxmode so that the gas
mixture (consisting of NO, NO2,O2and N2) now passes through the
converter. The indicated concentration (a) shall be recorded. (The
analyser is in the NOxmode.)
1.7.7. De-activation of the ozonator
The ozonator is now de-activated. The mixture of gases described in
section 1.7.6 passes through the converter into the detector. The indi-
cated concentration (b) shall be recorded. (The analyser is in the NOxmode.)
1.7.8. NO mode
Switched to NO mode with the ozonator de-activated, the flow of
oxygen or synthetic air is also shut off. The NOxreading of the analyser
shall not deviate by more than ± 5 % from the value measured
according to section 1.7.2. (The analyser is in the NO mode.)
1.7.9. Test interval
The efficiency of the converter must be tested prior to each calibration
of the NOxanalyser.
1.7.10. Efficiency requirement
The efficiency of the converter shall not be less than 90 %, but a higher
efficiency of 95 % iss trongly recommended.
Note:If, with the analyser in the most common range, the ozonator
cannot give a reduction from 80 % to 20 % according to section
1.7.5, then the highest range which will give the reduction shall
be used.
1.8.AdjustmentoftheFID
1.8.1. Optimization of the detector response
The HFID must be adjusted as specified by the instrument manufac-
turer. A propane in air span gas should be used to optimize the
response on the most common operating range.
With the fuel and air flow ratess et at the manufacturer'srecommenda-
tions, a 350 ± 75 ppm C span gas shall be introduced to the analyser.
The response at a given fuel flow shall be determined from the differ-
ence between the span gas response and the zero gas response. The fuel
flow shall be incrementally adjusted above and below the manufac-
turer's specification. The span and zero response at these fuel flows
shall be recorded. The difference between the span and zero response
shall be plotted and the fuel flow adjusted to the rich side of the curve.
1.8.2. Hydrocarbon response factors
The analyser shall be calibrated using propane in air and purified
synthetic air, according to section 1.5.
Response factors shall be determined when introducing an analyser into
service and after major service intervals. The response factor (Rf) for a
particular hydrocarbon species is the ratio of the FID C1 reading to the
gas concentration in the cylinder expressed by ppm C1.
The concentration of the test gas must be at a level to give a response
of approximately 80 % of full scale. The concentration must be known
to an accuracy of ± 2 % in reference to a gravimetric standard
expressed in volume. In addition, the gas cylinder must be pre-condi-
tioned for 24 hoursat a temperature of 298 K (25 ºC) ± 5 K.
The test gases to be used and the recommended relative response factor
rangesare asfollows :
— methane and purified synthetic air: 1,00 ≤Rf≤1,15
— propylene and purified synthetic air: 0,90 ≤Rf≤1,1
— toluene and purified synthetic air: 0,90 ≤Rf≤1,101997L0068 — EN — 11.02.2003 — 002.001 — 52
▼B
These values are relative to the response factor (Rf) of 1,00 for propane
and purified synthetic air.
1.8.3. Oxygen interference check
The oxygen interference check shall be determined when introducing an
analyser into service and after major service intervals.
The response factor is defined and shall be determined as described in
section 1.8.2. The test gas to be used and the recommended relative
response factor range are as follows:
— propane and nitrogen: 0,95 ≤Rf≤1,05
This value is relative to the response factor (Rf) of 1,00 for propane and
purified synthetic air.
The FID burner air oxygen concentration must be within ± 1 mole % of
the oxygen concentration of the burner air used in the latest oxygen
interference check. If the difference isgreater, the oxygen interference
must be checked and the analyser adjusted, if necessary.
1.9.Interference effectswithNDIRandCLDanalysers
Gases present in the exhaust other than the one being analysed can
interfere with the reading in several ways. Positive interference occurs
in NDIR instruments where the interfering gas gives the same effect as
the gas being measured, but to a lesser degree. Negative interference
occursin NDIR ins trumentsby the interfering gasbroadening the
absorption band of the measured gas, and in CLD instruments by the
interfering gasquenching the radiation. The interference checksin
sections 1.9.1 and 1.9.2 shall be performed prior to an analyser's initial
use and after major service intervals.
1.9.1. CO analyser interference check
Water and CO2can interfere with the CO analyser performance. There-
fore a CO2span gas having a concentration of 80 to 100 % of full scale
of the maximum operating range used during testing shall be bubbled
through water at room temperature and the analyser response recorded.
The analyser response must not be more than 1 % of full scale for
rangesequal to or above 300 ppm or more than 3 ppm for rangesbelow
300 ppm.
1.9.2. NOxanalyser quench checks
The two gases of concern for CLD (and HCLD) analysers are CO2and
water vapour. Quench responses of these gases are proportional to their
concentrations, and therefore require test techniques to determine the
quench at the highest expected concentrations experienced during
testing.
1.9.2.1. CO2quench check
AC O2span gas having a concentration of 80 to 100 % of full scale of
the maximum operating range shall be passed through the NDIR
analyser and the CO2value recorded asA. It s hall then be diluted
approximately 50 % with NO span gas and passed through the NDIR
and (H)CLD with the CO2and NO valuesrecorded asB and C, res pec-
tively. The CO2shall be shut off and only the NO span gas be passed
through the (H)CLD and the NO value recorded asD.
The quench shall be calculated as follows:
%C O 2quench ¼1/C0C/C2A ðÞ
D/C2A ðÞ /C0 D/C2B ðÞ/C18/C19/C20/C21
/C2100
and must not be greater than 3 % of full scale.
where:A: undiluted CO
2concentration measured with NDIR %
B: diluted CO2concentration measured with NDIR %
C: diluted NO concentration measured with CLD ppm
D: undiluted NO concentration measured with CLD ppm
1.9.2.2. Water quench check
Thischeck appliesto wet gasconcentration meas urementsonly. Calcu-
lation of water quench must consider dilution of the NO span gas with1997L0068 — EN — 11.02.2003 — 002.001 — 53
▼M1
▼M1
water vapour and scaling of water vapour concentration of the mixture
to that expected during testing. A NO span gas having a concentration
of 80 to 100 % of full scale to the normal operating range shall be
passed through the (H)CLD and the NO value recorded as D. The NO
gass hall then be bubbled through water at room temperature and
passed through the (H)CLD and the NO value recorded as C. The water
temperature shall be determined and recorded as F. The mixture's
saturation vapour pressure that corresponds to the bubbler water
temperature (F) shall be determined and recorded as G. The water
vapour concentration (in %) of the mixture shall be calculated as
follows:
and recorded asH. The expected diluted NO s pan gas(in water vapour)concentration shall be calculated as follows:
and recorded as De. For diesel exhaust, the maximum exhaust water
vapour concentration (in %) expected during testing shall be estimated,
under the assumption of a fuel atom H/C ration of 1,8 to 1, from the
maximum CO2concentration in the exhaust gas or from the undiluted
CO2span gas concentration (A, as measured in section 1.9.2.1) as
follows:
Hm=0,9×A
and recorded asHm.
The water quench shall be calculated as follows:
and must not be greater than 3 % of full scale.
De: expected diluted NO concentration (ppm)
C: diluted NO concentration (ppm)
Hm: maximum water vapour concentration (%)
H: actual water vapour concentration (%)
NB:It isimportant that the NO s pan gascontainsminimal NO2concentration for this check, since obsorption of NO2in water
hasnot been accounted for in the quench calculations .
1.10.Calibrationintervals
The analysers shall be calibrated according to section 1.5 at least every
three months or whenever a system repair or change is made that could
influence calibration.
2. CALIBRATION OF THE PARTICULATE MEASURING SYSTEM
2.1.Introduction
Each component shall be calibrated as often as necessary to fulfil the
accuracy requirementsof thiss tandard. The calibration method to be
used is described in this section for the components indicated in Annex
III, Appendix 1, section 1.5 and Annex V.
2.2.Flowmeasurement
The calibration of gas flow-meters or flow measurement instrumenta-
tion shall be traceable to national and/or international standards.
The maximum error of the measured value shall be within ± 2 % of
reading.
If the gasflow isdetermined by differential meas urement, the
maximum error of the difference shall be such that the accuracy of
GEDFis within ± 4 % (see also Annex V, section 1.2.1.1 EGA). It can1997L0068 — EN — 11.02.2003 — 002.001 — 54
▼B
▼B
be calculated by taking the root-mean-square of the errors of each
instrument.
2.3.Checkingthedilutionratio
When using particulate sampling systems without EGA (Annex V,
section 1.2.1.1), the dilution ratio shall be checked for each new engine
installation with the engine running and the use of either the CO2or
NOxconcentration measurements in the raw and dilute exhaust.
The measured dilution ratio shall be within ± 10 % of the calculated
dilution ratio from CO2or NOxconcentration measurement.
2.4.Checkingthepartialflowconditions
The range of the exhaust gas velocity and the pressure oscillations shall
be checked and adjusted according to the requirements of Annex V,
section 1.2.1.1, EP, if applicable.
2.5.Calibrationintervals
The flow measurement instrumentation shall be calibrated at least every
three months, or whenever a system change is made that could influ-
ence calibration.1997L0068 — EN — 11.02.2003 — 002.001 — 55
▼B
Appendix 3
1. DATA EVALUATION AND CALCULATIONS
1.1.Gaseousemissionsdataevaluation
For the evaluation of the gaseous emissions, the chart reading of the
last 60 seconds of each mode shall be averaged, and the average
concentrations(conc) of HC, CO, NOxand CO2if the carbon balance
method is used, during each mode shall be determined from the average
chart readingsand the corres ponding calibration data. A different type
of recording can be used if it ensures an equivalent data acquisition.
The average background concentrations(concd) may be determined
from the bag readingsof the dilution air or from the continous(non-
bag) background reading and the corresponding calibration data.
1.2.Particulate emissions
For the evaluation of the particulates, the total sample masses (MSAM,i)
or volumes(VSAM,i) through the filterss hall be recorded for each mode.
The filterss hall be returned to the weighing chamber and conditioned
for at least one hour, but not more than 80 hours, and then weighed.
The gross weight of the filters shall be recorded and the tare weight
(see section 3.1, Annex III) subtracted. The particulate mass (Mffor
single filter method; Mf,ifor the multiple filter method) isthe s um of
the particulate masses collected on the primary and back-up filters.
If background correction isto be applied, the dilution air mas s(MDIL)o r
volume (VDIL) through the filtersand the particulate mas s(Md) shall be
recorded. If more than one measurement was made, the quotient Md/
MDILor Md/VDILmust be calculated for each single measurement and
the valuesaveraged.
1.3.Calculationofthegaseousemissions
The finally reported test results shall be derived through the following
steps:
1.3.1. Determination of the exhaust gas flow
The exhaust gas flow rate (GEXHW,VEXHWor VEXHD) shall be determined
for each mode according to Annex III, Appendix 1, sections 1.2.1 to
1.2.3.
When using a full flow dilution system, the total dilute exhaust gas
flow rate (GTOTW,VTOTW) shall be determined for each mode according
to Annex III, Appendix 1, section 1.2.4.
1.3.2. Dry/wet correction
When applying GEXHW,VEXHW,GTOTWor VTOTW, the measured concentra-
tion shall be converted to a wet basis according to the following
formulae, if not already measured on a wet basis:
conc (wet) = kw× conc (dry)
For the raw exhaust gas:
kw;r;1¼1/C0FFH/C2GFUEL
GAIRD/C18/C19
/C0kw2
or:
kw;r;2¼1
1þ1;88/C20;005/C2% CO dry ½/C138 þ %C O 2dry½/C138 ðÞ/C18/C19
/C0kw2
For the diluted exhaust gas:
kw;e;1¼1/C01;88/C2CO2% wetðÞ
200/C18/C19
/C0kw11997L0068 — EN — 11.02.2003 — 002.001 — 56
▼B
or:
kw;e;2¼1/C0kw1
1þ1;88/C2CO2% dryðÞ
2000
BB@1
CCA
FFHmay be calculated by:
FFH¼1;969
1þGFUEL
GAIRW/C18/C19
For the dilution air:
kW,d=1−kW1
kW1¼1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
1000 þ1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
Hd¼6;22/C2Rd/C2pd
PB/C0Pd/C2Rd/C210/C02
For the intake air (if different from the dilution air):
kW,a=1−kW2
kW2¼1;608/C2Ha
1000 þ1;608/C2Ha ðÞ
Ha¼6;22/C2Ra/C2pa
pB/C0pa/C2Ra/C210/C02
where:
Ha: absolute humidity of the intake air, g water per kg dry air
Hd: absolute humidity of the dilution air, g water per kg dry air
Rd: relative humidity of the dilution air, %
Ra: relative humidity of the intake air, %
pd: saturation vapour pressure of the dilution air, kPa
pa: saturation vapour pressure of the intake air, kPa
pb: total barometric pressure, kPa.
1.3.3. Humidity correction for NOx
Asthe NOxemission depends on ambient air conditions, the NOxconcentration shall be corrected for ambient air temperature and
humidity by the factorsKHgiven in the following formula:
KH¼1
1þA/C2Ha/C010;71 ðÞ þ B/C2Ta/C0298 ðÞ
where:
A: 0,309 GFUEL/GAIRD− 0,0266
B: − 0,209 GFUEL/GAIRD+ 0,00954
T: temperaturesof the air in K
GFUEL
GAIRD¼Fuel air ratio dry air basis ðÞ
Ha: humidity of the intake air, g water per kg dry air:
Ha¼6;220/C2Ra/C2pa
pB/C0pa/C2Ra/C210/C021997L0068 — EN — 11.02.2003 — 002.001 — 57
▼B
Ra: relative humidity of the intake air, %
pa: saturation vapour pressure of the intake air, kPa
pb: total barometric pressure, kPa.
1.3.4. Calculation of emission mass flow rates
The emission mass flow rates for each mode shall be calculated as
follows:
(a) For the raw exhaust gas (1):
Gasmass= u × conc × GEXHW
or:
Gasmass= v × conc × VEXHD
or:
Gasmass= w × conc × VEXHW
(b) For the dilute exhaust gas (1):
Gasmass= u × concc×GTOTW
or:
Gasmass= w × concc×VTOTW
where:conc
cisthe background corrected concentration
concc= conc-concd× (1 − (1/DF))
DF = 13,4/(concCO2+ (concCO + concHC) × 10−4)
or:
DF = 13,4/concCO2.
The coefficients u — wet, v — dry, w — wet shall be used according
to the following table:
Gasu v w conc
NOx0,001587 0,002053 0,002053 ppm
CO 0,000966 0,00125 0,00125 ppmHC 0,000479 — 0,000619 ppm
CO
215,19 19,64 19,64 percent
The density of HC is based upon an average carbon to hydrogen ratio
of 1:1,85.1997L0068 — EN — 11.02.2003 — 002.001 — 58
(1) In the case of NOx, the NOxconcentration (NOxconc or NOxconcc) hasto be multiplied
by KHNOX(humidity correction factor for NOxquoted in the previouss ection 1.3.3) as
follows:
KHNOX× conc or KHNOX× concc
▼B
1.3.5. Calculation of the specific emissions
The specific emission (g/kWh) shall be calculated for all individual
componentsin the following way:
Individual gas ¼Xn
i¼1Gasmassi/C2WFi
Xn
i¼1Pi/C2WFi
where
Pi=Pm,i+PAE,i.
The weighting factorsand the number of modes(n) us ed in the above
calculation are according to Annex III, section 3.6.1.
1.4.Calculationoftheparticulateemission
The particulate emission shall be calculated in the following way:
1.4.1. Humidity correction factor for particulates
As the particulate emission of diesel engines depends on ambient air
conditions, the particulate mass flow rate shall be corrected for ambient
air humidity with the factor Kpgiven in the following formula:
Kp= 1/(1 + 0,0133 × (Ha− 10,71))
Ha: humidity of the intake air, grammesof water per kg dry air
Ha¼6;22/C2Ra/C2pa
pB/C0pa/C2Ra/C210/C02
Ra: relative humidity of the intake air, %
pa: saturation vapour pressure of the intake air, kPa
pb: total barometric pressure, kPa
1.4.2. Partial flow dilution system
The final reported test results of the particulate emission shall be
derived through the following steps. Since various types of dilution
rate control may be used, different calculation methods for equivalent
diluted exhaust gas mass flow rate GEDFor equivalent diluted exhaust
gasvolume flow rate VEDFapply. All calculations shall be based upon
the average valuesof the individual modes(i) during the s amplingperiod.
1.4.2.1. Isokinetic systems
G
EDFW,i=GEXHW,i×qi
or:
VEDFW,i=VEXHW,i×qi
qi¼GDILW ;iþGEXHW ;i/C2r/C0/C1
GEXHW ;i/C2r/C0/C1
or:
qi¼VDILW ;iþVEXHW ;i/C2r/C0/C1
VEXHW ;i/C2r/C0/C1
where r corresponds to the ratio of the cross sectional areas of the isoki-
netic probe Apand exhaust pipe AT:1997L0068 — EN — 11.02.2003 — 002.001 — 59
▼B
r¼Ap
AT
1.4.2.2. Systems with measurement of CO2or NOxconcentration
GEDFW,i=GEXHW,i×qi
or:
VEDFW,i=VEXHW,i×qi
qi¼Conc E;i/C0Conc A;i
Conc D;i/C0Conc A;i
where:
ConcE= wet concentration of the tracer gasin raw exhaus t
ConcD= wet concentration of the tracer gasin the diluted exhaus t
ConcA= wet concentration of the tracer gasin the dilution air
Concentrations measured on a dry basis shall be converted to a wet
basis according to section 1.3.2 of this Appendix.
1.4.2.3. Systems with CO2measurement and carbon balance method
GEDFW ;i¼206 ;6/C2GFUEL ;i
CO2D;i/C0CO2A;i
where:
CO2D=C O2concentration of the diluted exhaust
CO2A=C O2concentration of the dilution air
(concentrations in volume % on wet basis)This equation is based upon the carbon balance assumption (carbon
atomss upplied to the engine are emitted asCO
2) and derived through
the following steps:
GEDFW,i=GEXHW,i×qi
and:
qi¼206 ;6/C2GFUEL ;i
GEXHW ;i/C2CO2D;i/C0CO2A;i/C0/C1
1.4.2.4. Systems with flow measurement
GEDFW,i=GEXHW,i×qi
qi¼GTOTW ;i
GTOTW ;i/C0GDILW ;i/C0/C1
1.4.3. Full flow dilution system
The final reported test results of the particulate emission shall be
derived through the following steps.
All calculations shall be based upon the average values of the indivi-
dual modes(i) during the s ampling period.
GEDFW,i=GTOTW,i1997L0068 — EN — 11.02.2003 — 002.001 — 60
▼B
or:
VEDFW,i=VTOTW,i
1.4.4. Calculation of the particulate mass flow rate
The particulate mass flow rate shall be calculated as follows:
For the single filter method:
PTmass¼Mf
MSAM/C2GEDFWðÞaver
1000
or:
PTmass¼Mf
VSAM/C2VEDFWðÞaver
1000
where:
(GEDFW)aver,( VEDFW)aver,( MSAM)aver,( VSAM)averover the test cycle shall be
determined by summation of the average values of the individual modes
during the sampling period:
GEDFWðÞaver¼Xn
i¼1GEDFW ;i/C2WFi
VEDFWðÞaver¼Xn
i¼1VEDFW ;i/C2WFi
MSAM¼Xn
i¼1MSAM ;i
VSAM¼Xn
i¼1VSAM ;i
where i = 1, … n
For the multiple filter method:
PTmass ;i¼Mf;i
MSAM ;i/C2GEDFW ;i/C0/C1
1000
or:
PTmass ;i¼Mf;i
VSAM ;i/C2VEDFW ;i/C0/C1
1000
where i = 1, … n
The particulate mass flow rate may be background corrected as follows:For single filter method:
If more than one measurement is made, (Md/MDIL)o r( Md/VDIL) shall be
replaced with (Md/MDIL)averor (Md/VDIL)aver, respectively.1997L0068 — EN — 11.02.2003 — 002.001 — 61
▼M1
▼B
▼B
DF¼13;4
concCO 2þconcCO þconcHC ðÞ /C2 10/C04
or:
DF = 13,4/concCO2
For multiple filter method:
PTmass ;i¼Mf;i
MSAM ;i/C0Md
MDIL/C21/C01
DF/C18/C19 /C18/C19 /C20/C21
/C2GEDFW ;i
1000/C20/C21
or:
PTmass ;i¼Mf;i
VSAM ;i/C0Md
VDIL/C21/C01
DF/C18/C19 /C18/C19 /C20/C21
/C2VEDFW ;i
1000/C20/C21
If more than one measurement is made, (Md/MDIL)o r( Md/VDIL) shall be
replaced with (Md/MDIL)averor (Md/VDIL)aver, respectively.
