P.1 

OAR Box 1147 

Prepped by Ollie Stewart 

Document Number: 

174) IV-E-47 

Docket Number: 

A-87-11 

Printed 4/22/2008 2:42:56 PM Sheet 174 of 242 
UNITED STATES ENVIRONMENTAL PROTECTION AGENCY 

ANN ARBOR. MICHIGAN 48105 

MAY i 

OFFICE OF 

AIR AND FIADIATION 

MEMORANDUM 

SUBJECT: Meeting of SAE J285 Task Force on Nozzle Geometry 

Specifications 

FROM: John W. Mueller, Mechanical Engineer ji/yUi '//Ity'tyC^ 

Standards Development and Support Brarycn ' / 

TO: 

:HRU: 

Public Docket A-87-11 

John F. Anderson, Senior Project Manager 

Standards Development and Support Branch P/UOn April 14, 1988 I attended the first meeting of the SAE 

J285 task force on nozzle geometry specifications. The purpose 

of this task force is to revise the SAE recommended 

specifications for nozzle geometry in light of EPA's onboard 

refueling proposal. 

The meeting began with a discussion of the objectives of 

the task force. After a lengthy discussion of nozzle geometry 

issues it was decided that the group's main objective should be 

to define a more complete set of recommended spout dimensions 

to replace the present SAE J285 specifications. While other 

objectives were discussed, such as defining specifications for 

automatic shutoff response time a i overpressure shutoff, the 

task force decided thst such projects are beyond the scope of 

the present efforts and that only the nozzle spout should be 

dealt with at this ti*ne. 

Following the definition of the group's objectives, Mike 

Harrigan of Ford handed out some information (included as an 

attachment) on test 

of nozzle design on 

work Ford has done concerning the influence 

refueling and discussed it briefly. Robert 
P.3 

Thompson of Stant then discussed his handout concerning 

fuel dispensing nozzle evaluation (included as an attachment). 

Finally, John Auber of Borg-Warner Automotive presented a 

proposed nozzle spout configuration (included as an 

attachment). Before the meeting adjourned it was decided that 

the next step was to evaluate the four spout configurations 

proposed thus far and to arrive at a single compromised set of 

specifications for comment and evaluation. 

Attachments 
P.4 

Oilmen's Trvch Tsa^kt Inc. 

Smith Meier Inc. 

Vtedw • fiool Ce. 

Wllco, inc. 

®teri/regfgfer5p 

AnMor's inc. 

Doc Petroleum Systems Inc. 

EQulpmsnfSaiesCo.lnc 

Glasgow Equipment Service, Inc. 

Huiuei Ei-juipment Co. 

Oilmen'E Truck Tanks l/ic. 

101 -M0tor*/raafstar$ 

Ticket Prlrtfirie'&teGd* 

Ace Tank And Equipment Co. 

Amtfiar'slnc, 

Brownie TanK Mtg. Co. 

Dec f el^eyf" Splems Inc. 

Ostarman Welding £ Tank Serv.. Inc. 

Oover Corp; Rotary Lit; 

Emerson Electric/Brooks 

Equipment Sales Co. Inc. 

G fi G Oil Equipment Brokers 

Glasgow Equipment Service. Inc. 

HCS Petroleum Equip. Inc. 

Holloway Welding & Piping Co. 

Horner Equipment Co. 

Uquid Controls Corp. 

Parker Hannifin Corp./ Eis Div. 

scuiiy Eiecronic Systems 

Tripitods Ine. 

©esoHne--full-6©rv©/8elf 

-eerve/vopoi' R<5>€©v
fy 

Aee Tank Antf equipment Co. 

America's $vc. Sta. Supply a Mg. 

APS- Pel^eum Equipment 

M. Carder iitf ysirlw Inc. 

Callow inc. 

Concept Communications Co. 

Davis Safes Co., Inc. 

Dawn Duin/i 3plo»i lity. 

Dec Peiwteum Sjwms Inc. 

Determan Welding $, Taftk Serv., Inc. 

DoverCofp.Opwdiv. 

B8Wgmerpri$es 

Eastern Technologies Ltd. 

fmco Wheaton Inc. 

Equipment Sales Co. Inc. 

Q & G on Equipment BroKsrs 

GDNNortfe 

Gilbarco Inc. 

Glasgow Equipment Service, Inc. 

Harco Industries. Jnc, 

HCS Petroleum Equip. Inc. 

Holloway Welding & Piping Co. 

Horner Equipment Co. 

Husky Corp. 