DF¼13;4
concCO 2þconcCO þconcHC ðÞ /C2 10/C04
or:
DF = 13,4/concCO2
1.4.5. Calculation of the specific emissions
The specific emission of particulates PT (g/kWh) shall be calculated in
the following way (1):
For the single filter method:
PT¼PTmass
Xn
i¼1Pi/C2WFi
For the multiple filter method:
PT¼Xn
i¼1PTmass ;i/C2WFi
Xn
i¼1Pi/C2WFi
Pi=Pm,i+PAE,i
1.4.6. Effective weighting factor
For the single filter method, the effective weighting factor WFE,ifor
each mode shall be calculated in the following way:
WFE;i¼MSAM ;i/C2GEDFWðÞaver
MSAM/C2GEDFW ;i/C0/C11997L0068 — EN — 11.02.2003 — 002.001 — 62
(1) The particulate mass flow rate PTmasshasto be multiplied by Kp(humidity correction
factor for particulatesquoted in s ection 1.4.1).
▼B
or:
WFE;i¼VSAM ;i/C2VEDFWðÞaver
VSAM/C2VEDFW ;i/C0/C1
where i = l, … n.
The value of the effective weighting factorss hall be within ± 0,005
(absolute value) of the weighting factors listed in Annex III, section
3.6.1.1997L0068 — EN — 11.02.2003 — 002.001 — 63
▼M2
ANNEX IV
TESTPROCEDUREFORSPARKIGNITIONENGINES
1. INTRODUCTION
1.1. This Annex describes the method of determining emissions of gaseous
pollutantsfrom the enginesto be tes ted.
1.2. The test shall be carried out with the engine mounted on a test bench
and connected to a dynamometer.
2. TEST CONDITIONS2.1.Enginetestconditions
The absolute temperature (T
a) of the engine air at the inlet to the
engine, expressed in Kelvin, and the dry atmospheric pressure (ps),
expressed in kPa, shall be measured and the parameter fashall be deter-
mined according to the following provisions:
fa¼99
ps/C18/C191;2
/C2Ta
298/C18/C190;6
2.1.1. Test validity
For a test to be recognised as valid, the parameter fashall be such that:
0,93≤fa≤1,07
2.1.2. Engines with charge air-cooling
The temperature of the cooling medium and the temperature of the
charge air have to be recorded.
2.2.Engineairinletsystem
The test engine shall be equipped with an air inlet system presenting an
air inlet restriction within 10 % of the upper limit specified by the
manufacturer for a new air cleaner at the engine operating conditions,
as specified by the manufacturer, which result in maximum air flow in
the respective engine application.
For small spark ignition engines (< 1 000 cm3displacement) a system
representative of the installed engine shall be used.
2.3.Engineexhaustsystem
The test engine shall be equipped with an exhaust system presenting an
exhaust back pressure within 10 % of the upper limit specified by the
manufacturer for the engine operating conditionswhich res ult in the
maximum declared power in the respective engine application.
For small spark ignition engines (< 1 000 cm3displacement) a system
representative of the installed engine shall be used.
2.4.Coolingsystem
An engine cooling system with sufficient capacity to maintain the
engine at normal operating temperaturespres cribed by the manufacturer
shall be used. This provision shall apply to units which have to be
detached in order to measure the power, such as with a blower where
the blower (cooling) fan has to be disassembled to get access to the
crankshaft.
2.5.Lubricatingoil
Lubricating oil that meetsthe engine manufacturer'ss pecificationsfor a
particular engine and intended usage shall be used. Manufacturers must
use engine lubricants representative of commercially available engine
lubricants.
The specifications of the lubricating oil used for the test shall be
recorded at section 1.2 of Annex VII, Appendix 2, for SI engines and
presented with the results of the test.1997L0068 — EN — 11.02.2003 — 002.001 — 64
▼M2
2.6.Adjustablecarburettors
Engines with limited adjustable carburettors shall be tested at both
extremesof the adjus tment.
2.7.Testfuel
The fuel shall be the reference fuel specified in Annex V.
The octane number and the density of the reference fuel used for test
shall be recorded at section 1.1.1 of Annex VII, Appendix 2, for SI
engines.
For two-stroke engines, the fuel/oil mixture ratio must be the ratio
which shall be recommended by the manufacturer. The percentage of
oil in the fuel/lubricant mixture feeding the two-stroke engines and the
resulting density of the fuel shall be recorded at section 1.1.4 of Annex
VII, Appendix 2, for SI engines.
2.8.Determinationofdynamometersettings
Emissions measurements shall be based on uncorrected brake power.
Auxiliaries necessary only for the operation of the machine and which
may be mounted on the engine shall be removed for the test. Where
auxiliaries have not been removed, the power absorbed by them shall
be determined in order to calculate the dynamometer settings except
for engineswhere s uch auxiliariesform an integral part of the engine
(e.g. cooling fansfor air cooled engines ).
The settings of inlet restriction and exhaust pipe backpressure shall be
adjusted, for engines where it shall be possible to perform such an
adjustment, to the manufacturer's upper limits, in accordance with
sections 2.2 and 2.3. The maximum torque values at the specified test
speeds shall be determined by experimentation in order to calculate the
torque values for the specified test modes. For engines which are not
designed to operate over a speed range on a full load torque curve, the
maximum torque at the test speeds shall be declared by the manufac-turer. The engine setting for each test mode shall be calculated using
the formula:
S¼P
MþPAE ðÞ /C2L
100/C18/C19
/C0PAE
where:
S isthe dynamometer s etting [kW],
PMis the maximum observed or declared power at the test speed under
the test conditions (see Appendix 2 of Annex VII) [kW],
PAEisthe declared total power abs orbed by any auxiliary fitted for the
test [kW] and not required by Appendix 3 of Annex VII,
L is the percent torque specified for the test mode.
If the ratio
PAE
PM/C210;03
the value of PAEmay be verified by the technical authority granting
type-approval.
3. TEST RUN3.1.Installationofthemeasuringequipment
The instrumentation and sampling probes shall be installed as required.
When using a full flow dilution system for exhaust gas dilution, the
tailpipe shall be connected to the system.
3.2.Startingthedilutionsystemandengine
The dilution system and the engine shall be started and warmed up until
all temperatures and pressures have stabilised at full load and rated
speed (section 3.5.2).
3.3.Adjustmentofthedilutionratio
The total dilution ratio shall not be less than four.1997L0068 — EN — 11.02.2003 — 002.001 — 65
▼M2
For CO2or NOxconcentration controlled systems, the CO2or NOxcontent of the dilution air must be measured at the beginning and at
the end of each test. The pre- and post-test background CO2or NOxconcentration measurements of the dilution air must be within 100ppm or 5 ppm of each other, respectively.
When using a dilute exhaust gas analysis system, the relevant back-
ground concentrations shall be determined by sampling dilution air
into a sampling bag over the complete test sequence.
Continuous(non-bag) background concentration may be taken at the
minimum of three points, at the beginning, at the end, and a point
near the middle of the cycle and averaged. At the manufacturer's
request background measurements may be omitted.
3.4.Checkingtheanalysers
The emission analysers shall be set at zero and spanned.
3.5.Testcycle
3.5.1. Specification (c) of machinery according to section 1A(iii) of Annex I.
The following test cycles shall be followed in dynamometer operation
on the test engine according to the given type of machinery:
cycle D (
1): engines with constant speed and intermittent load such as
generating sets;
cycle G1: non-hand-held intermediate speed applications;cycle G2: non-hand-held rated speed applications;
cycle G3: hand-held applications.
3.5.1.1. Test modes and weighting factors
Cycle D
Mode number 12345
Engine speed Rated speed IntermediateLow-
idle
speed
Load (1) % 100 75 50 25 10
Weighting
factor0,05 0,25 0,3 0,3 0,1
Cycle G1
Mode number 1 2 3 4 5 6
Engine speed Rated speed Intermediate SpeedLow-
idle
speed
Load % 100 75 50 25 10 0
Weighting
factor0,09 0,2 0,29 0,3 0,07 0,05
Cycle G2
Mode number 12345 6
Engine speed Rated speed Intermediate SpeedLow-
idle
speed
Load % 100 75 50 25 10 01997L0068 — EN — 11.02.2003 — 002.001 — 66
(1) Identical with D2 cycle of the ISO 8168-4: 1996(E) standard.
▼M2
Cycle G2
Mode number 12345 6
Engine speed Rated speed Intermediate SpeedLow-
idle
speed
Weighting
factor0,09 0,2 0,29 0,3 0,07 0,05
Cycle G3
Mode number 1 2
Engine speed Rated speed Intermediate SpeedLow-
idle
speed
Load % 100 0
Weighting
factor0,8-
5 (*)0,15 (*)
(1) The load figuresare percentage valuesof the torque corres ponding to the prime power rating defined
asthe maximum power available during a variable power s equence, which may be run for an unlim-ited number of hours per year, between stated maintenance intervals and under the stated ambient
conditions, the maintenance being carried out as prescribed by the manufacturer. For a better illustra-
tion of the prime power definition, see figure 2 of ISO 8528-1: 1993(E) standard.
(*) For stage I, 0,90 and 0,10 may be used instead of 0,85 and 0,15 respectively.
3.5.1.2. Choosing an appropriate test cycle
If the primary end use of an engine model is known then the test cycle
may be chosen based on the examples given in section 3.5.1.3. If the
primary end use of an engine is uncertain then the appropriate test cycle
should be chosen based upon the engine specification.
3.5.1.3. Examples (the list is not exhaustive)
Typical examplesare for:
cycle D:
generating sets with intermittent load including generating sets on board
ships and trains (not for propulsion), refrigerating units, welding sets;
gas compressors;
cycle G1:
front or rear enginesriding lawn mowers ;
golf carts;lawn sweepers;pedestrian-controlled rotary or cylinder lawn mowers;snow-removal equipment;waste disposers;
cycle G2:
portable generators, pumps, welders and air compressors;
may also include lawn and garden equipment, which operate at engine
rated speed;
cycle G3:
blowers;
chain saws;hedge trimmers;portable saw mills;rotary tillers;sprayers;
string trimmers;1997L0068 — EN — 11.02.2003 — 002.001 — 67
▼M2
vacuum equipment.
3.5.2. Conditioning of the engine
Warming up of the engine and the system shall be at maximum speed
and torque in order to stabilise the engine parameters according to the
recommendationsof the manufacturer.
Note:The conditioning period should also prevent the influence of
deposits from a former test in the exhaust system. There is also
a required period of stabilisation between test points which has
been included to minimise point to point influences.
3.5.3. Test sequence
Test cycles G1, G2 or G3 shall be performed in ascending order of
mode number of the cycle in question. Each mode sampling time shall
be at least 180 s. The exhaust emission concentration values shall be
measured and recorded for the last 120 s of the respective sampling
time. For each measuring point, the mode length shall be of sufficient
duration to achieve thermal stability of the engine prior to the start of
sampling. The mode length shall be recorded and reported.
(a) For engines tested with the dynamometer speed control test config-
uration: During each mode of the test cycle after the initial
transition period, the specified speed shall be held to within ± 1 %
of rated speed or ± 3 min-1whichever isgreater except for low idle
which shall be within the tolerances declared by the manufacturer.
The specified torque shall be held so that the average over the
period during which the measurements are being taken is within
± 2 % of the maximum torque at the test speed.
(b) For engines tested with the dynamometer load control test config-
uration: During each mode of the test cycle after the initial
transition period, the specified speed shall be within ± 2 % of rated
speed or ± 3 min-1whichever is greater, but shall in any case be
held within ± 5 %, except for low idle which shall be within the
tolerancesdeclared by the manufacturer.
During each mode of the test cycle where the prescribed torque is
50 % or greater of the maximum torque at the test speed the speci-
fied average torque over the data acquisition period shall be held
within ± 5 % of the prescribed torque. During modes of the test
cycle where the prescribed torque is less than 50 % of the
maximum torque at the test speed the specified average torque
over the data acquisition period shall be held within ± 10 % of the
prescribed torque or ± 0,5 Nm whichever is greater.
3.5.4. Analyser response
The output of the analysers shall be recorded on a strip chart recorder
or measured with an equivalent data acquisition system with the
exhaust gas flowing through the analysers at least during the last 180 s
of each mode. If bag sampling is applied for the diluted CO and CO2measurement (see Appendix 1, section 1.4.4), a sample shall be baggedduring the last 180 s of each mode, and the bag sample analysed and
recorded.
3.5.5. Engine conditions
The engine speed and load, intake air temperature and fuel flow shall
be measured for each mode once the engine has been stabilised. Any
additional data required for calculation shall be recorded (see Appendix
3, sections 1.1 and 1.2).
3.6.Recheckingtheanalysers
After the emission test a zero gas and the same span gas shall be used
for re-checking. The test shall be considered acceptable if the difference
between the two measuring results is less than 2 %.1997L0068 — EN — 11.02.2003 — 002.001 — 68
▼M2
Appendix 1
1. MEASUREMENT AND SAMPLING PROCEDURES
Gaseous components emitted by the engine submitted for testing shall
be measured by the methods described in Annex VI. The methods of
Annex VI describe the recommended analytical systems for the gaseous
emissions (section 1.1).
1.1.Dynamometerspecification
An engine dynamometer with adequate characteristics to perform the
test cycles described in Annex IV, section 3.5.1 shall be used. The
instrumentation for torque and speed measurement shall allow the
measurement of the shaft power within the given limits. Additional
calculations may be necessary.
The accuracy of the measuring equipment must be such that the
maximum tolerancesof the figuresgiven in s ection 1.3 are not
exceeded.
1.2.Fuelflowandtotaldilutedflow
Fuel flow meters with the accuracy defined in section 1.3 shall be used
to measure the fuel flow that will be used to calculate emissions
(Appendix 3). When using a full flow dilution system, the total flow
of the dilute exhaust (GTOTW) shall be measured with a PDP or CFV —
Annex VI, section 1.2.1.2. The accuracy shall conform to the provisions
of Annex III, Appendix 2, section 2.2.
1.3.Accuracy
The calibration of all measuring instruments shall be traceable to
national (international) standards and comply with the requirements
given in tables2 and 3.
Table 2 — Permissible deviations of instruments for engine related
parameters
No Item Permissible deviation
1 Engine speed ± 2 % of the reading or
± 1 % of engine'smax
value whichever islarger
2 Torque ± 2 % of the reading or
± 1 % of engine'smax
value whichever islarger
3 Fuel consumption (a) ± 2 % of engine'smax
value
4 Air consumption (a) ± 2 % of the reading or
± 1 % of engine'smax
value whichever islarger
(a) The calculations of the exhaust emissions as described in this Directive are, in
some cases, based on different measurement and/or calculation methods.Because of limited total tolerances for the exhaust emission calculation, theallowable values for some items, used in the appropriate equations, must be
smaller than the allowed tolerances given in ISO 3046-3.
Table 3 — Permissible deviations of instruments for other essential
parameters
No Item Permissible deviation
1 Temperatures ≤600 K ± 2 K absolute
2 Temperatures ≥600 K ± 1 % of reading1997L0068 — EN — 11.02.2003 — 002.001 — 69
▼M2
No Item Permissible deviation
3 Exhaust gas pressure ± 0,2 kPa absolute
4 Inlet manifold depres-
sions± 0,05 kPa absolute
5 Atmospheric pressure ± 0,1 kPa absolute
6 Other pressures ± 0,1 kPa absolute7 Relative humidity ± 3 % absolute
8 Absolute humidity ± 5 % of reading
9 Dilution air flow ± 2 % of reading
10 Diluted exhaust gas flow ± 2 % of reading
1.4.Determinationofthegaseouscomponents
1.4.1. General analyser specifications
The analysers shall have a measuring range appropriate for the accuracy
required for measuring the concentrations of the exhaust gas compo-
nents (section 1.4.1.1). It is recommended that the analysers be
operated such that the measured concentration falls between 15 % and
100 % of full scale.
If the full scale value is 155 ppm (or ppm C) or less or if read-out
systems (computers, data loggers) that provide sufficient accuracy and
resolution below 15 % of full scale are used concentrations below
15 % of full scale are also acceptable. In this case, additional calibra-
tionsare to be made to ens ure the accuracy of the calibration curves—
Appendix 2, section 1.5.5.2, of this Annex.
The electromagnetic compatibility (EMC) of the equipment shall be on
a level as to minimise additional errors.
1.4.1.1. Accuracy
The analyser shall not deviate from the nominal calibration point by
more than ± 2 % of the reading over the whole measurement range
except zero, and ± 0,3 % of full scale at zero. The accuracy shall be
determined according to the calibration requirementslaid down in
section 1.3.
1.4.1.2. Repeatability
The repeatability, shall be such that 2,5 times the standard deviation of
10 repetitive responses to a given calibration or span gas is not greater
than ± 1 % of full scale concentration for each range used above 100
ppm (or ppmC) or ± 2 % of each range used below 100 ppm (or
ppmC).
1.4.1.3. Noise
The analyser peak-to-peak response to zero and calibration or span
gases over any 10-s period shall not exceed 2 % of full scale on all
rangesus ed.
1.4.1.4. Zero drift
Zero response is defined as the mean response, including noise, to a
zero gas during a 30-s time interval. The drift of the zero response
during a one-hour period shall be less than 2 % of full scale on the
lowest range used.
1.4.1.5. Span drift
Span response is defined as the mean response, including noise, to a
span gas during a 30-s time interval. The drift of the span response
during a one-hour period shall be less than 2 % of full scale on the
lowest range used.1997L0068 — EN — 11.02.2003 — 002.001 — 70
▼M2
1.4.2. Gas drying
Exhaust gases may be measured wet or dry. Any gas-drying device, if
used, must have a minimal effect on the concentration of the measured
gases. Chemical dryers are not an acceptable method of removing water
from the sample.
1.4.3. Analysers
Sections 1.4.3.1 to 1.4.3.5 describe the measurement principles to be
used. A detailed description of the measurement systems is given in
Annex VI.
The gases to be measured shall be analysed with the following instru-
ments. For non-linear analysers, the use of linearising circuits is
permitted.
1.4.3.1. Carbon m onoxide (CO) analysis
The carbon monoxide analyser shall be of the non-dispersive infrared
(NDIR) absorption type.
1.4.3.2. Carbon dioxide (CO2)a n a l y si s
The carbon dioxide analyser shall be of the non-dispersive infrared
(NDIR) absorption type.
1.4.3.3. Oxygen (O2)a n a l y si s
Oxygen analysers shall be of the paramagnetic detector (PMD), zirco-
nium dioxide (ZRDO) or electrochemical sensor (ECS) types.
Note:Zirconium dioxide sensors are not recommended when HC and
CO concentrations are high such as for lean burn spark ignited
engines. Electrochemical sensors shall be compensated for CO2and NOXinterference.
1.4.3.4. Hydrocarbon (HC) analysis
For direct gas sampling the hydrocarbon analyser shall be of the heated
flame ionisation detector (HFID) type with detector, valves, pipework,
etc., heated so as to maintain a gas temperature of 463 K ± 10 K
(190 ºC ± 10 ºC).
For diluted gas sampling the hydrocarbon analyser shall be either the
heated flame ionisation detector (HFID) type or the flame ionisation
detector (FID) type.
1.4.3.5. Oxidesof nitrogen (NOx)a n a l y si s
The oxides of nitrogen analyser shall be of the chemiluminescent
detector (CLD) or heated chemiluminescent detector (HCLD) type
with a NO2/NO converter, if measured on a dry basis. If measured on
a wet basis, a HCLD with converter maintained above 328 K (55 ºC)
shall be used, provided the water quench check (Annex III, Appendix
2, section 1.9.2.2) is satisfied. For both CLD and HCLD, the sampling
path shall be maintained at a wall temperature of 328 K to 473 K (55 ºC
to 200 ºC) up to the converter for dry measurement, and up to the
analyser for wet measurement.
1.4.4. Sampling for gaseous emissions
If the composition of the exhaust gas is influenced by any exhaust after-
treatment system, the exhaust sample shall be taken downstream of this
device.
The exhaust sampling probe should be in a high pressure side of the
muffler, but as far from the exhaust port as possible. To ensurecomplete mixing of the engine exhaust before sample extraction, a
mixing chamber may be optionally inserted between the muffler outlet
and the sample probe. The internal volume of the mixing chamber must
be not less than 10 times the cylinder displacement of the engine under
test and should be roughly equal dimensions in height, width and depth,
being similar to a cube. The mixing chamber size should be kept as
small as practicable and should be coupled as close as possible to the
engine. The exhaust line leaving the mixing chamber of muffler should
extend at least 610 mm beyond the sample probe location and be of
sufficient size to minimise back pressure. The temperature of the inner
surface of the mixing chamber must be maintained above the dew point
of the exhaust gases and a minimum temperature of 338
oK (65 ºC) is
recommended.1997L0068 — EN — 11.02.2003 — 002.001 — 71
▼M2
All componentsmay optionally be meas ured directly in the dilution
tunnel, or by sampling into a bag and subsequent measurement of the
concentration in the sampling bag.1997L0068 — EN — 11.02.2003 — 002.001 — 72
▼M2
Appendix 2
1. CALIBRATION OF THE ANALYTICAL INSTRUMENTS
1.1.Introduction
Each analyser shall be calibrated as often as necessary to fulfil the
accuracy requirementsof thiss tandard. The calibration method that
shall be used is described in this paragraph for the analysers indicated
in Appendix 1, section 1.4.3.
1.2.Calibrationgases
The shelf life of all calibration gases must be respected.The expiry date of the calibration gases stated by the manufacturer
shall be recorded.
1.2.1 Pure gases
The required purity of the gases is defined by the contamination limits
given below. The following gases must be available for operation:
— purified nitrogen (contamination ≤1 ppm C, ≤1 ppm CO,
≤400 ppm CO
2,≤0,1 ppm NO),
— purified oxygen (purity > 99,5 Vol.- % O2),
— hydrogen-helium mixture (40 ± 2 % hydrogen, balance helium);
contamination ≤1 ppm C, ≤400 ppm CO2,
— purified synthetic air (contamination ≤1 ppm C, ≤1 ppm CO,
≤400 ppm CO2,≤0,1 ppm NO (oxygen content between 18 %
and 21 % vol).
1.2.2 Calibration and span gases
Mixture of gases having the following chemical compositions shall be
available:
—C3H8and purified synthetic air (see section 1.2.1),
— CO and purified nitrogen,— and purified nitrogen (the amount of NO
2contained in thiscalibra-
tion gasmus t not exceed 5 % of the NO content),
—C O2and purified nitrogen,
—C H4and purified synthetic air,
—C2H6and purified synthetic air.
Note:Other gascombinationsare allowed provided the gas esdo not
react with one another.
The true concentration of a calibration and span gas shall be within
± 2 % of the nominal value. All concentrationsof calibration gass hall
be given on a volume basis (volume percent or volume ppm).
The gases used for calibration and span may also be obtained by
means of precision blending devices (gas dividers), diluting with puri-
fied N2or with purified synthetic air. The accuracy of the mixing
device must be such that the concentration of the diluted calibration
gases is accurate to within ± 1,5 %. This accuracy implies that
primary gases used for blending must be known to an accuracy of at
least ± 1 %, traceable to national or international gas standards. The
verification shall be performed at between 15 % and 50 % of full scale
for each calibration incorporating a blending device.
Optionally, the blending device may be checked with an instrument,
which by nature is linear, e.g. using NO gas with a CLD. The spanvalue of the instrument shall be adjusted with the span gas directly
connected to the instrument. The blending device shall be checked at
the used settings and the nominal value shall be compared to the
measured concentration of the instrument. This difference shall in
each point be within ± 0,5 % of the nominal value.1997L0068 — EN — 11.02.2003 — 002.001 — 73
▼M2
1.2.3 Oxygen interference check
Oxygen interference check gases shall contain propane with 350 ppm
C ± 75 ppm C hydrocarbon. The concentration value shall be deter-
mined to calibration gastolerancesby chromatographic analys isof
total hydrocarbonsplusimpuritiesor by dynamic blending. Nitrogen
shall be the predominant diluent with the balance oxygen. Blend
required for gasoline-fuelled engine testing is as follows:
O2interference concentration Balance
10 (9 to 11) Nitrogen
5 (4 to 6) Nitrogen0 (0 to 1) Nitrogen.
1.3.Operatingprocedureforanalysersandsamplingsystem
The operating procedure for analysers shall follow the start-up and
operating instructions of the instrument manufacturer. The minimum
requirements given in sections 1.4 to 1.9 shall be included. For labora-
tory instruments such as GC and high performance liquid
chromatography (HPLC) only section 1.5.4 shall apply.
1.4.Leakagetest
A system leakage test shall be performed. The probe shall be discon-
nected from the exhaust system and the end plugged. The analyser
pump shall be switched on. After an initial stabilisation period all
flow meters should read zero. If not, the sampling lines shall be
checked and the fault corrected.
The maximum allowable leakage rate on the vacuum side shall be
0,5 % of the in-use flow rate for the portion of the system being
checked. The analyser flows and bypass flows may be used to estimate
the in-use flow rates.
Alternatively, the system may be evacuated to a pressure of at least 20
kPa vacuum (80 kPa absolute). After an initial stabilisation period the
pressure increase δp (kPa/min) in the system shall not exceed:
δp = p/V
syst× 0,005 × fr
Where:V
syst= system volume [l]
fr = system flow rate [l/min]
Another method isthe introduction of a concentration s tep change at
the beginning of the sampling line by switching from zero to span gas.
If after an adequate period of time the reading shows a lower concen-
tration compared to the introduced concentration, thispointsto
calibration or leakage problems.
1.5.Calibrationprocedure
1.5.1 Instrument assembly
The instrument assembly shall be calibrated and calibration curves
checked against standard gases. The same gas flow rates shall be
used as when sampling exhaust gas.
1.5.2. Warming-up time
The warming-up time should be according to the recommendations of
the manufacturer. If not specified, a minimum of two hours is recom-
mended for warming-up the analysers.
1.5.3. NDIR and HFID analyser
The NDIR analyser shall be tuned, as necessary, and the combustion
flame of the HFID analyser shall be optimised (section 1.9.1).
1.5.4. GC and HPCL
Both instruments shall be calibrated according to good laboratory
practice and the recommendationsof the manufacturer.1997L0068 — EN — 11.02.2003 — 002.001 — 74
▼M2
1.5.5. Establishment of the calibration curves
1.5.5.1. General guidelines
(a) Each normally used operating range shall be calibrated.
(b) Using purified synthetic air (or nitrogen), the CO, CO2,N Oxand
HC analysers shall be set at zero.
(c) The appropriate calibration gases shall be introduced to the analy-
sers, the values recorded, and the calibration curves established.
(d) For all instrument ranges except for the lowest range, the calibra-
tion curve shall be established by at least 10 calibration points
(excluding zero) equally spaced. For the lowest range of the
instrument, the calibration curve shall be established by at least
10 calibration points (excluding zero) spaced so that half of the
calibration pointsare placed below 15 % of the analys er'sfull
scale and the rest are placed above 15 % of full scale. For all
ranges the highest nominal concentration must be equal to or
higher than 90 % of full scale.
(e) The calibration curve shall be calculated by the method of least
squares. A best-fit linear or non-linear equation may be used.
(f) The calibration points must not differ from the least-squares best-
fit line by more than ± 2 % of reading or ± 0,3 % of full scale
whichever islarger.
(g) The zero setting shall be rechecked and the calibration procedure
repeated, if necessary.
1.5.5.2. Alternative methods
If it can be shown that alternative technology (e.g. computer, electro-
nically controlled range switch, etc.) can give equivalent accuracy,
then these alternatives may be used.
1.6.Verificationofthecalibration
Each normally used operating range shall be checked prior to each
analysis in accordance with the following procedure.
The calibration is checked by using a zero gas and a span gas whose
nominal value is more than 80 % of full scale of the measuring range.
If, for the two pointscons idered, the value found doesnot differ by
more than ± 4 % of full scale from the declared reference value, the
adjustment parameters may be modified. Should this not be the case,
the span gas shall be verified or a new calibration curve shall be estab-
lished in accordance with section 1.5.5.1.
1.7.Calibrationoftracer gasanalyserforexhaustflowmeasurement
The analyser for measurement of the tracer gas concentration shall be
calibrated using the standard gas.
The calibration curve shall be established by at least 10 calibration
points (excluding zero) spaced so that half of the calibration points
are placed between 4 % to 20 % of the analyser's full scale and the
rest are in between 20 % and 100 % of the full scale. The calibration
curve shall be calculated by the method of least squares.
The calibration curve must not differ by more than ± 1 % of the full
scale from the nominal value of each calibration point, in the range
from 20 % to 100 % of the full scale. It also must not differ by more
than ± 2 % of reading from the nominal value in the range from 4 %
to 20 % of the full scale. The analyser shall be set at zero and spanned
prior to the test run using a zero gas and a span gas whose nominal
value is more than 80 % of the analyser full scale.
1.8.Efficiency testoftheNOxconverter
The efficiency of the converter used for the conversion of NO2into
NO is tested as given in sections 1.8.1 to 1.8.8 (figure 1 of Annex
III, Appendix 2).
1.8.1. Test set-up
Using the test set-up as shown in figure 1 of Annex III and the proce-
dure below, the efficiency of converterscan be tes ted by meansof an
ozonator.1997L0068 — EN — 11.02.2003 — 002.001 — 75
▼M2
1.8.2. Calibration
The CLD and the HCLD shall be calibrated in the most common oper-
ating range following the manufacturer's specifications using zero and
span gas (the NO content of which must amount to about 80 % of the
operating range and the NO2concentration of the gasmixture to les s
than 5 % of the NO concentration). The NOxanalyser must be in the
NO mode so that the span gas does not pass through the converter.
The indicated concentration hasto be recorded.
1.8.3. Calculation
The efficiency of the NOx, converter iscalculated asfollows :
Efficiency ð%Þ¼1þa/C0b
c/C0d/C18/C19
/C2100
Where:
a=N Oxconcentration according to section 1.8.6
b=N Oxconcentration according to section 1.8.7
c = NO concentration according to section 1.8.4d = NO concentration according to section 1.8.5.
1.8.4. Adding of oxygen
Via a T-fitting, oxygen or zero air isadded continuous ly to the gas
flow until the concentration indicated isabout 20 % les sthan the indi-
cated calibration concentration given in section 1.8.2. (The analyser is
in the NO mode.)
The indicated concentration (c) shall be recorded. The ozonator is kept
deactivated throughout the process.
1.8.5 Activation of the ozonator
The ozonator isnow activated to generate enough ozone to bring the
NO concentration down to about 20 % (minimum 10 %) of the cali-
bration concentration given in section 1.8.2. The indicated
concentration (d) shall be recorded. (The analyser is in the NO mode.)
1.8.6 NO
xmode
The NO analyser is then switched to the NOxmode so that the gas
mixture (consisting of NO, NO2,O2and N2) now passes through the
converter. The indicated concentration (a) shall be recorded. (The
analyser is in the NOxmode.)
1.8.7. Deactivation of the ozonator
The ozonator is now deactivated. The mixture of gases described in
section 1.8.6 passes through the converter into the detector. The indi-
cated concentration (b) shall be recorded. (The analyser is in the NOxmode.)
1.8.8. NO mode
Switched to NO mode with the ozonator deactivated, the flow of
oxygen or synthetic air is also shut off. The NOxreading of the
analyser shall not deviate by more than ± 5 % from the value
measured according to section 1.8.2. (The analyser is in the NO
mode.)
1.8.9. Test interval
The efficiency of the converter must be checked monthly.
1.8.10. Efficiency requirement
The efficiency of the converter shall not be less than 90 %, but a
higher efficiency of 95 % iss trongly recommended.
Note:If, with the analyser in the most common range, the ozonator
cannot give a reduction from 80 % to 20 % according to section
1.8.5, then the highest range which will give the reduction shall
be used.1997L0068 — EN — 11.02.2003 — 002.001 — 76
▼M2
1.9.AdjustmentoftheFID
1.9.1. Optimisation of the detector response
The HFID must be adjusted as specified by the instrument manufac-
turer. A propane in air span gas should be used to optimise the
response on the most common operating range.
With the fuel and airflow ratess et at the manufacturer'srecommenda-
tions, a 350 ± 75 ppm C span gas shall be introduced to the analyser.
The response at a given fuel flow shall be determined from the differ-
ence between the span gas response and the zero gas response. The
fuel flow shall be incrementally adjusted above and below the manu-
facturer's specification. The span and zero response at these fuel flows
shall be recorded. The difference between the span and zero response
shall be plotted and the fuel flow adjusted to the rich side of the curve.
This is the initial flow rate setting, which may need further optimisa-
tion depending on the results of the hydrocarbon response factor and
the oxygen interference check according to sections 1.9.2 and 1.9.3.
If the oxygen interference or the hydrocarbon response factors do not
meet the following specifications, the airflow shall be incrementally
adjusted above and below the manufacturer's specifications, sections
1.9.2 and 1.9.3 should be repeated for each flow.
1.9.2. Hydrocarbon response factors
The analyser shall be calibrated using propane in air and purified
synthetic air, according to section 1.5.
Response factors shall be determined when introducing an analyser
into service and after major service intervals. The response factor
(Rf) for a particular hydrocarbon species is the ratio of the FID C1
reading to the gas concentration in the cylinder expressed by ppm C1.
The concentration of the test gas must be at a level to give a response
of approximately 80 % of full scale. The concentration must be known
to an accuracy of ± 2 % in reference to a gravimetric standard
expressed in volume. In addition, the gas cylinder must be precondi-
tioned for 24 hoursat a temperature of 298 K (25 ºC) ± 5 K.
The test gases to be used and the recommended relative response
factor rangesare asfollows :
— methane and purified synthetic air: 1,00 ≤Rf≤1,15
— propylene and purified synthetic air: 0,90 ≤Rf≤1,1
— toluene and purified synthetic air: 0,90 ≤Rf≤1,10.
These values are relative to the response factor (Rf) of 1,00 for
propane and purified synthetic air.
1.9.3. Oxygen interference check
The oxygen interference check shall be determined when introducing
an analyser into service and after major service intervals. A range
shall be chosen where the oxygen interference check gases will fall
in the upper 50 %. The test shall be conducted with the oven tempera-
ture set as required. The oxygen interference gases are specified in
section 1.2.3.
(a) The analyser shall be zeroed.
(b) The analyser shall be spanned with the 0 % oxygen blend for
gasoline fuelled engines.
(c) The zero response shall be rechecked. If it has changed more than
0,5 % of full scale subsections (a) and (b) of this section shall be
repeated.
(d) The 5 % and 10 % oxygen interference check gases shall be intro-
duced.
(e) The zero response shall be rechecked. If it has changed more than
± 1 % of full scale, the test shall be repeated.1997L0068 — EN — 11.02.2003 — 002.001 — 77
▼M2
(f) The oxygen interference ( % O2I) shall be calculated for each
mixture in step (d) as follows:
O2I¼B/C0C ðÞ
B/C2100
ppm C ¼A
D
where:
A = hydrocarbon concentration (ppm C) of the span gas used in
subsection (b)
B = hydrocarbon concentration (ppm C) of the oxygen interfer-
ence check gases used in subsection (d)
C = analyser response
D = percent of full scale analyser response due to A
(g) The % of oxygen interference ( % O2I) shall be less than ± 3 %
for all required oxygen interference check gases prior to testing.
(h) If the oxygen interference isgreater than ± 3 %, the air flow
above and below the manufacturer's specifications shall be incre-
mentally adjusted, repeating section 1.9.1 for each flow.
(i) If the oxygen interference isgreater than ± 3 %, after adjus ting the
air flow, the fuel flow and thereafter the sample flow shall be
varied, repeating section 1.9.1 for each new setting.
(j) If the oxygen interference is still greater than ± 3 %, the analyser,
FID fuel, or burner air shall be repaired or replaced prior to
testing. This section shall then be repeated with the repaired or
replaced equipment or gases.
1.10.Interference effectswithCO,CO2,NOXandO2analysers
Gases other than the one being analysed can interfere with the reading
in several ways. Positive interference occurs in NDIR and PMD instru-
mentswhere the interfering gasgivesthe s ame effect asthe gasbeing
measured, but to a lesser degree. Negative interference occurs in
NDIR instruments by the interfering gas broadening the absorption
band of the measured gas, and in CLD instruments by the interfering
gasquenching the radiation. The interference checksin s ections1.10.1
and 1.10.2 shall be performed prior to an analyser's initial use and
after major service intervals, but at least once per year.
1.10.1. CO analyser interference check
Water and CO2can interfere with the CO analyser performance.
Therefore a CO2span gas having a concentration of 80 % to 100 %
of full scale of the maximum operating range used during testing shall
be bubbled through water at room temperature and the analyser
response recorded. The analyser response must not be more than 1 %
of full scale for ranges equal to or above 300 ppm or more than 3 ppm
for rangesbelow 300 ppm.
1.10.2. NOxanalyser quench checks
The two gases of concern for CLD (and HCLD) analysers are CO2and
water vapour. Quench responses of these gases are proportional to
their concentrations, and therefore require test techniques to determine
the quench at the highest expected concentrations experienced during
testing.
1.10.2.1. CO2quench check
AC O2span gas having a concentration of 80 % to 100 % of full scale
of the maximum operating range shall be passed through the NDIR
analyser and the CO2value recorded asA. It s hall then be diluted
approximately 50 % with NO span gas and passed through the NDIR
and (H)CLD with the CO2and NO valuesrecorded asB and C,
respectively. The CO2shall be shut off and only the NO span gas is
passed through the (H)CLD and the NO value recorded as D.1997L0068 — EN — 11.02.2003 — 002.001 — 78
▼M2
The quench, which shall not be greater than 3 % full scale, shall be
calculated asfollows :
%C O 2quench ¼1/C0C/C2A ðÞ
D/C2A ðÞ /C0 D/C2B ðÞ/C18/C19/C20/C21
/C2100
where:
A: undiluted CO2concentration measured with NDIR %
B: diluted CO2concentration measured with NDIR %
C: diluted NO concentration measured with CLD ppmD: undiluted NO concentration measured with CLD ppm
Alternative methodsof diluting and quantifying CO
2and NO span gas
values, such as dynamic/mixing/blending, can be used.
1.10.2.2. Water quench check
Thischeck appliesto wet gasconcentration meas urementsonly.
Calculation of water quench must consider dilution of the NO span
gaswith water vapour and s caling of water vapour concentration of
the mixture to that expected during testing.
A NO span gas having a concentration of 80 % to 100 % of full scale
to the normal operating range shall be passed through the (H)CLD and
the NO value recorded as D. The NO span gas shall then be bubbled
through water at room temperature and passed through the (H)CLD
and the NO value recorded asC. The water temperature s hall be deter-
mined and recorded as F. The mixture's saturation vapour pressure that
corresponds to the bubbler water temperature (F) shall be determined
and recorded asG. The water vapour concentration (in %) of the
mixture shall be calculated as follows:
H¼100/C2G
pB/C18/C19
and recorded asH. The expected diluted NO s pan gas(in water
vapour) concentration shall be calculated as follows:
De¼D/C21/C0H
100/C18/C19
and recorded asDe.
The water quench shall not be greater than 3 % and shall be calculated
asfollows :
%H2O quench ¼100/C2De/C0C
De/C18/C19
/C2Hm
H/C18/C19
where:
De: expected diluted NO concentration (ppm)
C: diluted NO concentration (ppm)H
m: maximum water vapour concentration
H: actual water vapour concentration (%).
Note:It isimportant that the NO s pan gascontainsminimal NO2concentration for this check, since absorption of NO2in water
hasnot been accounted for in the quench calculations .