Aee IMA/W Equipment Co 

•Allied Piaatica foe. 

ealcf ank Procuct* 

ft*'Ma* attribute* Ine 

HubCt/Pcodslfic. 

KPlneustrtw 

Jjjnmafc Division Witco Corporal! 

Mc Ned Corp. 

National-Spencer inc 

Patter Hannifin Cotpvpiewsoiv 

Charles C.ParH, Co. 

Sunshine Jr. Stores inc. 

; Inc. 

Balcrank products 

isaay - Way Co. 

Julian Associates. Inc. 

K P Industries 

McNeil Corp. 

MurtfHWJ? - NATIONAL PETROLEUM NEWS 

mi 

Aintiiur's free, 

DG$ Pot^eteuffl Syeteme ln§. 

Eastern Technologies Lld, • 

Glasgow Eqylpment Service, Inc. 

unai ruins iroustflu " 

H C 8 Petroleum Equip. Ino. 

Holloway Welding & Piping Co. 

Homer equipment Co. 

Neptune Measurement c a 

Oilman's Tfuek Tanke Ine. 

Southwest Pun© Co. 

H7SM®t©fi.Trek®t 

Acs Tank tad Equipment Co. 

Amlhor'slnc. 

BeaudfiauEiectraflfCsjne. 

gcewnieTaAkMlg.Ce. 

Dec Petroleum Systems Inc. 

Detarman Welding & Tank Serv., Inc. 

Dresser Industries Inc. 

Cealein TWiwtoyiea Ltd. 

Emar&on Electric/Brooks 

Equipment Sales Co. Inc. 

Glasgow Equipment Servica, Inc. 

HCS Paliukiuiii Eijuij-). Int. 

Holloway Wgying ft Piping Co 

Homer Equipment Co. 

Uquid Controls Corp. 

Nftotune Measurement Co. 

Neptune WocisgromOnt Co. 

Oilmen's Truck Tanks Inc. 

Smith Meter Inc. 

lokhetmUorp. 

Vcodor neolC*. 

162 Mirrors, 

Windehleld/sids 

Amthor'fi Ine. 

General Electric Plastics 

General Electric Plastics 

Geiieutl 3-Jentllii; Safely Equip. Cu. 

K-DUmpCo. 

Farter Hannifin Corp./ Sis Div. 

183 Monitors. 

Oxyg©n/co2/-*9tc. 

Argo Instruments Inc. 

Capital Controls Co. Inc. 

EiuujWIigdluiiliiu 

Emhart Industries Inc. 

Lynn Products Co. Inc. 

MSA 

National Draeger Inc. 

noseflwunt Analytical 

Sansidynfl Inc. 

184 Mufflsrs/failoip&s 

Amthor's Inc. 

i v in (..na... i ,,t.-o,„. h:,, 

iRPCOlrtq. 

L H . Lynn Industries Inc. 

Me Neil Corp. 

Mornson Bros. Ue. 

Oilmen's Truck Tanka Ine. 

Private Rranrt Sflrviroe Inr " * 

Radfqrd Equipment Company 

Richards Industries Inc. 

Richards Industries Of Utah, Inc. 

William ftisHnlph A Crt inr 

Seyierth Mfg., Inc. 

SunstoM Jr. Stores Inc. 

Tims Oaring fiila Inc. 

TripilrtftfiR Inn 

Vltana Corp. Cf WiH Inc. 

Weil Sarvfce Products Corp. 

FUfflJiui,6/-d4uipnlerl! 

Allen-Morrison, Inc. 

DurToughs Corp. 

CPTCorp. 

Owree Dav Slstems. Inc. 

EricayMfg.Co. 

Pilot Corp. 0\ America. Mktg. Oiv. 

Shuro Mfg. Corp. 

Standard fiefHoefaticn Co., Inc. 

Westinghouse Electric Co. 

16SOiiBurndf Nd22ids 

^' 

Altai'Muufeu< 

Berks'? Sve. 

CONCEPT COi 

DCIMatatinc 

I.T.W. fuiiBor 

Modem MalalF 

ShuraMlg.Con* 

SouiWand Disir 

ValvelinoffllCe 

Warren Steal $t 

Wail Servica Pn 

193Qi!°IF 

iquipmei 

Amenta's 3vw.» 

Chsmical Centre 

Dover Cofp. OpE 8 W Entsiprls 

trniwdiflcopor,' 

Enquip. Inc. 

Enyiranetica !n.c 

G&dCorp. 

ittMrtlSosntit. 