1.10.3. O2analyser interference
Instrument response of a PMD analyser caused by gases other than
oxygen iscomparatively s light. The oxygen equivalentsof the
common exhaust gas constituents are shown in table 1.
Tabel 1 — Oxygen equivalents
GasO2equivalent %
Carbon dioxide (CO2) − 0,623
Carbon monoxide (CO) − 0,354
Nitrogen oxide (NO) + 44,4Nitrogen dioxide (NO
2) + 28,71997L0068 — EN — 11.02.2003 — 002.001 — 79
▼M2
GasO2equivalent %
Water (H2O) − 0,381
The observed oxygen concentration shall be corrected by the following
formula if high precision measurements are to be done:
Interference ¼Equivalent % O 2/C2Obs :conc : ðÞ
100
1.11.Calibrationintervals
The analysers shall be calibrated according to section 1.5 at least
every three months or whenever a system repair or change is made
that could influence calibration.1997L0068 — EN — 11.02.2003 — 002.001 — 80
▼M2
Appendix 3
1. DATA EVALUATION AND CALCULATIONS
1.1.Gaseousemissionsevaluation
For the evaluation of the gaseous emissions, the chart reading for a
minimum of the last 120 s of each mode shall be averaged, and the
average concentrations(conc) of HC, CO, NOxand CO2during each
mode shall be determined from the average chart readings and the corre-
sponding calibration data. A different type of recording can be used if it
ensures an equivalent data acquisition.
The average background concentration (concd) may be determined from
the bag readingsof the dilution air or from the continuous(non-bag)
background reading and the corresponding calibration data.
1.2.Calculationofthegaseousemissions
The finally reported test results shall be derived through the following
steps.
1.2.1. Dry/wet correction
The measured concentration, if not already measured on a wet basis, shall
be converted to a wet basis:
conc (wet) = kw× conc (dry)
For the raw exhaust gas:
kw¼kw;r¼1
1þα/C20;005/C2% CO dry ½/C138 þ %C O 2dry½/C138 ðÞ /C0 0;01/C2%H2dry½/C138 þ kw2
where αisthe hydrogen to carbon ratio in the fuel.
The H2concentration in the exhaust shall be calculated:
H2dry½/C138 ¼05/C2α/C2% CO dry ½/C138 /C2 % CO dry ½/C138 þ %C O 2dry½/C138 ðÞ
% CO dry ½/C138 þ 3/C2%C O 2dry½/C138 ðÞ
The factor kw2shall be calculated:
kw2¼1;608/C2Ha
1000 þ1;608/C2Ha ðÞ
with Haabsolute humidity of the intake air as g of water per kg of dry air.
For the diluted exhaust gas:
for wet CO2measurement::
kw¼kw;e;1¼1/C0α/C2% CO2 wet ½/C138
200/C18/C19
/C0kw1
or, for dry CO2measurement:
kw¼kw;e;2¼1/C0kw1 ðÞ
1þα/C2%C O 2dry½/C138
2000
BB@1
CCA
where αisthe hydrogen to carbon ratio in the fuel.
The factor kw1shall be calculated from the following equations:
kw1¼1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
1000 þ1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
where:
Hdabsolute humidity of the dilution air, g of water per kg of dry air1997L0068 — EN — 11.02.2003 — 002.001 — 81
▼M2
Haabsolute humidity of the intake air, g of water per kg of dry air
DF¼13;4
% conc CO2þppm conc COþppm conc HC ðÞ /C2 10/C04
For the dilution air:
kw,d=1−kw1
The factor kw1shall be calculated from the following equations:
DF¼13;4
% conc CO2þppm conc COþppm conc HC ðÞ /C2 10/C04
kw1¼1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
1000 þ1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
where:
Hdabsolute humidity of the dilution air, g of water per kg of dry air
Haabsolute humidity of the intake air, g of water per kg of dry air
DF¼13;4
% conc CO2þppm conc COþppm conc HC ðÞ /C2 10/C04
For the intake air (if different from the dilution air):
kw,a=1−kw2
The factor kw2shall be calculated from the following equations:
kw2¼1;608/C2Ha
1000 þ1;608/C2Ha ðÞ
with Haabsolute humidity of the intake air, g of water per kg of dry air.
1.2.2. Humidity correction for NOx
Asthe NOxemission depends on ambient air conditions, the NOxconcen-
tration shall be multiplied by the factor KHtaking into account humidity:
KH= 0,6272 + 44,030 × 10−3×Ha− 0,862 × 10−3×Ha2(for 4 stroke
engines)
KH= 1 (for 2 stroke engines)
with Haabsolute humidity of the intake air as g of water per kg of dry air.
1.2.3. Calculation of emission mass flow rate
The emission mass flow rates Gasmass[g/h] for each mode shall be calcu-
lated asfollows .
(a) For the raw exhaust gas (1):
Gasmass¼MWGas
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
where:
GFUEL[kg/h] isthe fuel mas sflow rate;1997L0068 — EN — 11.02.2003 — 002.001 — 82
(1) In the case of NOxthe concentration hasto be multiplied by the humidity correction
factor KH(humidity correction factor for NOx).
▼M2
MWGas[kg/kmol] isthe molecular weight of the individual gass hown
in table 1;
Table 1 — Molecular weights
GasMWGas[kg/kmol]
NOx46,01
CO 28,01HC MW
HC=M WFUEL
CO244,01
—M WFUEL= 12,011 + α× 1,00794 + β× 15,9994 [kg/kmole] isthe
fuel molecular weight with αhydrogen to carbon ratio and β
oxygen to carbon ratio of the fuel (1);
—C O2AIRisthe CO2concentration in the intake air (that is assumed
equal to 0,04 % if not measured).
(b) For the diluted exhaust gas (2):
Gasmass= u × concc×GTOTW
where:
—GTOTW[kg/h] is the diluted exhaust gas mass flow rate on wet
basis that, when using a full flow dilution system, shall be deter-mined according to Annex III, Appendix 1, section 1.2.4,
— conc
cisthe background corrected concentration:
concc= conc − concd× (1 − 1/DF)
with
DF¼13;4
% conc CO2þppm conc COþppm conc HC ðÞ /C2 10/C04
The u coefficient iss hown in table 2.
Table 2 — Valuesof u coefficient
Gasu conc
NOx0,001587 ppm
CO 0,000966 ppm
HC 0,000479 ppmCO
215,19 %
Valuesof the u coefficient are bas ed upon a molecular weight of the
dilute exhaust gases equal to 29 [kg/kmol]; the value of u for HC is
based upon an average carbon to hydrogen ratio of 1:1,85.
1.2.4. Calculation of specific emissions
The specific emission (g/kWh) shall be calculated for all individual
components:1997L0068 — EN — 11.02.2003 — 002.001 — 83
(1) In the ISO 8178-1 a more complete formula of the fuel molecular weight isquoted
(formula 50 of Chapter 13.5.1(b)). The formula takesinto account not only the
hydrogen to carbon ratio and the oxygen to carbon ratio but also other possible fuel
components such as sulphur and nitrogen. However, as the SI. engines of the Directiveare tested with a petrol (quoted as a reference fuel in Annex V) containing usually onlycarbon and hydrogen, the simplified formula is considered.
(
2) In the case of NOxthe concentration hasto be multiplied by the humidity correction
factor KH(humidity correction factor for NOx).
▼M2
Individual Gas ¼Xn
i¼1Gasmassi/C2WFi ðÞ
Xn
i¼1Pi/C2WFi ðÞ
where Pi=PM,i+PAE,i
When auxiliaries, such as cooling fan or blower, are fitted for the test, the
power absorbed shall be added to the results except for engines where
such auxiliaries are an integral part of the engine. The fan or blower
power shall be determined at the speeds used for the tests either by calcu-
lation from standard characteristics or by practical tests (Appendix 3 of
Annex VII).
The weighting factorsand the number of the n modesus ed in the above
calculation are shown in Annex IV, section 3.5.1.1.
2. EXAMPLES
2.1.Rawexhaustgasdatafromafour-strokeSIengine
With reference to the experimental data (table 3), calculationsare carried
out first for mode 1 and then are extended to other test modes using the
same procedure.
Table 3 — Experimental data of a four-stroke SI engine
Mode 1 2 3 4 5 6
Engine speed min−12 550 2 550 2 550 2 550 2 550 1 480
Power kW 9,96 7,5 4,88 2,36 0,94 0Load percent % 100 75 50 25 10 0
Weighting
factors— 0,090 0,200 0,290 0,300 0,070 0,050
Barometric
pressurekPa 101,0 101,0 101,0 101,0 101,0 101,0
Air temperature ºC 20,5 21,3 22,4 22,4 20,7 21,7
Air relative
humidity% 38,0 38,0 38,0 37,0 37,0 38,0
Air absolute
humidityg
H20/kgair5,696 5,986 6,406 6,236 5,614 6,136
CO dry ppm 60 995 40 725 34 646 41 976 68 207 37 439
NOxwet ppm 726 1 541 1 328 377 127 85
HC wet ppm C1 1 461 1 308 1 401 2 073 3 024 9 390
CO2dry % Vol. 11,4098 12,691 13,058 12,566 10,822 9,516
Fuel mass flow kg/h 2,985 2,047 1,654 1,183 1,056 0,429Fuel H/C ratio
α— 1,85 1,85 1,85 1,85 1,85 1,85
Fuel O/C ratio
β00000 01997L0068 — EN — 11.02.2003 — 002.001 — 84
▼M2
2.1.1. Dry/wet correction factor kw
The dry/wet correction factor kw shall be calculated for converting dry
CO and CO2measurements on a wet basis:
kw¼kw;r¼1
1þα/C20;005/C2% CO dry ½/C138 þ %C O 2dry½/C138 ðÞ /C0 0;01/C2%H2dry½/C138 þ kw2
where:
H2dry½/C138 ¼0;5/C2α/C2% CO dry ½/C138 /C2 % CO dry ½/C138 þ %C O 2dry½/C138 ðÞ
% CO dry ½/C138 þ 3/C2%C O 2dry½/C138 ðÞ
and
kw2¼1;608/C2Ha
1000 þ1;608/C2Ha ðÞ
H2dryðÞ ¼0;5/C21;85/C26;0995 /C26;0995 þ11;4098 ðÞ
6;0995 þ3/C211;4098 ðÞ¼2;450 %
kw2¼1;608/C25;696
1000 þ1;608/C25;696 ðÞ¼0;009
kw¼kw;r¼1
1þ1;85/C20;005/C26;0995 þ11;4098 ðÞ /C00;01/C22;450þ0;009¼0;872
CO [wet] = CO [dry] × kw= 60 995 × 0,872 = 53 198 ppm
CO2[wet] = CO2[dry] × kw= 11,410 × 0,872 = 9,951 % Vol
Table 4 — CO and CO2wet valuesaccording to different tes t modes
Mode 1 2 3 4 5 6
H2dry % 2,450 1,499 1,242 1,554 2,834 1,422
kw2— 0,009 0,010 0,010 0,010 0,009 0,010
kw— 0,872 0,870 0,869 0,870 0,874 0,894
CO wet ppm 53 198 35 424 30 111 36 518 59 631 33 481
CO2wet % 9,951 11,039 11,348 10,932 9,461 8,510
2.1.2. HC emissions
HCmass¼MWHC
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
Where:
MWHC=M WFUEL
MWFUEL= 12,011 + α 1,00794 = 13,876
HCmass¼13;876
13;876/C21
9;951/C00;04þ5;3198 þ0;1461 ðÞ/C20;1461 /C22;985/C21000 ¼28;361 g =h1997L0068 — EN — 11.02.2003 — 002.001 — 85
▼M2
Table 5 — HC emissions [g/h] according to different test modes
Mode 123456
HCmass28,361 18,248 16,026 16,625 20,357 31,578
2.1.3. NOxemissions
At first the humidity correction factor KHof NOxemissions shall be
calculated:
KH= 0,6272 + 44,030 × 10−3×Ha− 0,862 × 10−3×Ha2
KH= 0,6272 + 44,030 × 10−3× 5,696 − 0,862 × 10−3×(5,696)2= 0,850
Table 6 — Humidity correction factor KHof NOxemissions according to different modes
Mode 123456
KH0,850 0,860 0,874 0,868 0,847 0,865
Then NOxmass[g/h] shall be calculated:
NOxmass¼MWNOx
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2KH/C2GFUEL/C21000
NOxmass¼46;01
13;876/C21
9;951/C00;04þ5;3198 þ0;1461/C20;073/C20;85/C22;985/C21000 ¼39;717 g =h
Table 7 — NOxemissions [g/h] according to the different test modes
Mode 123456
NOxmass39,717 61,291 44,013 8,703 2,401 0,820
2.1.4 CO emissions
COmass¼MWCO
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
CO2mass¼44;01
13;876/C21
9;951/C00;04þ5;3198 þ0;1461/C29;951/C22;985/C21000 ¼6126 ;806 g =h
Table 8 — CO emissions [g/h] according to different test modes
Mode 123456
COmass2 084,588 997,638 695,278 591,183 810,334 227,285
2.1.5. CO2emissions
CO2mass¼MWCO2
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
CO2mass¼44;01
13;876/C21
9;951/C00;04þ5;3198 þ0;1461/C29;951/C22;985/C21000 ¼6126 ;806 g =h1997L0068 — EN — 11.02.2003 — 002.001 — 86
▼M2
Table 9 — CO2emissions [g/h] according to different test modes
Mode 123456
CO2mass6 126,806 4 884,739 4 117,202 2 780,662 2 020,061 907,648
2.1.6. Specific emissions
The specific emission (g/kWh) shall be calculated for all individual
components:
Individual gas ¼Xn
i¼1Gasmassi/C2WFi ðÞ
Xn
i¼1Pi/C2WFi ðÞ
Table 10 — Emissions [g/h] and weighting factors according to the test modes
Mode 1 2 3 4 5 6
HCmassg/h 28,361 18,248 16,026 16,625 20,357 31,578
NOxmassg/h 39,717 61,291 44,013 8,703 2,401 0,820
COmassg/h 2 084,5-
88997,638 695,278 591,183 810,334 227,285
CO2massg/h 6 126,8-
064 884,7-
394 117,2-
022 780,6-
622 020,0-
61907,648
Power PIkW 9,96 7,50 4,88 2,36 0,94 0
Weighting
factorsWFI— 0,090 0,200 0,290 0,300 0,070 0,050
HC¼28;361/C20;090þ18;248/C20;200þ16;026/C20;290þ16;625/C20;300þ20;357/C20;070þ31;578/C20;050
9;96/C20;090þ7;50/C20;200þ4;88/C20;290þ2;36/C20;300þ0;940/C20;070þ0/C20;050¼4;11 g =kWh
NOx¼39;717/C20;090þ61;291/C20;200þ44;013/C20;290þ8;703/C20;300þ2;401/C20;070þ0;820/C20;050
9;96/C20;090þ7;50/C20;200þ4;88/C20;290þ2;36/C20;300þ0;940/C20;070þ0/C20;050¼6;85 g =kWh
CO¼2084 ;59/C20;090þ997 ;64/C20;200þ695 ;28/C20;290þ591 ;18/C20;300þ810 ;33/C20;070þ227 ;92/C20;050
9;96/C20;090þ7;50/C20;200þ4;88/C20;290þ2;36/C20;300þ0;940/C20;070þ0/C20;050¼181 ;93 g =kWh
CO2¼6126 ;81/C20;090þ4884 ;74/C20;200þ4117 ;20/C20;290þ2780 ;66/C20;300þ2020 ;06/C20;070þ907 ;65/C20;050
9;96/C20;090þ7;50/C20;200þ4;88/C20;290þ2;36/C20;300þ0;940/C20;070þ0/C20;050¼816 ;36 g =kWh
2.2.Rawexhaustgasdatafromatwo-strokeSIengine
With reference to the experimental data (table 11), calculationss hall be
carried out first for mode 1 and then extended to the other test mode
using the same procedure.
Table 11 — Experimental data of a two-stroke SI engine
Mode 1 2
Engine speed min−19 500 2 800
Power kW 2,31 0Load percent % 100 0
Weighting
factors— 0,9 0,11997L0068 — EN — 11.02.2003 — 002.001 — 87
▼M2
Mode 1 2
Barometric
pressurekPa 100,3 100,3
Air temperature ºC 25,4 25
Air relative
humidity% 38,0 38,0
Air absolute
humiditygH20/kgair7,742 7,558
CO dry ppm 37 086 16 150
NOxwet ppm 183 15
HC wet ppmC1 14 220 13 179CO
2dry % Vol. 11,986 11,446
Fuel mass flow kg/h 1,195 0,089
Fuel H/C ratio
α— 1,85 1,85
Fuel O/C ratio
β00
2.2.1 Dry/wet correction factor kw
The dry/wet correction factor kw shall be calculated for converting dry
CO and CO2measurements on a wet basis:
kw¼kw;r¼1
1þα/C20;005/C2% CO dry ½/C138 þ %C O 2dry½/C138 ðÞ /C0 0;01/C2%H2dry½/C138 þ kw2
Where:
H2dry½/C138 ¼0:5/C2α/C2% CO dry ½/C138 /C2 % CO dry ½/C138 þ %C O 2dry½/C138 ðÞ
% CO dry ½/C138 þ 3/C2%C O 2dry½/C138 ðÞ
H2dry½/C138 ¼0;5/C21;85/C23;7086 /C23;7086 þ11;986 ðÞ
3;7086 þ3/C211;986 ðÞ¼1;357 %
kw2¼1;608/C2Ha
1000 þ1;608/C2Ha ðÞ
kw2¼1;608/C27;742
1000 þ1;608/C27;742 ðÞ¼0;012
kw¼kw;r¼1
1þ1;85/C20;005/C23;7086 þ11;986 ðÞ /C0 0;01/C21;357þ0;012¼0;874
CO [wet] = CO [dry] × kw= 37 086 × 0,874 = 32 420 ppm
CO2[wet] = CO2[dry] × kw= 11,986 × 0,874 = 10,478 % Vol
Table 12 — CO and CO2wet valuesaccording to different tes t modes
Mode 1 2
H2dry % 1,357 0,5431997L0068 — EN — 11.02.2003 — 002.001 — 88
▼M2
Mode 1 2
kw2— 0,012 0,012
kw — 0,874 0,887CO wet ppm 32 420 14 325
CO
2wet % 10,478 10,153
2.2.2. HC emissions
HCmass¼MWHC
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
where:
MWHC=M WFUEL
MWFUEL= 12,011 + α× 1,00794 = 13,876
HCmass¼13;876
13;876/C21
10;478/C00;04þ3;2420 þ1;422 ðÞ/C21;422/C21;195/C21000 ¼112 ;520 g =h
Table 13 — HC emissions [g/h] according to test modes
Mode 1 2
HCmass112,520 9,119
2.2.3. NOxemissions
The factor KHfor the correction of the NOxemissions is equal to 1 for
two-stroke engines:
NOxmass¼MWNOx
MWFUEL/C21
f%C O 2wet½/C138 /C0%C O 2AIR ðÞ þ% CO wet ½/C138 þ% HC wet ½/C138 g/C2% conc /C2KH/C2GFUEL/C21000
NOxmass¼46;01
13;876/C21
10;478/C00;04þ3;2420 þ1;422/C20;0183 /C21/C21;195/C21000 ¼4;800 g =h
Table 14 — NOxemissions [g/h] according to test modes
Mode 1 2
NOxmass4,800 0,034
2.2.4. CO emissions
COmass¼MWCO
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
COmass¼28;01
13;876/C21
10;478/C00;04þ3;2420 þ1;422 ðÞ/C23;2420 /C21;195/C21000 ¼517 ;851 g =h1997L0068 — EN — 11.02.2003 — 002.001 — 89
▼M2
Table 15 — CO emissions [g/h] according to test modes
Mode 1 2
COmass517,851 20,007
2.2.5. CO2emissions
CO2mass¼MWCO2
MWFUEL/C21
f%C O 2wet½/C138 /C0 %C O 2AIR ðÞ þ % CO wet ½/C138 þ % HC wet ½/C138 g/C2% conc /C2GFUEL/C21000
CO2mass¼44;01
13;876/C21
10;478/C00;04þ3;2420 þ1;422 ðÞ/C210;478/C21;195/C21000 ¼2629 ;658 g =h
Table 16 — CO2emissions [g/h] according to test modes
Mode 1 2
CO2mass2 629,658 222,799
2.2.6. Specific emissions
The specific emission (g/kWh) shall be calculated for all individual
componentsin the following way:
Individual gas ¼Xn
i¼1Gasmassi/C2WFi ðÞ
Xn
i¼1Pi/C2WFi ðÞ
Table 17 — Emissions [g/h] and weighting factors in two test modes
Mode 1 2
HCmassg/h 112,520 9,119
NOxmassg/h 4,800 0,034
COmassg/h 517,851 20,007
CO2massg/h 2 629,658 222,799
Power PIIkW 2,31 0
Weighting
factorsWFi— 0,85 0,15
HC¼112 ;52/C20;85þ9;119/C20;15
2;31/C20;85þ0/C20;15¼49;4g =kWh
NOx¼4;800/C20;85þ0;034/C20;15
2;31/C20;85þ0/C20;15¼2;08 g =kWh
CO¼517 ;851/C20;85þ20;007/C20;15
2;31/C20;85þ0/C20;15¼225 ;71 g =kWh
CO2¼2629 ;658/C20;85þ222 ;799/C20;15
2;31/C20;85þ0/C20;15¼1155 ;4g =kWh1997L0068 — EN — 11.02.2003 — 002.001 — 90
▼M2
2.3.Dilutedexhaustgasdatafromafour-strokeSIengine
With reference to the experimental data (table 18), calculationss hall be
carried out first for mode 1 and then extended to other test modes using
the same procedure.
Table 18 — Experimental data of a four-stroke SI engine
Mode 1 2 3 4 5 6
Engine speed min−13 060 3 060 3 060 3 060 3 060 2 100
Power kW 13,15 9,81 6,52 3,25 1,28 0
Load percent % 100 75 50 25 10 0
Weighting
factors— 0,090 0,200 0,290 0,300 0,070 0,050
Barometric
pressurekPa 980 980 980 980 980 980
Intake air
temperature (1)ºC 25,3 25,1 24,5 23,7 23,5 22,6
Intake air rela-
tive humidity (1)% 19,8 19,8 20,6 21,5 21,9 23,2
Intake air abso-
lute humidity (1)gH20/kgair4,08 4,03 4,05 4,03 4,05 4,06
CO dry ppm 3 681 3 465 2 541 2 365 3 086 1 817
NOxwet ppm 85,4 49,2 24,3 5,8 2,9 1,2
HC wet ppm C1 91 92 77 78 119 186CO
2dry % Vol 1,038 0,814 0,649 0,457 0,330 0,208
CO dry (back-
ground)p p m 33322 3
NOxwet (back-
ground)ppm 0,1 0,1 0,1 0,1 0,1 0,1
HC wet (back-
ground)ppm C1 6 6 5 6 6 4
CO2dry (back-
ground)% Vol 0,042 0,041 0,041 0,040 0,040 0,040
Dil. exh. gas
mass flow
GTOTWkg/h 625,722 627,171 623,549 630,792 627,895 561,267
Fuel H/C ratio
α— 1,85 1,85 1,85 1,85 1,85 1,85
Fuel O/C ratio
β00000 0
(1) Dilution air conditionsequal to intake air conditions .
2.3.1. Dry/wet correction factor kw
The dry/wet correction factor kwshall be calculated for converting dry
CO and CO2measurements on a wet basis.1997L0068 — EN — 11.02.2003 — 002.001 — 91
▼M2
For the diluted exhaust gas:
kw¼kw;e;2¼1/C0kw1 ðÞ
1þα/C2%C O 2dry½/C138
2000
BB@1
CCA
where:
kw1¼1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
1000 þ1;608/C2Hd/C21/C01=DF ðÞ þ Ha/C21=DFðÞ ½/C138
DF¼13;4
% conc CO2þppm conc COþppm conc HC ðÞ /C2 10/C04
DF¼13;4
1;038þ3681 þ91 ðÞ /C2 10/C04¼9;465
kw1¼1;608/C24;08/C21/C01=9;465 ðÞ þ 4;08/C21=9;465 ðÞ ½/C138
1000 þ1;608/C24;08/C21/C01=9;465 ðÞ þ 4;08/C21=9;465 ðÞ ½/C138¼0;007
kw¼kw;e;2¼1/C00;007 ðÞ
1þ1;85/C21;038
2000
B@1
CA¼0;984
CO [wet] = CO [dry] × kw= 3 681 × 0,984 = 3 623 ppm
CO2[wet] = CO2[dry] × kw= 1,038 × 0,984 = 1,0219 %
Table 19 — CO and CO2wet values for the diluted exhaust gas according to test modes
Mode 1 2 3 4 5 6
DF — 9,465 11,454 14,707 19,100 20,612 32,788
kw1— 0,007 0,006 0,006 0,006 0,006 0,006
kw— 0,984 0,986 0,988 0,989 0,991 0,992
CO wet ppm 3 623 3 417 2 510 2 340 3 057 1 802
CO2wet % 1,0219 0,8028 0,6412 0,4524 0,3264 0,2066
For the dilution air:
kw,d=1−kw1
Where the factor kw1isthe s ame asthat already calculated for the diluted
exhaust gas.
kw,d= 1 − 0,007 = 0,993
CO [wet] = CO [dry] × kw= 3 × 0,993 = 3 ppm
CO2[wet] = CO2[dry] × kw= 0,042 × 0,993 = 0,0421 % Vol
Table 20 — CO and CO2wet valuesfor the dilution air according to tes t modes
Mode 1 2 3 4 5 6
Kw1— 0,007 0,006 0,006 0,006 0,006 0,0061997L0068 — EN — 11.02.2003 — 002.001 — 92
▼M2
Mode 1 2 3 4 5 6
Kw — 0,993 0,994 0,994 0,994 0,994 0,994
CO wet ppm 3 3 3 2 2 3CO
2wet % 0,0421 0,0405 0,0403 0,0398 0,0394 0,0401
2.3.2. HC emissions
HCmass= u × concc×GTOTW
Where:u = 0,000478 from table 2
conc
c= conc − concd× (1−1/DF)
concc= 91 − 6 × (1−1/9,465) = 86 ppm
HCmass= 0,000478 × 86 × 625,722 = 25,666 g/h
Table 21 — HC emissions [g/h] according to test modes
Mode 123456
HCmass25,666 25,993 21,607 21,850 34,074 48,963
2.3.3. NOxemissions
The factor KHfor the correction of the NOxemissions shall be calculated
from:
KH¼0;6272 þ44;030/C210/C03/C2Ha/C00;862/C210/C03/C2H2
a
KH= 0,6272 + 44,030 × 10−3× 4,08 − 0,862 × 10−3× (4,08)2= 0,79
Table 22 — Humidity correction factor KHof NOxemissions according to test modes
Mode 123456
KH0,793 0,791 0,791 0,790 0,791 0,792
NOxmass= u × concc×KH×GTOTW
where:
u = 0,001587 from table 2
concc= conc − concd× (1−1/DF)
concc= 85 − 0 × (1−1/9,465) = 85 ppm
NOxmass= 0,001587 × 85 × 0,79 × 625,722 = 67,168 g/h
Table 23 — NOxemissions [g/h] according to test modes
Mode 123456
NOxmass67,168 38,721 19,012 4,621 2,319 0,811
2.3.4. CO emissions
COmass= u × concc×GTOTW
where:
u = 0,000966 from table 2
concc= conc − concd× (1−1/DF)
concc= 3 622 − 3 × (1−1/9,465) = 3 620 ppm1997L0068 — EN — 11.02.2003 — 002.001 — 93
▼M2
COmass= 0,000966 × 3 620 × 625,722 = 2 188,001 g/h
Table 24 — CO emissions [g/h] according to test modes
Mode 123456
COmass2 188,001 2 068,760 1 510,187 1 424,792 1 853,109 975,435
2.3.5. CO2emissions
CO2mass= u × concc×GTOTW
where:u = 15,19 from table 2
conc
c= conc − concd× (1−1/DF)
concc= 1,0219 − 0,0421 × (1−1/9,465) = 0,9842 % Vol
CO2mass= 15,19 × 0,9842 × 625,722 = 9 354,488 g/h
Table 25 — CO2emissions [g/h] according to different test modes
Mode 123456
CO2mass9 354,488 7 295,794 5 717,531 3 973,503 2 756,113 1 430,229
2.3.6. Specific emissions
The specific emission (g/kWh) shall be calculated for all individual
components:
Individual gas ¼Xn
i¼1Gasmassi/C2WFi ðÞ
Xn
i¼1Pi/C2WFi ðÞ
Table 26 — Emissions [g/h] and weighting factors according to different test modes
Mode 1 2 3 4 5 6
HCmassg/h 25,666 25,993 21,607 21,850 34,074 48,963
NOxmassg/h 67,168 38,721 19,012 4,621 2,319 0,811
COmassg/h 2 188,0-
012 068,7-
601 510,1-
871 424,7-
921 853,1-
09975,435
CO2massg/h 9 354,4-
887 295,7-
945 717,5-
313 973,5-
032 756,1-
131 430,229
Power PikW 13,15 9,81 6,52 3,25 1,28 0
Weighting
factorsWFI— 0,090 0,200 0,290 0,300 0,070 0,0501997L0068 — EN — 11.02.2003 — 002.001 — 94
▼M2
HC¼25;666/C20;090þ25;993/C20;200þ21;607/C20;290þ21;850/C20;300þ34;074/C20;070þ48;963/C20;050
13;15/C20;090þ9;81/C20;200þ6;52/C20;290þ3;25/C20;300þ1;28/C20;070þ0/C20;050¼4;12 g =kWh
NOx¼67;168/C20;090þ38;721/C20;200þ19;012/C20;290þ4;621/C20;300þ2;319/C20;070þ0;811/C20;050
13;15/C20;090þ9;81/C20;200þ6;52/C20;290þ3;25/C20;300þ1;28/C20;070þ0/C20;050¼3;42 g =kWh
CO¼2188 ;001/C20;09þ2068 ;760/C20;2þ1510 ;187/C20;29þ1424 ;792/C20;3þ1853 ;109/C20;07þ975 ;435/C20;05
13;15/C20;090þ9;81/C20;200þ6;52/C20;290þ3;25/C20;300þ1;28/C20;070þ0/C20;050¼271 ;15 g =kWh
CO2¼9354 ;488/C20;09þ7295 ;794/C20;2þ5717 ;531/C20;29þ3973 ;503/C20;3þ2756 ;113/C20;07þ1430 ;229/C20;05
13;15/C20;090þ9;81/C20;200þ6;52/C20;290þ3;25/C20;300þ1;28/C20;070þ0/C20;050¼887 ;53 g =kWh1997L0068 — EN — 11.02.2003 — 002.001 — 95
▼M2
Appendix 4
1. COMPLIANCE WITH EMISSION STANDARDS
This Appendix shall apply to SI engines stage 2 only.
1.1. The exhaust emission standards for stage 2 engines in Annex I (4.2)
apply to the emissions of the engines for their emission durability
period EDP asdetermined in accordance with thisAppendix.
1.2. For all stage 2 engines, if, when properly tested according to the proce-
dures in this Directive, all test engines representing an engine family
have emissions which, when adjusted by multiplication by the dete-
rioration factor (DF) laid down in thisAppendix, are les sthan or
equal to each stage 2 emission standard (family emission limit (FEL),
where applicable) for a given engine class, that family shall be consid-
ered to comply with the emission standards for that engine class. If any
test engine representing an engine family has emissions which, when
adjusted by multiplication by the deterioration factor laid down in this
Appendix, are greater than any single emission standard (FEL, where
applicable) for a given engine class, that family shall be considered
not to comply with the emission standards for that engine class.
1.3. Small volume engine manufacturersmay, optionally, take deterioration
factorsfor HC+NOxand CO from table 1 or 2 in thiss ection, or they
may calculate deterioration factorsfor HC+NOxand CO according to
the process described in section 1.3.1. For technologies not covered by
tables 1 and 2 in this section, the manufacturer must use the process
described in section 1.4 in this Appendix.
Table 1: Hand-held engine HC+NOxand CO assigned deterioration factors for small volume manu-
facturer
Engine classTwo-stroke engines Four-stroke enginesEngineswith after
treatmentHC + NOxCO HC + NOxCO
SH:1 1,1 1,1 1,5 1,1 DFsmus t be calcu-
lated using the
formula in section
1.3.1SH:2 1,1 1,1 1,5 1,1
SH:3 1,1 1,1 1,5 1,1
Table 2: Non-hand-held engine HC+NOxand CO assigned deterioration factors for small volume
manufacturers
Engine ClassSide Valve EnginesOverhead Valve EnginesEngineswith after
treatmentHC + NOxCO HC + NOxCO
SN:1 2,1 1,1 1,5 1,1 DFsmus t be calcu-
lated using the
formula in section
1.3.1SN:2 2,1 1,1 1,5 1,1
SN:3 2,1 1,1 1,5 1,1
SN:4 1,6 1,1 1,4 1,1
1.3.1. Formula for calculating deterioration factors for engines with after
treatment:
DF = [(NE * EDF) − (CC * F)] / (NE − CC)
where:
DF = deterioration factor
NE = new engine emission levels prior to the catalyst (g/kWh)EDF = deterioration factor for engines without catalyst as shown in
table 1
CC = amount converted at 0 hoursin g/kWhF = 0,8 for HC and 0,0 for NO
xfor all classes of engines
F = 0,8 for CO for all classes of engines1997L0068 — EN — 11.02.2003 — 002.001 — 96
▼M2
1.4. Manufacturers shall obtain an assigned DF or calculate a DF, as appro-
priate, for each regulated pollutant for all stage 2 engine families. Such
DFs shall be used for type approval and production line testing.
1.4.1. For engines not using assigned DFs from tables 1 or 2 of this section,
DFs shall be determined as follows:
1.4.1.1. On at least one test engine representing the configuration chosen to be
the most likely to exceed HC + NOxemission standards, (FELs where
applicable), and constructed to be representative of production engines,
conduct (full) test procedure emission testing as described in this Direc-
tive after the number of hours representing stabilised emissions.
1.4.1.2 If more than one engine is tested, average the results and round to the
same number of decimal places contained in the applicable standard,
expressed to one additional significant figure.
1.4.1.3 Conduct such emission testing again following ageing of the engine.
The ageing procedure should be designed to allow the manufacturer to
appropriately predict the in-use emission deterioration expected over the
durability period of the engine, taking into account the type of wear and
other deterioration mechanisms expected under typical consumer use
which could affect emissions performance. If more than one engine is
tested, average the results and round to the same number of decimal
places contained in the applicable standard, expressed to one additionalsignificant figure.
1.4.1.4. Divide the emissions at the end of the durability period (average emis-
sions, if applicable) for each regulated pollutant by the stabilised
emissions (average emissions, if applicable) and round to two signifi-
cant figures. The resulting number shall be the DF, unless it is less
than 1,00, in which case the DF shall be 1,0.
1.4.1.5. At the manufacturer's option additional emission test points can be
scheduled between the stabilised emission test point and the emission
durability period. If intermediate tests are scheduled, the test points
must be evenly spaced over the EDP (plus or minus two hours) and
one such test point shall be at one half of full EDP (plus or minus two
hours).
For each pollutant HC + NO
xand CO, a straight line must be fitted to
the data pointstreating the initial tes t asoccurring at hour zero, and
using the method of least-squares. The deterioration factor is the calcu-
lated emissions at the end of the durability period divided by the
calculated emissions at zero hours.
1.4.1.6. Calculated deterioration factorsmay cover familiesin addition to the
one on which they were generated if the manufacturer submits a justifi-
cation acceptable to the national type approval authority in advance of
type approval that the affected engine familiescan be reas onably
expected to have similar emission deterioration characteristic based on
the design and technology used.
A non-exclusive list of design and technology groupings is given
below:
— conventional two-stroke engines without after treatment system,
— conventional two-stroke engines with a ceramic catalyst of the same
active material and loading, and the same number of cells per cm2,
— conventional two-stroke engines with a metallic catalyst of the same
active material and loading, same substrate and the same number of
cellsper cm2,
— two-stroke engines provided with a stratified scavenging system,— four-stroke engines with catalyst (defined as above) with same valve
technology and identical lubrication system,
— four-stroke engines without catalyst with the same valve technology
and identical lubrication system.
2. EMISSION DURABILITY PERIODS FOR STAGE 2 ENGINES
2.1. Manufacturerss hall declare the applicable EDP category for each
engine family at the time of type approval. Such category shall be the
category which most closely approximates the expected useful lives of
the equipment into which the enginesare expected to be ins talled as
determined by the engine manufacturer. Manufacturerss hall retain
data appropriate to support their choice of EDP category for each
engine family. Such data shall be supplied to the approval authority
upon request.1997L0068 — EN — 11.02.2003 — 002.001 — 97
▼M2
2.1.1. For hand-held engines: manufacturers shall select an EDP category
from table 1.
Table 1: EDP categoriesfor hand-held engines(hours )
Category 1 2 3
Class SH:1 50 125 300
Class SH:2 50 125 300
Class SH:3 50 125 300
2.1.2. For non-hand-held engines: manufacturers shall select an EDP cate-
gory from table 2.
Table 2: EDP categoriesfor non-hand-held engines(hours )
Category 1 2 3
Class SN:1 50 125 300
Class SN:2 125 250 500Class SN:3 125 250 500Class SN:4 250 500 1 000
2.1.3. The manufacturer must satisfy the approval authority that the declared
useful life is appropriate. Data to support a manufacturer's choice of
EDP category, for a given engine family, may include but are not
limited to:
— surveys of the life spans of the equipment in which the subject
enginesare ins talled,
— engineering evaluationsof field aged enginesto as certain when
engine performance deteriorates to the point where usefulness and/
or reliability is impacted to a degree sufficient to necessitate over-
haul or replacement,
— warranty statements and warranty periods,
— marketing materialsregarding engine life,
— failure reports from engine customers, and— engineering evaluations of the durability, in hours, of specific
engine technologies, engine materials or engine designs.1997L0068 — EN — 11.02.2003 — 002.001 — 98
▼B
ANNEX►M2V◄
TECHNICAL CHARACTERISTICS OF REFERENCE FUEL PRESCRIBED FOR
APPROVALTESTSANDTOVERIFYCONFORMITYOFPRODUCTION
NON-ROAD MOBILE MACHINERY REFERENCE FUEL FOR CI ENGINES (1)
Note:Key properties for engine performance/exhaust emissions are highlighted.
Limitsand units(2) Test method
Cetanenumber (4) minimum 45 (7)
maximum 50ISO 5165
Densityat15ºC minimum 835 kg/m3
maximum 845 kg/m3(10)ISO 3 675, ASTM D 4 052
Distillation (3)
— 95 % pointMaximum 370 ºC ISO 3405
Viscosityat40ºC Minimum 2,5 mm2/s
Maximum 3,5 mm2/sISO 3104
Sulphurcontent Minimum 0,1 % mass (9)
Maximum 0,2 % mass (8)ISO 8754, EN 24260
Flash point Minimum 55 ºC ISO 2719
CFPP Minimum —
Maximum + 5 ºCEN 116
Copper corrosion Maximum 1 ISO 2160
Conradson carbon residue (10 %
DR)Maximum 0,3 % mass ISO 10370
Ash content Maximum 0,01 % mass ASTM D 482 (12)
Water content Maximum 0,05 % mass ASTM D 95, D 1744Neutralization (strong acid)
number►
M1►M2Maximum ◄
0,20 mg KOH/g ◄
Oxidation stability (5) Maximum 2,5 mg/100 ml ASTM D 2274
Additives(6)
Note 1: If it isrequired to calculate thermal efficiency of an engine or vehicle, the calorific value of the fuel can
be calculated from:
Specific energy (calorific value) (net)
MJ/kg = (46,423 − 8,792 · d2+ 3,17 · d) × (1 − (x + y + s)) + 9,42 · s − 2,499 · x
where:d = isthe dens ity at 288 K (15 ºC)
x = isthe proportion by mas sof water (%/100)
y = is the proportion by mass of ash (%/100)s = is the proportion by mass of sulphur (%/100).