GSosgow E^i'tpp. 

6rou<3water Teci 

Holloway WeWir. 

HVfiS PfOfiUflS. i 
THE INFLUENCE OF DISPENSER NOZZLE DESIGN ON REFUELING 

M. J. HARRIGAN - (W+eJ1 «T~ J +- Wto 4/>F -

 -*>Z&5~ > -*>* ^ ~M. ' *"/f/» ' y 

D. L. CRAGGS 

FORD MOTOR COMPANY 

1 -

bi 
DESIGNED EXPERIMENT TO DETERMINE WHAT PARAMETERS CONTROL QUALITY OF REFUELING 

FIRST STEP: BROAD SCREENING EXPERIMENT 

BLOCKED PARTIAL FACTORIAL DESIGN 

13 PARAMETERS IN 32 RUNS 

INCLUDES THE EFFECT OF NOZZLES AS AN ENVIRONMENTAL FACTOR 

• OPW IIA UNLEADED 

• EMCO-WHEATON A-4000 STAGE II VAPOR RECOVERY 

• EMCO-WHEATON A-2000 UNLEADED 

• EMCO-WHEATON A-2000 WITH IMPROVED SPOUT 

• HUSKY I + X UNLEADED 

b> 
FUEL FILLER PIPE DIMENSIONS FOR EXPERIMENTAL DESIGN 

SYMBOL DESCRIPTION FILLE R PIP E DESIG N NUMBE R 

t 

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 

B Restrictor opening 

offset 

C Distance to first bend 

a Pipe inlet angle 

D2 Mid-pipe diameter 

F Length of run 

D3 Pipe outlet diameter 

E2 Total drop height 

7 Incline of long run 

<5 Incline of major 

drop 

A Depth to restrictor 

V Vent diameter 

0 Filler opening depth 

below fuel at shutoff 

Nozzle designs: 

OPW 

Emco-Wheaton Unleaded 

Emco-Wheaton Stage II 

Emco-Wheaton Improved 

Husky Unleaded 

-

-

-

+ 

+ 

+ 

+ 

+ 

-

-

+ 

+ 

-

-

-

-

+ 

+ 

+ 

+ 

+ 

. 

-

+ 

-

-

+ 

- . 

-

+ 

+ 

-

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+ 

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-

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-

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_ 

+ 

-

+ 

-

+ 

-

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+ 

-

-

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+ 

+ 

+ 

+ 

+ 

+ 

+ 

+ 

+ 

-

-

-

. 

-

-

-

+ 

+ 

+ 

+ 

-

+ 

+ 

. 

+ 

-

-

+ 

-

-

+ 

-

-

-

+ 

-

+ 

-

+ 

-

+ 

-

+ 

-

+ 

+ 

+ 

+ 

-

+ 

+ 

-

-

+ 

+ 

-

_ 

-

-

+ 

+ 

+ 

-

-

-

+ 

+ 

-

+ 

+ 

-

+ 

+ 

-

+ 

-

-

+ 

-

+ 

_ 

-

+ 

+ 

+ 

-

-

+ 

+ 

+ 

-

-

_ 

+ 

+ 

+ 

+ 

+ 

+ 

+ 

+ 

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+ 

+ 

+ 

-

-

-

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o 

X 

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o 

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o 

X 

o 

o 

o 

X 

o 

o 

o 

X 

o 

o 

o 

X 

o 

o 

X X 

o o 

0 

X 

0 

0 

0 

X 

0 

X 

0 

0 

0 

X 

0 

X 

0 

0 

X 

0 

0 

X 

0 

0 

0 

X 

0 

0 

0 

X 

0 

X 

0 

0 

0 

0 

0 

X 

0 

0 

X 

0 

0 

X 

0 

0 

0 

X 

Specified or Derived Dimensions 

D\ Inlet diameter 

Restrictor opening diameter 

E\ Height of first drop 

fi Included angle at first bend 

R Bend radii (to centerline) 

Taper angle at transitions 

to smaller diameters 

50.0 mm 

21.0 mm 

As Derived 

As Derived 

100 mm 

30° 

- 3 
EXPERIMENTAL CONDITIONS 

•FLOW RATE CONTROLLED AT PUMP -

•FUEL VOLATILITY 

•FUEL, TANK AND PIPE TEMPERATURE 

•FILLER PIPE AND TANK ATTITUDE -

•FUEL SUPPLY 

1 TO 20 GALLONS PER MINUTE +/" 1/8

 GPM ) 