Note 2: The values quoted in the specification are ‘true values’. In establishment of their limit values the terms of
ASTM D 3244 ‘Defining a basis for petroleum produce quality disputes’ have been applied and in fixing aminimum value, a minimum difference of 2R above zero hasbeen taken into account; in fixing a
maximum and minimum value, the minimum difference is4R (R = reproducibility).
Notwithstanding this measure, which is necessary for statistical reasons, the manufacturer of fuel should
nevertheless aim at a zero value where the stipulated maximum value is 2R and the mean value in the
case of quotations of maximum and minimum limits. Should it be necessary to clarify the question as towhether a fuel meets the requirements of the specifications, the terms of ASTM D 3244 should be applied.
Note 3: The figures quoted show the evaporated quantities (percentage recovered + percentage loss).
Note 4: The range of cetane isnot in accordance with the requirement of a minimum range of 4R. Hovever, in
cases of dispute between fuel supplier and fuel user, the terms in ASTM D 3244 can be used to resolvesuch disputes provided replicate measurements, of sufficient number to achieve the necessary precision, aremade in preference to single determinations.
Note 5: Even though oxidation stability is controlled, it is likely that shelf life will be limited. Advice should be
sought from the supplier as to storage conditions and life.
Note 6: This fuel should be based straight run and cracked hydrocarbon distillate components only; desulphuriza-
tion is allowed. It must not contain any metallic additives or cetane improver additives.
Note 7: Lower values are permitted, in which case the cetane number of the reference fuel used is to be reported.
Note 8: Higher values are permitted, in which case the sulphur content of the reference fuel used is to be reported.1997L0068 — EN — 11.02.2003 — 002.001 — 99
▼M2
▼B
▼B
Note 9: To be kept under constant review in the light of trends in the markets. ►M1 For the purpose of the
initial approval of an engine with no exhaust gas after treatment on the request of the applicant a
0,05 % mass nominal sulphur level (minimum 0,03 % mass) is permissible, in which case themeasuredparticulatelevelmustbecorrectedupwardtotheaveragevaluethatisnominallyspecifiedforfuelsulphurcontent(0,15%mass)pertheequationbelow: ◄
PT
adj= PT + [SFC × 0,0917 × (NSLF − FSF)]
where:
PTadj= adjusted PT value (g/kWh)
PT = measured weighted specific emission value for particulate emission (g/kWh)
SFC = weighted specific fuel consumption (g/kWh) calculated according to the formula as belowNSLF = average of the nominal specification of sulphur content mass fraction (i.e. 0,15 %/100)FSF = fuel sulphur content mass fraction (%/100)
Equationforthecalculation oftheweightedspecific fuelconsumption:
SFC¼Xn
i¼1Gfuel ;i/C2WFi
Xn
i¼1Pi/C2WFi
where:
Pi=Pm,i+PAE,i
For thepurposeofconformity ofproduction assessmentsinaccordance withsection 5.3.2. of Annex
I,therequirementsmustbemetusingreferencefuelwithasulphurcontentwhichcomplieswiththeminimum/maximumlevel of0,1/0,2%mass.
Note 10: Higher valuesare permitted up to 855 kg/m
3, in which case the density of the reference fuel used is to be
reported.For the purpose of conformity of production assessments in accordance with section 5.3.2.
of Annex I, the requirements must be met using reference fuel which complies with the minimum/
maximumlevelof835/845kg/m3.
Note 11: All fuel characteristics and limit values are to be kept under review in light of trends in the markets.
Note 12: To be replaced by EN/ISO 6245 with effect of the date of implementation.1997L0068 — EN — 11.02.2003 — 002.001 — 100
▼M2
NON-ROAD MOBILE MACHINERY REFERENCE FUEL FOR SI ENGINES
Note:The fuel for two-stroke engines is a blend of lubricant oil and the petrol specified below. The
fuel/oil mixture ratio must be the ratio which is recommended by the manufacturer as specified
in Annex IV, section 2.7.
Parameter UnitLimits(1)
Test method Publication
Minimum Maximum
Research octane
number, RON95,0 — EN 25164 1 993
Motor octane
number, MON85,0 — EN 25 163 1 993
Density at 15 ºC kg/m3748 762 ISO 3675 1 995
Reid vapour pres-
surekPa 56,0 60,0 EN 12 1 993
Distillation —
Initial boiling
pointºC 24 40 EN-ISO
34051 988
— Evaporated at
100 ºC% v/v 49,0 57,0 EN-ISO
34051 988
— Evaporated at
150 ºC% v/v 81,0 87,0 EN-ISO
34051 988
— Final boiling
pointºC 190 215 EN-ISO
34051 988
Residue % — 2 EN-ISO
34051 988
Hydrocarbon
analysis——
— Olefins% v/v — 10 ASTM D
13191 995
— Aromatics% v/v 28,0 40,0 ASTM D
13191 995
— Benzene % v/v — 1,0 EN 12177 1 998
— Saturates% v/v — balance ASTM D
13191 995
Carbon/hydrogen
ratioreport report
Oxidation stability
(2)min. 480 — EN-ISO
75361 996
Oxygen content % m/m — 2, 3 EN 1601 1 997
Existent gum mg/ml — 0,04 EN-ISO
62461 997
Sulphur content mg/kg — 100 EN-ISO
145961 998
Copper corrosion
at 50 ºC— 1 EN-ISO
21601 995
Lead content g/l — 0,005 EN 237 1 996
Phosphorus
contentg/l — 0,0013 ASTM D
32311 994
Note 1: The values quoted in the specification are ‘true values’. In establishment of their limit values
the termsof ISO 4259 ‘Petroleum products— Determination and application of precis ion
data in relation to methodsof tes t’ have been applied and in fixing a minimum value, aminimum difference of 2R above zero hasbeen taken into account; in fixing a maximum
and minimum value, the minimum difference is4R (R = reproducibility). Notwiths tanding
this measure, which is necessary for statistical reasons, the manufacturer of fuels should
nevertheless aim at a zero value where the stipulated maximum value is 2R and at the mean
value in the case of quotations of maximum and minimum limits. Should it be necessary to
clarify the question as to whether a fuel meets the requirements of the specifications, the
termsof ISO 4259 s hould be applied.1997L0068 — EN — 11.02.2003 — 002.001 — 101
▼M2
Note 2: The fuel may contain oxidation inhibitors and metal deactivators normally used to stabilise
refinery gasoline streams, but detergent/dispersive additives and solvent oils must not be
added.1997L0068 — EN — 11.02.2003 — 002.001 — 102
▼B
ANNEX►M2VI◄
1.ANALYTICALANDSAMPLINGSYSTEM
GASEOUS AND PARTICULATE SAMPLING SYSTEMS
Figure Number Description
2 Exhaust gas analysis system for raw exhaust
3 Exhaust gas analysis system for dilute exhaust
4 Partial flow, isokinetic flow, suction blower
control, fractional sampling
5 Partial flow, isokinetic flow, pressure blower
control, fractional sampling
6 Partial flow, CO2or NOxcontrol, fractional
sampling
7 Partial flow, CO2and carbon balance, total
sampling
8 Partial flow, single venturi and concentration
measurement, fractional sampling
9 Partial flow, twin venturi or orifice and concentra-
tion measurement, fractional sampling
10 Partial flow, multiple tube splitting and concentra-
tion measurement, fractional sampling
11 Partial flow, flow control, total sampling
12 Partial flow, flow control, fractional sampling
13 Full flow, positive displacement pump or critical
flow venturi, fractional sampling
14 Particulate sampling system
15 Dilution system for full flow system
1.1.Determinationofthegaseousemissions
Section 1.1.1 and Figures2 and 3 contain detailed des criptionsof the
recommended sampling and analysing systems. Since various config-
urations can produce equivalent results, exact conformance with these
figures is not required. Additional components such as instruments,
valves, solenoids, pumps and switches may be used to provide addi-
tional information and coordinate the functionsof the component
systems. Other components which are not needed to maintain the accu-
racy on some systems, may be excluded if their exclusion is based upon
good engineering judgement.
1.1.1. Gaseous exhaust components CO, CO2, HC, NOx
An analytical system for the determination of the gaseous emissions in
the raw or diluted exhaust gas is described based on the use of:
— HFID analyser for the measurement of hydrocarbons,
— NDIR analysers for the measurement of carbon monoxide and
carbon dioxide,
— HCLD or equivalent analyser for the measurement of nitrogen
oxide.
For the raw exhaust gas (see Figure 2), the sample for all components
may be taken with one sampling probe or with two sampling probes
located in close proximity and internally split to the different analysers.
Care must be taken that no condensation of exhaust components
(including water and sulphuric acid) occurs at any point of the analy-
tical system.
For the diluted exhaust gas (see Figure 3), the sample for the hydrocar-
bons shall be taken with another sampling probe than the sample for the
other components. Care must be taken that no condensation of exhaust
components(including water and s ulphuric acid) occursat any point of
the analytical system.1997L0068 — EN — 11.02.2003 — 002.001 — 103
▼B
Figure 2
FlowdiagramofexhaustgasanalysissystemforCO,NOxandHC
1997L0068 — EN — 11.02.2003 — 002.001 — 104
▼B
Figure 3
Flow diagram of dilute exhaust gas analysis system for CO, CO2,
NOxandHC
Descriptions—Figures2and3
General statement:All components in the sampling gas path must be maintained at the
temperature specified for the respective systems.
—SP1 raw exhaust gas sampling probe (Figure 2 only)
A stainless steel straight closed and multihole probe is recom-
mended. The inside diameter shall not be greater than the inside
diameter of the sampling line. The wall thickness of the probe shall
not be greater than 1 mm. There shall be a minimum of three holes
in three different radial planes sized to sample approximately the
same flow. The probe must extend across at least 80 % of the
diameter of the exhaust pipe.
—SP2 dilute exhaust gas HC sampling probe (Figure 3 only)
The probe shall:
— be defined asthe firs t 254 mm to 762 mm of the hydrocarbon
sampling line (HSL3),
— have a 5 mm minimum inside diameter,— be installed in the dilution tunnel DT (section 1.2.1.2) at a point
where the dilution air and exhaust gas are well mixed (i.e.
approximately 10 tunnel diametersdowns tream of the point
where the exhaust enters the dilution tunnel),
— be sufficiently distant (radially) from other probes and the tunnel
wall so as to be free from the influence of any wakes or eddies,
— be heated so as to increase the gas stream temperature to 463 K
(190 ºC) ± 10 K at the exit of the probe.
—SP3 dilute exhaust gas CO, CO
2,N Oxsampling probe (Figure 3
only)1997L0068 — EN — 11.02.2003 — 002.001 — 105
▼B
The probe shall:
— be in the same plane as SP2,
— be sufficiently distant (radially) from other probes and the tunnel
wall so as to be free from the influence of any wakes or eddies,
— be heated and insulated over its entire length to a minimum
temperature of 328 K (55 ºC) to prevent water condensation.
—HSL1 heated sampling line
The sampling line provides gas sampling from a single probe to the
split point(s) and the HC analyser.
The sampling line shall:
— have a 5 mm minimum and a 13,5 mm maximum inside
diameter,
— be made of stainless steel or PTFE,
— maintain a wall temperature of 463 (190 ºC) ± 10 K as
measured at every separately controlled heated section, if the
temperature of the exhaust gas at the sampling probe is equal
or below 463 K (190 ºC),
— maintain a wall temperature greater than 453 K (180 ºC) if the
temperature of the exhaust gas at the sampling probe is above
463 K (190 ºC),
— maintain a gastemperature of 463 K (190 ºC) ± 10 K immedi-
ately before the heated filter (F2) and the HFID.
—HSL2 heated NOxsampling line
The sampling line shall:
— maintain a wall temperature of 328 to 473 K (55 to 200 ºC) up
to the converter when using a cooling bath, and up to the
analyser when a cooling bath is not used,
— be made of stainless steel or PTFE.
Since the sampling line need only be heated to prevent condensation
of water and sulphuric acid, the sampling line temperature will
depend on the sulphur content of the fuel.
—SL sampling line for CO (CO2)
The line shall be made of PTFE or stainless steel. It may be heated
or unheated.
—BK background bag (optional; Figure 3 only)
For the measurement of the background concentrations.
—BG sample bag (optional; Figure 3 CO and CO2only)
For the measurement of the sample concentrations.
—F1 heated pre-filter (optional)
The temperature shall be the same as HSL1.
—F2 heated filter
The filter shall extract any solid particles from the gas sample prior
to the analyser. The temperature shall be the same as HSL1. The
filter shall be changed as needed.
—P heated sampling pump
The pump shall be heated to the temperature of HSL1.
—HC
Heated flame ionization detector (HFID) for the determination of
the hydrocarbons. The temperature shall be kept at 453 to 473 K
(180 to 200 ºC).
—CO, CO2
NDIR analysers for the determination of carbon monoxide and
carbon dioxide.
—NO2
(H)CLD analyser for the determination of the oxides of nitrogen. If
a HCLD is used it shall be kept at a temperature of 328 to 473 K
(55 to 200 ºC).
—C converter
Aconverter shall be used for the catalytic reduction of NO2to NO
prior to analysis in the CLD or HCLD.
—B cooling bath
To cool and condense water from the exhaust sample. The bath
shall be maintained at a temperature of 273 to 277 K (0 to 4 ºC)
by ice or refrigeration. It isoptional if the analys er isfree from
water vapour interference asdetermined in Annex III, Appendix 3,
sections 1.9.1 and 1.9.2.
Chemical dryersare not allowed for removing water from the
sample.1997L0068 — EN — 11.02.2003 — 002.001 — 106
▼B
—T1, T2, T3 temperature sensor
To monitor the temperature of the gass tream.
—T4 temperature sensor
Temperature of the NO2-NO converter.
—T5 temperature sensor
To monitor the temperature of the cooling bath.
—G1, G2, G3 pressure gauge
To measure the pressure in the sampling lines.
—R1, R2 pressure regulator
To control the pressure of the air and the fuel, respectively, for the
HFID.
—R3, R4, R5 pressure regulator
To control the pressure in the sampling lines and the flow to the
analysers.
—FL1, FL2, FL3 flow-meter
To monitor the sample bypass flow.
—FL4 to FL7 flowmeter (optional)
To monitor the flow rate through the analysers.
—V1 to V6 selector valve
Suitable valving for selecting sample, span gas or zero gas flow to
the analyser.
—V7, V8 solenoid valve
To bypass the NO2-NO converter.
—V9 needle valve
To balance the flow through the NO2-NO converter and the bypass.
—V10, V11 needle valve
To regulate the flows to the analysers.
—V12, V13 toggle valve
To drain the condensate from the bath B.
—V14 selector valve
Selecting the sample or background bag.
1.2.Determinationoftheparticulates
1.2.1 and 1.2.2 and Figures4 to 15 contain detailed des criptionsof the
recommended dilution and sampling systems. Since various configura-
tions can produce equivalent results, exact conformance with these
figures is not required. Additional components such as instruments,
valve, solenoids, pumps and switches may be used to provide additional
information and coordinate the functions of the component systems.
Other componentswhich are not needed to maintain the accuracy on
some systems, may be excluded if their exclusion is based on good
engineering judgement.
1.2.1. Dilution system
1.2.1.1. Partial flow dilution system (Figures 4 to 12)
A dilution system is described based on the dilution of a part of the
exhaust stream. Splitting of the exhaust stream and the following dilu-
tion process may be done by different dilution system types. For
subsequent collection of the particulates, the entire dilute exhaust gas
or only a portion of the dilute exhaust gas may be passed to the parti-
culate sampling system (section 1.2.2, Figure 14). The first method is
referred to as total sampling type , the second method as fractional
sampling type .
The calculation of the dilution ratio depends on the type of system
used.
The following typesare recommended:
—isokinetic systems (Figures4 and 5)
With these systems, the flow into the transfer tube is matched to the
bulk exhaust flow in terms of gas velocity and/or pressure, thus
requiring an undisturbed and uniform exhaust flow at the sampling
probe. This is usually achieved by using a resonator and a straight
approach tube upstream of the sampling point. The split ratio is then
calculated from easily measurable values like tube diameters. It
should be noted that isokinesis is only used for matching the flow
conditions and not for matching the size distribution. The latter is
typically not necessary, as the particles are sufficiently small as to
follow the fluid streamlines,1997L0068 — EN — 11.02.2003 — 002.001 — 107
▼B
—flow controlled systems with concentration measurement (Figures6
to 10)
With these systems, a sample is taken from the bulk exhaust stream
by adjusting the dilution air flow and the total dilution exhaust flow.
The dilution ratio isdetermined from the concentrationsof tracer
gases, such as CO2or NOx, naturally occurring in the engine
exhaust. The concentrations in the dilution exhaust gas and in the
dilution air are measured, whereas the concentration in the raw
exhaust gas can be either measured directly or determined from
fuel flow and the carbon balance equation, if the fuel composition
is known. The systems may be controlled by the calculated dilution
ratio (Figures6 and 7) or by the flow into the trans fer tube (Figures
8, 9 and 10),
—flow controlled systems with flow measurement (Figures11 and 12)
With these systems, a sample is taken from the bulk exhaust stream
by setting the dilution air flow and the total dilution exhaust flow.
The dilution ratio isdetermined from the difference of the two flow
rates. Accurate calibration of the flow-meters relative to one another
isrequired, s ince the relative magnitude of the two flow ratescan
lead to significant errors at higher dilution ratios (Figures 9 and
above). Flow control isvery s traightforward by keeping the dilute
exhaust flow rate constant and varying the dilution air flow rate, if
needed.
In order to realize the advantagesof the partial flow dilution
systems, attention must be paid to avoiding the potential problems
of loss of particulates in the transfer tube, ensuring that a represen-
tative sample is taken from the engine exhaust, and determination of
the split ratio.
The systems described pay attention to these critical areas.1997L0068 — EN — 11.02.2003 — 002.001 — 108
▼B
Figure 4
Partial flow dilution system with isokinetic probe and fractional
sampling(SBcontrol)
Raw exhaust gas is transferred from the exhaust pipe to EP to the dilu-
tion tunnel DT through the transfer tube TT by the isokinetic sampling
probe ISP. The differential pressure of the exhaust gas between exhaust
pipe and inlet to the probe is measured with the pressure transducer
DPT. This signal is transmitted to the flow controller FC1 that controls
the suction blower SB to maintain a differential pressure of zero at the
tip of the probe. Under these conditions, exhaust gas velocities in EP
and ISP are identical, and the flow through ISP and TT isa cons tant
fraction (split) of the exhaust gas flow. The split ratio is determined
from the cross sectional areas of EP and ISP. The dilution air flow
rate is measured with the flow measurement device FM1. The dilution
ratio iscalculated from the dilution air flow rate and the s plit ratio.1997L0068 — EN — 11.02.2003 — 002.001 — 109
▼B
Figure 5
Partial flow dilution system with isokinetic probe and fractional
sampling(PBcontrol)
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the transfer tube TT by the isokinetic sampling
probe ISP. The differential pressure of the exhaust gas between exhaust
pipe and inlet to the probe is measured with the pressure transducer
DPT. This signal is transmitted to the flow controller FC1 that controls
the pressure blower PB to maintain a differential pressure of zero at the
tip of the probe. Thisisdone by taking a s mall fraction of the dilution
air whose flow rate has already been measured with the flow measure-
ment device FM1, and feeding it to TT by meansof a pneumatic
orifice. Under these conditions, exhaust gas velocities in EP and ISP
are identical, and the flow through ISP and TT isa cons tant fraction
(split) of the exhaust gas flow. The split ratio is determined from the
cross sectional areas of EP and ISP. The dilution air is sucked through
DT by the suction blower SB, and the flow rate is measured with FM1
at the inlet to DT. The dilution ratio iscalculated from the dilution air
flow rate and the split ratio.1997L0068 — EN — 11.02.2003 — 002.001 — 110
▼B
Figure 6
Partial flow dilution system with CO2or NOxconcentration
measurementandfractionalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilution
tunnel DT through the sampling probe SP and the transfer tube TT. The
concentrationsof a tracer gas(CO2or NOx) are measured in the raw
and diluted exhaust gas as well as in the dilution air with the exhaust
gas analyser(s) EGA. These signals are transmitted to the flow
controller FC2 that controls either the pressure blower PB or the suction
blower SB to maintain the desired exhaust split and dilution ratio in
DT. The dilution ratio iscalculated from the tracer gasconcentrations
in the raw exhaust gas, the diluted exhaust gas, and the dilution air.1997L0068 — EN — 11.02.2003 — 002.001 — 111
▼B
Figure 7
Partial flow dilution system with CO2concentration measurement,
carbonbalanceandtotalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the sampling probe SP and the transfer tube TT. The
CO
2concentrations are measured in the diluted exhaust gas and in the
dilution air with the exhaust gas analyser(s) EGA. The CO2and fuel
flow GFUELsignals are transmitted either to the flow controller FC2, or
to the flow controller FC3 of the particulate sampling system (see
Figure 14). FC2 controls the pressure blower PB, while FC3 controls
the particulate sampling system (see Figure 14), thereby adjusting the
flows into and out of the system so as to maintain the desired exhaust
split and dilution ratio in DT. The dilution ratio is calculated from the
CO2concentrationsand GFUELusing the carbon balance assumption.1997L0068 — EN — 11.02.2003 — 002.001 — 112
▼B
Figure 8
Partial flow dilution system with single venturi, concentration
measurementandfractionalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the sampling probe SP and the transfer tube TT due
to the negative pressure created by the venturi VN in DT. The gas flow
rate through TT dependson the momentum exchange at the venturi
zone, and istherefore affected by the abs olute temperature of the gas
at the exit of TT. Consequently, the exhaust split for a given tunnel
flow rate isnot cons tant, and the dilution ratio at low load iss lightly
lower than at high load. The tracer gasconcentrations(CO
2or NOx)
are measured in the raw exhaust gas, the diluted exhaust gas, and the
dilution air with the exhaust gas analyser(s) EGA, and the dilution ratio
is calculated from the values so measured.1997L0068 — EN — 11.02.2003 — 002.001 — 113
▼B
Figure 9
Partialflowdilutionsystemtwinventuriortwinorifice, concentra-
tionmeasurementandfractionalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the sampling probe SP and the transfer tube TT by a
flow divider that contains a set of orifices or venturis. The first one
(FD1) islocated in EP, the s econd one (FD2) in TT. Additionally, two
pressure control valves (PCV1 and PCV2) are necessary to maintain a
constant exhaust split by controlling the backpressure in EP and the
pressure in DT. PCV1 is located downstream of SP in EP, PCV2
between the pressure blower PB and DT. The tracer gas concentrations
(CO
2or NOx) are measured in the raw exhaust gas, the diluted exhaust
gas, and the dilution air with the exhaust gas analyser(s) EGA. They are
necessary for checking the exhaust split, and may be used to adjust
PCV1 and PCV2 for precise split control. The dilution ratio is calcu-
lated from the tracer gasconcentrations .1997L0068 — EN — 11.02.2003 — 002.001 — 114
▼B
Figure 10
Partial flowdilutionsystemwithmultipletubesplitting,concentra-
tionmeasurementandfractionalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the transfer tube TT by the flow divider FD3 that
consists of a number of tubes of the same dimensions (same diameter,
length and bed radius) installed in EP. The exhaust gas through one of
these tubes is lead to DT, and the exhaust gas through the rest of the
tubes is passed through the damping chamber DC. Thus, the exhaust
split is determined by the total number of tubes. A constant split control
requires a differential pressure of zero between DC and the outlet of
TT, which is measured with the differential pressure transducer DPT.
A differential pressure of zero is achieved by injecting fresh air into
DT at the outlet of TT. The tracer gasconcentrations(CO
2or NOx)
are measured in the raw exhaust gas, the diluted exhaust gas, and the
dilution air with the exhaust gas analyser(s) EGA. They are necessary
for checking the exhaust split and may be used to control the injection
air flow rate for precise split control. The dilution ratio is calculated
from the tracer gasconcentrations .1997L0068 — EN — 11.02.2003 — 002.001 — 115
▼B
Figure 11
Partial flowdilutionsystemwithflowcontrolandtotalsampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilution
tunnel DT through the sampling probe SP and the transfer tube TT. The
total flow through the tunnel isadjus ted with the flow controller FC3
and the sampling pump P of the particulate sampling system (see Figure
16). The dilution air flow iscontrolled by the flow controller FC2,
which may use GEXH,GAIRor GFUELas command signals, for the desired
exhaust split. The sample flow into DT is the difference of the total
flow and the dilution air flow. The dilution air flow rate ismeas ured
with flow measurement device FM1, the total flow rate with the flow
measurement device FM3 of the particulate sampling system (see
Figure 14). The dilution ratio is calculated from these two flow rates.1997L0068 — EN — 11.02.2003 — 002.001 — 116
▼B
Figure 12
Partial flow dilution system with flow control and fractional
sampling
Raw exhaust gas is transferred from the exhaust pipe EP to the dilutiontunnel DT through the sampling probe SP and the transfer tube TT. The
exhaust split and the flow into DT is controlled by the flow controller
FC2 that adjusts the flows (or speeds) of the pressure blower PB and
the suction blower SB, accordingly. This is possible since the sample
taken with the particulate sampling system is returned into DT. G
EXH,
GAIRor GFUELmay be used as command signals for FC2. The dilution
air flow rate is measured with the flow measurement device FM1, the
total flow with the flow measurement device FM2. The dilution ratio is
calculated from these two flow rates.
Description—Figures4to12
—EP exhaust pipe
The exhaust pipe may be insulated. To reduce the thermal inertia of
the exhaust pipe a thickness to diameter ratio of 0,015 or less is
recommended. The use of flexible sections shall be limited to a
length to diameter ratio of 12 or less. Bends will be minimized to
reduce inertial deposition. If the system includes a test bed silencer,
the silencer may also be insulated.
For an isokinetic system, the exhaust pipe must be free of elbows,
bends and sudden diameter changes for at least six pipe diameters
upstream and three pipe diameters downstream of the tip of the
probe. The gas velocity at the sampling zone must be higher than
10 m/s except at idle mode. Pressure oscillations of the exhaust
gas must not exceed ± 500 Pa on the average. Any steps to reduce
pressure oscillations beyond using a chassis-type exhaust system
(including silencer and after-treatment device) must not alter engine
performance nor cause the deposition of particulates.
For systems without isokinetic probes, it is recommended to have a
straight pipe of six pipe diameters upstream and three pipe
diametersdowns tream of the tip of the probe.
—SP sampling probe (Figures6 to 12)1997L0068 — EN — 11.02.2003 — 002.001 — 117
▼B
The minimum inside diameter shall be 4 mm. The minimum
diameter ratio between exhaust pipe and probe shall be four. The
probe shall be an open tube facing upstream on the exhaust pipe
centre-line, or a multiple hole probe asdes cribed under SP1 in
section 1.1.1.
—ISP isokinetic sampling probe (Figures4 and 5)
The isokinetic sampling probe must be installed facing upstream on
the exhaust pipe centre-line where the flow conditions in section EP
are met, and designed to provide a proportional sample of the raw
exhaust gas. The minimum inside diameter shall be 12 mm.
A control system is necessary for isokinetic exhaust splitting by
maintaining a differential pressure of zero between EP and ISP.
Under these conditions exhaust gas velocities in EP and ISP are
identical and the mass flow through ISP is a constant fraction of
the exhaust gas flow. The ISP has to be connected to a differential
pressure transducer. The control to provide a differential pressure of
zero between EP and ISP isdone with blower s peed or flow
controller.
—FD1, FD2 flow divider (Figure 9)
A set of venturis or orifices is installed in the exhaust pipe EP and
in the transfer tube TT, respectively, to provide a proportional
sample of the raw exhaust gas. A control system consisting of two
pressure control valves PCV1 and PCV2 is necessary for propor-
tional splitting by controlling the pressures in EP and DT.
—FD3 flow divider (Figure 10)
A set of tubes (multiple tube unit) is installed in the exhaust pipe
EP to provide a proportional sample of the raw exhaust gas. One
of the tubesfeedsexhaus t gasto the dilution tunnel DT, whereas
the other tubesexit exhaus t gasto a damping chamber DC. The
tubes must have the same dimensions (same diameter, length, bend
radius), so that the exhaust split depends on the total number of
tubes. A control system is necessary for proportional splitting by
maintaining a differential pressure of zero between the exit of the
multiple tube unit into DC and the exit of TT. Under these condi-
tions, exhaust gas velocities in EP and FD3 are proportional, and
the flow TT is a constant fraction of the exhaust gas flow. The
two points have to be connected to a differential pressure transducer
DPT. The control to provide a differential pressure of zero is done
with the flow controller FC1.
—EGA exhaust gas analyser (Figures6 to 10)
CO2or NOxanalysers may be used (with carbon balance method
CO2only). The analysers shall be calibrated like the analysers for
the measurement of the gaseous emissions. One or several analysers
may be used to determine the concentration differences.
The accuracy of the measuring systems has to be such that the accu-
racy of GEDFW,ior VEDFW,iiswithin ± 4 %.
—TT transfer tube (Figures4 to 12)
The particulate sample transfer tube shall be:
— as short as possible, but not more than 5 m in length,
— equal to or greater than the probe diameter, but not more than
25 mm in diameter,
— exiting on the centre-line of the dilution tunnel and pointing
down-stream.
If the tube is 1 metre or less in length, it is to be insulated with
material with a maximum thermal conductivity of 0,05 W/(m · K)
with a radial insulation thickness corresponding to the diameter of
the probe. If the tube is longer than 1 metre, it must be insulated
and heated to a minimum wall temperature of 523 K (250 ºC).
Alternatively, the transfer tube wall temperatures required may be
determined through standard heat transfer calculations.
—DPT differential pressure transducer (Figures4, 5 and 10)
The differential pressure transducer shall have a range of ± 500 Pa
or less.
—FC1 flow controller (Figures4, 5 and 10)
For the isokinetic systems (Figures 4 and 5) a flow controller is
necessary to maintain a differential pressure of zero between EP
and ISP. The adjustment can be done by:
(a) controlling the speed or flow of the suction blower (SB) and
keeping the speed of the pressure blower (PB) constant during
each mode (Figure 4);
or1997L0068 — EN — 11.02.2003 — 002.001 — 118
▼B
(b) adjusting the suction blower (SB) to a constant mass flow of the
diluted exhaust and controlling the flow of the pressure blower
PB, and therefore the exhaust sample flow in a region at the end
of the transfer tube (TT) (Figure 5).
In the case of a pressure controlled system the remaining error in
the control loop must not exceed ± 3 Pa. The pressure oscillations
in the dilution tunnel must not exceed ± 250 Pa on average.
For a multi-tube system (Figure 10) a flow controller is necessary
for proportional exhaust splitting to maintain a differential pressure
of zero between the outlet of the multi-tube unit and the exit of TT.
The adjustment can be done by controlling the injection air flow
rate into DT at the exit of TT.
—PCV1, PCV2 pressure control valve (Figure 9)
Two pressure control valves are necessary for the twin venturi/twin
orifice system for proportional flow splitting by controlling the
backpressure of EP and the pressure in DT. The valves shall belocated downstream of SP in EP and between PB and DT.
—DC damping chamber (Figure 10)
A damping chamber shall be installed at the exit of the multiple
tube unit to minimize the pressure oscillations in the exhaust pipe
EP.
—VN venturi (Figure 8)
A venturi isins talled in the dilution tunnel DT to create a negative
pressure in the region of the exit of the transfer tube TT. The gas
flow rate through TT isdetermined by the momentum exchange at
the venturi zone, and isbas ically proportional to the flow rate of the
pressure blower PB leading to a constant dilution ratio. Since the
momentum exchange isaffected by the temperature at the exit of
TT and the pressure difference between EP and DT, the actual dilu-
tion ratio iss lightly lower at low load than at high load.
—FC2 flow controller (Figures6, 7, 11 and 12; optional)
A flow controller may be used to control the flow of the pressure
blower PB and/or the suction blower SB. It may be connected to
the exhaust flow or fuel flow signal and/or to the CO
2or NOxdiffer-
ential signal.
When using a pressurized air supply (Figure 11) FC2 directly
controlsthe air flow.
—FM1 flow measurement device (Figures6, 7, 11 and 12)
Gas meter or other flow instrumentation to measure the dilution air
flow. FM1 isoptional if PB iscalibrated to meas ure the flow.
—FM2 flow measurement device (Figure 12)
Gas meter or other flow instrumentation to measure the diluted
exhaust gas flow. FM2 is optional if the suction blower SB is cali-
brated to measure the flow.
—PB pressure blower (Figures4, 5, 6, 7, 8, 9 and 12)
To control the dilution air flow rate, PB may be connected to the
flow controllersFC1 or FC2. PB isnot required when us ing a
butterfly valve. PB may be used to measure the dilution air flow,
if calibrated.
—SB suction blower (Figures4, 5, 6, 9, 10 and 12)
For fractional sampling systems only. SB may be used to measure
the dilute exhaust gas flow, if calibrated.
—DAF dilution air filter (Figures4 to 12)
It isrecommended that the dilution air be filtered and charcoal
scrubbed to eliminate background hydrocarbons. The dilution air
shall have a temperature of 298 K (25 ºC) ± 5 K.
At the manufacturer's request the dilution air shall be sampled
according to good engineering practice to determine the background
particulate levels, which can then be subtracted from the values
measured in the diluted exhaust.
—PSP particulate sampling probe (Figures4, 5, 6, 8, 9, 10 and 12)
The probe isthe leading s ection of PTT and
— shall be installed facing upstream at a point where the dilution
air and exhaust gas are well mixed, i.e. on the dilution tunnel
DT centre-line of the dilution systems approximately 10 tunnel
diameters downstream of the point where the exhaust enters the
dilution tunnel,
— shall be 12 mm in minimum inside diameter,— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the1997L0068 — EN — 11.02.2003 — 002.001 — 119
▼B
air temperature doesnot exceed 325 K (52 ºC) prior to the intro-
duction of the exhaust in the dilution tunnel,
— may be insulated.
—DT dilution tunnel (Figures4 to 12)
The dilution tunnel:
— shall be of a sufficient length to cause complete mixing of the
exhaust and dilution air under turbulent flow conditions,
— shall be constructed of stainless steel with:
— a thickness to diameter ratio of 0,025 or less for dilution
tunnelsof greater than 75 mm ins ide diameter,
— a nominal wall thickness of not less than 1,5 mm for dilution
tunnels of equal to or less than 75 mm inside diameter,
— shall be at least 75 mm in diameter for the fractional sampling
type,
— isrecommended to be at leas t 25 mm in diameter for the total
sampling type.
May be heated to no greater than 325 K (52 ºC) wall temperature by
direct heating or by dilution air pre-heating, provided the air
temperature doesnot exceed 325 K (52 ºC) prior to the introduction
of the exhaust in the dilution tunnel.
May be insulated.
The engine exhaust shall be thoroughly mixed with the dilution air.
For fractional sampling systems, the mixing quality shall be
checked after introduction into service by means of a CO2profile
of the tunnel with the engine running (at least four equally spaced
measuring points). If necessary, a mixing orifice may be used.
Note:If the ambient temperature in the vicinity of the dilution
tunnel (DT) isbelow 293 K (20 ºC), precautionss hould be
taken to avoid particle losses onto the cool walls of the dilu-
tion tunnel. Therefore, heating and/or insulating the tunnel
within the limitsgiven above isrecommended.
At high engine loads, the tunnel may be cooled by a non-aggressive
meanss uch asa circulating fan, aslong asthe temperature of the
cooling medium isnot below 293 K (20 ºC).
—HE heat exchanger (Figures9 and 10)
The heat exchanger shall be of sufficient capacity to maintain the
temperature at the inlet to the suction blower SB within ± 11 K of
the average operating temperature observed during the test.
1.2.1.2. Full flow dilution system (Figure 13)
A dilution system is described based upon the dilution of the total
exhaust using the constant volume sampling (CVS) concept. The total
volume of the mixture of exhaust and dilution air must be measured.
Either a PDP or a CFV system may be used.
For subsequent collection of the particulates, a sample of the dilute
exhaust gas is passed to the particulate sampling system (section 1.2.2,
Figures14 and 15). If thisisdone directly, it isreferred to ass ingle
dilution. If the sample is diluted once more in the secondary dilution
tunnel, it isreferred to asdouble dilution. Thisisus eful, if the filter
face temperature requirement cannot be met with single dilution.
Although partly a dilution system, the double dilution system is
described as a modification of a particulate sampling system in section
1.2.2, Figure 15, since it shares most of the parts with a typical particu-
late sampling system.
The gaseous emissions may also be determined in the dilution tunnel of
a full flow dilution system. Therefore, the sampling probes for the
gaseous components are shown in Figure 13 but do not appear in the
description list. The respective requirements are described in section
1.1.1.
Description:—Figure13—EP exhaust pipe
The exhaust pipe length from the exit of the engine exhaust mani-
fold, turbocharger outlet or after-treatment device to the dilution
tunnel is required to be not more than 10 m. If the system exceeds
4 m in length, then all tubing in excess of 4 m shall be insulated,
except for an in-line smoke-meter, if used. The radial thickness of
the insulation must be at least 25 mm. The thermal conductivity of
the insulating material must have a value no greater than 0,1 W/(m ·
K) measured at 673 K (400 ºC). To reduce the thermal inertia of the
exhaust pipe a thickness to diameter ratio of 0,015 or less is recom-1997L0068 — EN — 11.02.2003 — 002.001 — 120
▼B
mended. The use of flexible sections shall be limited to a length to
diameter ratio of 12 or less.1997L0068 — EN — 11.02.2003 — 002.001 — 121
▼B
Figure 13
Fullflowdilutionsystem
The total amount of raw exhaust gas is mixed in the dilution tunnel DT
with the dilution air.
The diluted exhaust gas flow rate is measured either with a positive
displacement pump PDP or with a critical flow venturi CFV. A heat
exchanger HE or electronic flow compensation EFC may be used for
proportional particulate sampling and for flow determination. Since
particulate mass determination is based on the total diluted exhaust gas
flow, the dilution ratio isnot required to be calculated.
—PDP positive displacement pump
The PDP meterstotal diluted exhaus t flow from the number of the
pump revolutions and the pump displacement. The exhaust system
back pressure must not be artificially lowered by the PDP or dilu-
tion air inlet system. Static exhaust back pressure measured with the
CVS system operating shall remain within ± 1,5 kPa of the static
pressure measured without connection to the CVS at identical
engine speed and load.
The gasmixture temperature immediately ahead of the PDP s hall be
within ± 6 K of the average operating temperature observed during
the test, when no flow compensation is used.
Flow compensation can only be used if the temperature at the inlet
of the PDP doesnot exceed 50 ºC (323 K).
—CFV critical flow venturi
CFV measures total diluted exhaust flow by maintaining the flow at
choked conditions (critical flow). Static exhaust backpressure
measured with the CFV system operating shall remain within ± 1,5
kPa of the static pressure measured without connection to the CFV
at identical engine speed and load. The gas mixture temperature
immediately ahead of the CFV shall be within ± 11 K of the
average operating temperature observed during the test, when no
flow compensation is used.
—HE heat exchanger (optional if EFC isus ed)1997L0068 — EN — 11.02.2003 — 002.001 — 122
▼B
The heat exchanger shall be of sufficient capacity to maintain the
temperature within the limitsrequired above.
—EFC electronic flow compensation (optional if HE isus ed)
If the temperature at the inlet to either the PDP or CFV isnot kept
within the limits stated above, a flow compensation system is
required for continuousmeas urement of the flow rate and control
of the proportional sampling in the particulate system.
To that purpose, the continuously measured flow rate signals are
used to correct the sample flow rate through the particulate filters
of the particulate sampling system (see Figures 14 and 15), accord-ingly.
—DT dilution tunnel
The dilution tunnel:
— shall be small enough in diameter to cause turbulent flow
(Reynoldsnumber greater than 4 000) of s ufficient length to
cause complete mixing of the exhaust and dilution air. A mixing
orifice may be used,
— shall be at least 75 mm in diameter,
— may be insulated.
The engine exhaust shall be directed downstream at the point where
it isintroduced into the dilution tunnel, and thoroughly mixed.