13+/"-5 psi RVP 

ROOM TEMPERATURE - 73.8 +/-1.3°¥ 

FIXTURED TO +/-.5 DEGREE OF IN-CAR POSITION 

DIRECTLY FROM 55 GALLON DRUMS 

/ -f '^* 

&.<L 7 

- 4 -

Tl 

00 
EXPERIMENTAL TECHNIQUE 

• INSERT NOZZLE TO THE FULLEST EXTENT POSSIBLE AND LATCHED ON THE PIPE OPENING 

• ALIGN NOZZLE PERPENDICULAR TO THE GROUND IN THE PIPE OPENING 

• OPERATE NOZZLE WITH THE TRIGGER LATCHED AT THE HIGHEST FLOW RATE SETTING 

• CONTROL FLOW RATE AT THE PUMP 

• MAKE SHUTOFF MEASUREMENTS BASED ON AUTOMATIC NOZZLE SHUTOFF 

• MAKE ALL FILL QUALITY AND SHUTOFF MEASUREMENTS WITH HANDS OFF THE NOZZLES 

- 5 -

Tl 

CO 
CRITERIA FOR MEASUREMENTS 

• FILL: 

HIGHEST FLOW RATE DURING STEADY STATE FILL WHERE NO FUEL LEAVES THE PIPE 

• SHUTOFF: 

HIGHEST FLOW RATE AT AUTOMATIC NOZZLE SHUTOFF WHERE NO FUEL LEAVES THE PIPE 

NOTE: Fill and shutoff are treated as two totally different phenomenon. Thus it is possible to have a maximum 

acceptable shutoff at a higher flow rate than is acceptable for steady state filling. 

6 -
EFFECT OF NOZZLE DESIGN ON FILL RATE 

j (16 Pipes) 

| FILL 

| SHUTOFF 

OPW 

x | 

13.06 | 

10.14 | 

s 

4.69 

4.32 

EMCO UNLEADED 

x | s 

10.78 | 5.10 

6.55 | 4.46 

EMCO IMPROVED 

x | s 

10.97 

7.95 

4.58 

3.21 

HUSKY | 

x | s j 

10.66 | 2.05 | 

6.72 | 4.01 | 

| (8 Pipes) 

| FILL 

| SHUTOFF 

j (24 pipes) 

| FILL 

| SHUTOFF 

OPW 

x | 

11.06 | 

7.50 | 

OPW 

x | 

12.72 | 

9.41 | 

s 

3.86 

3.36 

s 

4.45 

4.56 

Emco Stage II | 

x | s j 

9.87 | 2.25 | 

5.69 | 4.08 | 

Emco Improved | 

x | s j 

10.40 | | 

7.79 | 4.04 | 
P.12 

Stant 

Fuel Dispensing Nozzle Evaluation 

14 March 1988 

Field Survey of Service Station Nozzles 1 

Fuel Dispensing Nozzle Survey 2 

Appendix A 3 

Appendix B 9 

Appendix C 10 
P.13 

Stant FIELD SURVEY OF SERVICE STATION NOZZLES 

Nozzle Shut-off Signal, Vacuum: X=7.18 kPa CT =0.958 kPa 

(Full fill rate) 

Nozzle Diameter: X=0.184 in. O" =0.005 in. 

(SAE Recommendation: 13/16 in. (0.9125 to 0.840)) 

Vacuum Signal Nozzle Diameter 

Service Station (kPa) (in^J 

Amoco " 8713 0.816 

U T 5 1 J n fil'' 

OPW 9.0 0.813n oitr 

°'8150.812 

7.5 0.812n 

u'0i 0.812 

°'8180.813 

0.813 

0.814 

°*8130.815 

°*8130.815 

°'8130.810 

0,8330.812 

°*8280.832 

°'8250.810 

°'8150.808 

°*8130.812 

°'8140.812 

0.815 

0,8130.810 

0.810 

0.812 

°'8100.820 

°'8110.816 

0 -812 ^8 -0.815 

°-8170-8-0.815 

°-8120.813 

Note: Each pressure represents three trials for a nozzle. It should 

be noted there was little measurable variation between trials 

for each nozzle. 

Shell (1) 

OPW, Husky 

Bonded 

OPW 

United 

OPW, Hus 

Shell (2) 

Husky 

Mobil 

Viking 

»ky 

Clark 

Emco Wheaton 

Shell (3) 

OPW 

Marathon 

Emco,Hus 

Checker 

OPW 

ky 

6.5 

7.0 

5.25 

7.5 

7.5 

8.0 

7.0 

7.0 

6.5 

6.0 

7.5 

9.0 

8.0 

5.75 

6.5 

6.25 

7.5 

7.0 

7.5 
P.14 

Pg. I 

SlCKHt 4/12/88 

Liquid , 

Flow Rate 

gal/min. 