When using single dilution , a sample from the dilution tunnel is
transferred to the particulate sampling system (section 1.2.2, Figure
14). The flow capacity of the PDP or CFV must be sufficient tomaintain the diluted exhaust at a temperature of less than or equal
to 325 K (52 ºC) immediately before the primary particulate filter.
When using double dilution , a sample from the dilution tunnel is
transferred to the secondary dilution tunnel where it is further
diluted, and then passed through the sampling filters (section 1.2.2,
Figure 15).
The flow capacity of the PDP or CFV must be sufficient to maintain
the diluted exhaust stream in the DT at a temperature of less than or
equal to 464 K (191 ºC) at the sampling zone. The secondary dilu-
tion system must provide sufficient secondary dilution air to
maintain the doubly-diluted exhaust stream at a temperature of less
than or equal to 325 K (52 ºC) immediately before the primary
particulate filter.
—DAF dilution air filter
It isrecommended that the dilution air be filtered and charcoal
scrubbed to eliminate background hydrocarbons. The dilution air
shall have a temperature of 298 K (25 ºC) ± 5 K. At the manufac-
turer's request the dilution air shall be sampled according to good
engineering practice to determine the background particulate levels,
which can then be subtracted from the values measured in the
diluted exhaust.
—PSP particulate sampling probe
The probe isthe leading s ection of PTT and
— shall be installed facing upstream at a point where the dilution
air and exhaust gas are well mixed, i.e. on the dilution tunnel
DT centre-line of the dilution systems approximately 10 tunnel
diameters downstream of the point where the exhaust enters the
dilution tunnel,
— shall be 12 mm in minimum inside diameter,
— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the
air temperature doesnot exceed 325 K (52 ºC) prior to the intro-
duction of the exhaust in the dilution tunnel,
— may be insulated.
1.2.2. Particulate sampling system (Figures14 and 15)
The particulate sampling system is required for collecting the particu-
lates on the particulate filter. In the case of total sampling partial flow
dilution, which consists of passing the entire dilute exhaust sample
through the filters, dilution (section 1.2.1.1, Figures 7 and 11) and
sampling system usually form an integral unit. In the case of fractional
sampling partial flow dilution or full flow dilution, which consists of
passing through the filters only a portion of the diluted exhaust, the
dilution (section 1.2.1.1, Figures 4, 5, 6, 8, 9, 10 and 12 and section
1.2.1.2, Figure 13) and sampling systems usually form different units.
In this Directive, the double dilution system DDS (Figure 15) of a full
flow dilution system is considered as a specific modification of a
typical particulate sampling system as shown in Figure 14. The double1997L0068 — EN — 11.02.2003 — 002.001 — 123
▼B
dilution system includes all important parts of the particulate sampling
system, like filter holders and sampling pump, and additionally some
dilution features, like a dilution air supply and a secondary dilution
tunnel.
In order to avoid any impact on the control loops, it is recommended
that the sample pump be running throughout the complete test proce-
dure. For the single filter method, a bypass system shall be used for
passing the sample through the sampling filters at the desired times.
Interference of the switching procedure on the control loops must be
minimized.
Descriptions—Figures14and15—PSP particulate sampling probe (Figures14 and 15)
The particulate sampling probe shown in the figures is the leading
section of the particulate transfer tube PTT.
The probe:
— shall be installed facing upstream at a point where the dilution
air and exhaust gas are well mixed, i.e. on the dilution tunnel
DT centre-line of the dilution systems (see section 1.2.1),
approximately 10 tunnel diametersdowns tream of the point
where the exhaust enters the dilution tunnel),
— shall be 12 mm in minimum inside diameter,— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the
air temperature doesnot exceed 325 K (52 ºC) prior to the intro-
duction of the exhaust in the dilution tunnel,
— may be insulated.1997L0068 — EN — 11.02.2003 — 002.001 — 124
▼B
Figure 14
Particulate samplingsystem
A sample of the diluted exhaust gas is taken from the dilution tunnel
DT of a partial flow or full flow dilution system through the particulate
sampling probe PSP and the particulate transfer tube PTT by means of
the sampling pump P. The sample is passed through the filter holders(s)
FH that contain the particulate sampling filters. The sample flow rate is
controlled by the flow controller FC3. If electronic flow compensation
EFC (see Figure 13) is used, the diluted exhaust gas flow is used as
command signal for FC3.1997L0068 — EN — 11.02.2003 — 002.001 — 125
▼B
Figure 15
Dilutionsystem(fullflowsystemonly)
A sample of the diluted exhaust gas is transferred from the dilution
tunnel DT of a full flow dilution system through the particulate
sampling probe PSP and the particulate transfer tube PTT to the
secondary dilution tunnel SDT, where it is diluted once more. The
sample is then passed through the filter holder(s) FH that contain the
particulate sampling filters. The dilution air flow rate is usuallyconstant whereas the sample flow rate is controlled by the flow
controller FC3. If electronic flow compensation EFC (see Figure 13) is
used, the total diluted exhaust gas flow is used as command signal for
FC3.
—PTT particulate transfer tube (Figures14 and 15)
The particulate transfer tube must not exceed 1 020 mm in length,
and must be minimized in length whenever possible.
The dimensions are valid for:
— the partial flow dilution fractional sampling type and the full
flow single dilution system from the probe tip to the filter
holder,
— the partial flow dilution total sampling type from the end of the
dilution tunnel to the filter holder,
— the full flow double dilution system from the probe tip to the
secondary dilution tunnel.
The transfer tube:
— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the
air temperature doesnot exceed 325 K (52 ºC) prior to the intro-
duction of the exhaust in the dilution tunnel,
— may be insulated.
—SDT secondary dilution tunnel (Figure 15)
The secondary dilution tunnel should have a minimum diameter of
75 mm and should be sufficient length so as to provide a residence
time of at least 0,25 seconds for the doubly-diluted sample. The1997L0068 — EN — 11.02.2003 — 002.001 — 126
▼B
primary filter holder, FH, shall be located within 300 mm of the
exit of the SDT.
The secondary dilution tunnel:
— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the
air temperature doesnot exceed 325 K (52 ºC) prior to the intro-
duction of the exhaust in the dilution tunnel,
— may be insulated.
—FH filter holder(s) (Figures14 and 15)
For primary and back-up filters one filter housing or separate filter
housings may be used. The requirements of Annex III, Appendix 1,
section 1.5.1.3 have to be met.
The filter holder(s):
— may be heated to no greater than 325 K (52 ºC) wall tempera-
ture by direct heating or by dilution air pre-heating, provided the
air temperature doesnot exceed 325 K (52 ºC),
— may be insulated.
—P sampling pump (Figures14 und 15)
The particulate sampling pump shall be located sufficiently distant
from the tunnel so that the inlet gas temperature is maintained
constant (± 3 K), if flow correction by FC3 is not used.
—DP dilution air pump (Figure 15) (full flow double dilution only)
The dilution air pump shall be located so that the secondary dilution
air iss upplied at a temperature of 298 K (25 ºC) ± 5 K.
—FC3 flow controller (Figures14 und 15)
A flow controller shall be used to compensate the particulate sample
flow rate for temperature and backpressure variations in the sample
path, if no other meansare available. The flow controller isrequired
if electronic flow compensation EFC (see Figure 13) is used.
—FM3 flow measurement device (Figures14 und 15) (particulate
sample flow)
The gas meter or flow instrumentation shall be located sufficiently
distant from the sample pump so that the inlet gas temperature
remains constant (± 3 K), if flow correction by FC3 is not used.
—FM4 flow measurement device (Figure 15) (dilution air, full flow
double dilution only)
The gas meter or flow instrumentation shall be located so that the
inlet gastemperature remainsat 298 K (25 ºC) ± 5 K.
—BV ball valve (optional)
The ball valve shall have a diameter not less than the inside
diameter of the sampling tube and a switching time of less than
0,5 seconds.
Note:If the ambient temperature in the vicinity of PSP, PTT, SDT,
and FH isbelow 239 K (20 ºC), precautionss hould be taken
to avoid particle losses onto the cool wall of these parts.
Therefore, heating and/or insulating these parts within the
limits given in the respective descriptions is recommended.
It isals o recommended that the filter face temperature during
sampling be not below 293 K (20 ºC).
At high engine loads, the above parts may be cooled by a non-
aggressive means such as a circulating fan, as long as the tempera-
ture of the cooling medium isnot below 293 K (20 ºC).1997L0068 — EN — 11.02.2003 — 002.001 — 127
▼B
ANNEX►M2VII◄
1997L0068 — EN — 11.02.2003 — 002.001 — 128
▼B
1997L0068 — EN — 11.02.2003 — 002.001 — 129
▼B
Appendix 1
►(1) (2) (3)M21997L0068 — EN — 11.02.2003 — 002.001 — 130
▼B
►(1)M21997L0068 — EN — 11.02.2003 — 002.001 — 131
▼M2
Appendix 2
TESTRESULTSFORSPARKIGNITIONENGINES
1. INFORMATION CONCERNING THE CONDUCT OF THE
TEST(S) (1):
1.1.Octanenumber
1.1.1. Octane number:1.1.2. State percentage of oil in mixture when lubricant and petrol are mixed as
in the case of two-stroke engines
1.1.3. Density of petrol for four-stroke engines and petrol/oil mixture for two-
stroke engines
1.2.Lubricant
1.2.1. Make(s)1.2.2. Type(s)
1.3.Enginedrivenequipment(ifapplicable)
1.3.1. Enumeration and identifying details
1.3.2. Power absorbed at indicated engine speed (as specified by the manufac-
turer)
EquipmentPower PAE(kW) absorbed at various engine speeds (*),
taking into account Appendix 3 of thisAnnex
Equipment Rated
Total
(*) Must not be greater than 10 % of the power measured during the test.
1.4.Engineperformance
1.4.1. Engine speeds:
Idle: min−1
Intermediate: min−1
Rated: min−1
1.4.2. Engine power (2)
ConditionPower setting (kW) at various engine speeds
Intermediate (if applic-
able)Rated
Maximum power measured on test (PM) (kW) (a)
Total power absorbed by engine driven equip-
ment asper s ection 1.3.2 of thisAppendix, or
section 2.8 of Annex III (PAE) (kW) (b)
Net engine power as specified in section 2.4 of
Annex I (kW) (c)
c=a+b1997L0068 — EN — 11.02.2003 — 002.001 — 132
(1) In case of several parent engines, to be indicated for each of them.
(2) Uncorrected power measured in accordance with the provisions of section 2.4 of Annex
I.
▼M2
1.5.Emissionlevels
1.5.1. Dynamometer setting (kW)
Percent LoadDynamometer setting (kW) at various engine speeds
Intermediate (if applic-
able)Rated (if applicable)
10 (if applicable)
25 (if applicable)
5075100
1.5.2. Emission results on the test cycle:
CO: g/kWh
HC: g/kWhNO
x: g/kWh1997L0068 — EN — 11.02.2003 — 002.001 — 133
▼M2
Appendix 3
EQUIPMENT AND AUXILIARIES TO BE INSTALLED FOR THE TEST TO DETERMINE
ENGINEPOWER
Numb-
erEquipment and auxiliaries Fitted for emission test
1 Inlet system
Inlet manifold Yes, standard production equipment
Crankcase emission control system Yes, standard production equipment
Control devicesfor dual induction inlet
manifold systemYes, standard production equipment
Air flow meter Yes, standard production equipment
Air inlet duct work Yes(a)
Air filter Yes(a)
Inlet silencer Yes (a)
Speed-limiting device Yes(a)
2 Induction-heating device of inlet manifold Yes, standard production equipment. If
possible to be set in the most favourable
condition
3 Exhaust system
Exhaust purifier Yes, standard production equipment
Exhaust manifold Yes, standard production equipmentConnecting pipesYes (
b)
Silencer Yes(b)
Tail pipe Yes(b)
Exhaust brake No (c)
Pressure charging device Yes, standard production equipment
4 Fuel supply pump Yes, standard production equipment (d)
5 Carburation equipment
Carburettor Yes, standard production equipment
Electronic control system, air flow meter,
etc.Yes, standard production equipment
Equipment for gasengines
Pressure reducer Yes, standard production equipment
Evaporator Yes, standard production equipment
Mixer Yes, standard production equipment
6 Fuel injection equipment (petrol and
diesel)
Prefilter Yes, standard production or test bed equip-
ment
Filter Yes, standard production or test bed equip-
ment
Pump Yes, standard production equipment
High-pressure pipe Yes, standard production equipment
Injector Yes, standard production equipment
Air inlet valve Yes, standard production equipment (e)
Electronic control system, air flow meter,
etc.Yes, standard production equipment
Governor/control system Yes, standard production equipment
Automatic full-load stop for the control Yes, standard production equipment1997L0068 — EN — 11.02.2003 — 002.001 — 134
▼M2
Numb-
erEquipment and auxiliaries Fitted for emission test
rack depending on atmospheric conditions
7 Liquid-cooling equipment
Radiator No
Fan No
Fan cowl No
Water pump Yes, standard production equipment (f)
Thermostat Yes, standard production equipment (g)
8 Air cooling
Cowl No (h)
Fan or Blower No (h)
Temperature-regulating device No
9 Electrical equipment
Generator Yes, standard production equipment (i)
Spark distribution system Yes, standard production equipment
Coil or coils Yes, standard production equipment
Wiring Yes, standard production equipment
Spark plugs Yes, standard production equipmentElectronic control system including knock
sensor/spark retard systemYes, standard production equipment
10 Pressure charging equipment
Compressor driven either directly by the
engine and/or by the exhaust gasesYes, standard production equipment
Charge air cooler Yes, standard production or test bed equip-
ment (
j)(k)
Coolant pump or fan (engine-driven) No (h)
Coolant flow control device Yes, standard production equipment
11 Auxiliary test-bed fan Yes, if necessary
12 Anti-pollution device Yes, standard production equipment (l)
13 Starting equipment Test bed equipment14 Lubricating oil pump Yes, standard production equipment
(a) The complete inlet system shall be fitted as provided for the intended application:
where there isa ris k of an appreciable effect on the engine power;
in the case of naturally aspirated spark ignition engines;when the manufacturer requests that this should be done.
In other cases, an equivalent system may be used and a check should be made to ascertain that the intake pres-
sure does not differ by more than 100 Pa from the upper limit specified by the manufacturer for a clean air
filter.
(
b) The complete exhaust system shall be fitted as provided for the intended application:
where there isa ris k of an appreciable effect on the engine power;
in the case of naturally aspirated spark ignition engines;
when the manufacturer requests that this should be done.
In other cases, an equivalent system may be installed provided the pressure measured does not differ by more
than 1 000 Pa from the upper limit specified by the manufacturer.
(c) If an exhaust brake is incorporated in the engine, the throttle valve shall be fixed in the fully open position.
(d) The fuel feed pressure may be adjusted, if necessary, to reproduce the pressure existing in the particular engine
application (particularly when a ‘fuel return’ system is used).
(e) The air intake valve isthe control valve for the pneumatic governor of the injection pump. The governor or the
fuel injection equipment may contain other deviceswhich may affect the amount of injected fuel.
(f) The cooling-liquid circulation shall be operated by the engine water pump only. Cooling of the liquid may be
produced by an external circuit, such that the pressure loss of this circuit and the pressure at the pump inletremain substantially the same as those of the engine cooling system.
(
g) The thermostat may be fixed in the fully open position.1997L0068 — EN — 11.02.2003 — 002.001 — 135
▼M2
(h) When the cooling fan or blower is fitted for the test, the power absorbed shall be added to the results, except for
cooling fans of air cooled engines directly fitted on the crankshaft. The fan or blower power shall be determined
at the speeds used for the test either by calculation from standard characteristics or by practical tests.
(i) Minimum power of the generator: the electrical power of the generator shall be limited to that necessary for
operation of accessories which are indispensable for engine operation. If the connection of a battery is necessary,a fully charged battery in good condition shall be used.
(
j) Charge air-cooled engines shall be tested with charge air cooling, whether liquid- or air-cooled, but if the manu-
facturer prefers, a test bench system may replace the air cooler. In either case, the measurement of power at eachspeed shall be made with the maximum pressure drop and the minimum temperature drop of the engine airacross the charge air cooler on the test bench system as specified by the manufacturer.
(
k) These may include, for example, exhaust-gas recirculation (EGR)-system, catalytic converter, thermal reactor,
secondary air-supply system and fuel evaporation protecting system.
(l) The power for electrical or other starting systems shall be provided from the test bed.1997L0068 — EN — 11.02.2003 — 002.001 — 136
▼B
ANNEX►M2VIII◄
APPROVALCERTIFICATENUMBERINGSYSTEM
(see Article 4 (2))
1. The number shall consist of five sections separated by the ‘*’ character.
Section 1: the lower case letter ‘e’followed by the distinguishing letter(s) or
number of the Member State issuing the approval:
1 for Germany
2 for France
3 for Italy
4 for the Netherlands5 for Sweden
6 for Belgium
9 for Spain11 for the United Kingdom12 for Austria
13 for Luxembourg
17 for Finland18 for Denmark
21 for Portugal
23 for GreeceIRL for Ireland
Section 2: the number of thisDirective. Asit containsdifferent implemen-
tation dates and different technical standards, two alphabetical
charactersare added. Thes e charactersrefer to the different
application dates for the stages of severity and to the application
of the engine for different specification of mobile machinery, on
the basis of which type-approval was granted. The first character
isdefined in Article 9. The s econd character isdefined in Annex
I, section 1 with regard to the test mode defined in Annex III,
section 3.6.
Section 3: the number of the latest amending Directive applicable to the
approval. If applicable two further alphabetical charactersare to
be added depending on the conditions described in section 2,
even if asa res ult of the new parametersonly one of the charac-
terswasto be changed. If no change of thes e charactersapply
they shall be omitted.
Section 4: a four-digit sequential number (with leading zeros as applicable)
to denote the base approval number. The sequence shall start
from 0001.
Section 5: a two-digit sequential number (with a leading zero if applicable)
to denote the extension. The sequence shall start from 01 for
each base approval number.
2. Example for the third approval (with, as yet, no extension) corresponding to
application date A (stage I, upper powerband) and to the application of the
engine for specification A of mobile machinery, issued by the United
Kingdom:
e 11*98/…AA*00/000XX*0003*00
3. Example of the second extension to the fourth approval corresponding to
application date E (stage II, medium powerband) for the same specification
of machinery (A), issued by Germany:
e 1*01/…EA*00/000XX*0004*021997L0068 — EN — 11.02.2003 — 002.001 — 137
▼B
ANNEX►M2IX◄
1997L0068 — EN — 11.02.2003 — 002.001 — 138
▼B
ANNEX►M2X◄
1997L0068 — EN — 11.02.2003 — 002.001 — 139
▼B
ANNEX►M2XI◄
1997L0068 — EN — 11.02.2003 — 002.001 — 140
▼M2
ANNEX XII
RECOGNITIONOFALTERNATIVETYPE-APPROVALS
1. The following type-approvalsand, where applicable, the pertaining
approval marksare recognis ed asbeing equivalent to an approval to this
Directive for enginesof categoriesA, B and C asdefined in Article 9(2):
1.1. Directive 2000/25/EC.1.2. Type-approvalsto Directive 88/77/EEC, complying with the requirements
of stage A or B regarding Article 2 and Annex I, section 6.2.1 of Directive
88/77/EEC asamended by Directive 91/542/EEC, or UN-ECE Regulation
49.02 series of amendments corrigenda I/2.
1.3. Certificatesof type approvalsaccording to UN-ECE Regulation 96.2. For enginescategoriesD, E, F and G (s tage II) asdefined in Article 9(3),
the following type-approvalsand, where applicable, the pertaining approval
marksare recognis ed asbeing equivalent to an approval to thisDirective:
2.1. Directive 2000/25/EC, stage II approvals;
2.2. Type-approvalsto Directive 88/77/EEC asamended by Directive 99/96/EC
which are in compliance with stages A, B1, B2 or C provided for in Article
2 and section 6.2.1 of Annex I;
2.3. UN-ECE Regulation 49.03 series of amendments;
2.4. UN-ECE Regulation 96 stage B approvals according to paragraph 5.2.1 of
the 01 series of amendments of Regulation 96.1997L0068 — EN — 11.02.2003 — 002.001 — 141