3 

5 

8 

10 

13 

15 

18 

Liquid , 

Flow Rate 

gal/min. 

3 

5 

8 

10 

13 

15 

18 

Fuel 

Nozzle 

Emco W 

4.7 

4.4 

6.1 

6.5 

7.6 

8.9 

9.5 

Nozzle 

Emco W 

2.8 

2.8 

3.6 

4.0 

3.6 

3.8 

3.9 

D 

1 

1 

Lspensing Nozz 

Nozzle ShutAir 

Nozzle 2 

OPW 1 

4.9 

7.0 

7.0 

8.4 

7.3 

7.2 

8.2 

Flow Into 

Nozzle 2 

OPW 1 

4.0 

4.6 

5.9 

6,5 

5.0 

5.1 

4.8 

le 

off 

Survey 

Vacuum, 

Nozzle 

OPW 2 

5.2 

6.7 

7.2 

8.0 

9.0 

9.1 

9.5 

*<,ty pkPa2 

3 

Sensing Port 

Nozzle 

OPW 2 

3.8 

5.2 

5.6 

5.6 

6.9 

6.0 

6.5 

3 

, u 

Nozzle 

OPW 3 

6.0 

6.4 

7.7 

9.2 

8.4 

9.6 

8.7 

min. 

Nozzle 

OPW 3 

3.6 

4.0 

4.5 

5.5 

5.5 

5.5 

4.5 

4 

4 

-

Liquid Dispensed: MS 4957 Carburator Calibration Fluid; See Appenxix B 

2 The average of 10 trials for each nozzle at each flow rate is listed; 

See Appendix A. 
Stant 

Appendix A 

Nozzle Evaluation 

Emco Wheaton 

OPW 

OPW 

OPW 

Test Fixture 

Al 

A2 

A3 

A4 

AS 

P.15 

"T 

rg. J 
P.16 

Stant 4/12/88 

Ps. 4 

Al 

Nozzle:

 #1 Emco Wheaton 

Flow Rate 

gal/min 

3 

5 

8 

10 

13 

15 

18 

Flow Rate 

gal/min. 

3 

5 

8 

10 

13 

15 

18 

1 

5.0 

5.0 

5.0 

6.5 

8.0 

10. 

19. 

Trial 

2.8 

2.8 

3.6 

4.0 

3.6 

5.8 

3.9 

2 

4.0 

5.0 

6.0 

6.5 

8.0 

9.0 

9.0 

n 

Va 

3 

4.5 

4.5 

6.0 

6.5 

7.5 

9.0 

9.5 

A 

cuum 

4 

4.5 

4.5 

6.0 

6.5 

7.5 

8.0 

9.5 

ir Fl 

At Nozzle Shut-off, 

Trial # 

5 6 7 

5.0 

4.0 

6.0 

6.5 

7.5 

8.5 

9.5 

5.0 

4.0 

6.0 

6.5 

7.5 

8.5 

9.5 

ow To Sensing 

L/min 

4.0 

4.0 

6.5 

7.0 

7.5 

9.0 

10. 

Port 

kPa 

8 

5.0 

4.5 

6.5 

6.5 

8.0 

8.0 

10. 

9 

5.0 

4.5 

7.0 

6.0 

7.5 

8.0 

9.0 

10 

5.0 

4.5 

6.0 

6.5 

7.0 

8.0 

9.0 

X 

4.7 

4.4 

6.1 

6.5 

7.6 

8.9 

9.5 

cr 

0.4 

0.3 

0.5 

0.2 

0.3 

0.5 

0.4 

Nozzle Diameter: 0.810j.n. 
Stant 4/12/8 8 

Pg. 5 

A2 

Nozzle : #1 OPW 

Flow Rate 

gal/min 

3 

5 

8 

10 

13 

15 

18 

Flow Rate 

gal/min. 

3 

5 

8 

10 

13 

15 

18 

1 

5. Q 

7.0 

7.0 

9.0 

7.0 

7.0 

770 

Tria 

4.0 

4.6 

5.9 

6.5 

5.0 

5.1 

4.8 

2 

5.0 

7.0 

7.0 

9.0 

7.0 

7.0 

7.0 

i n 

Vacuum 

3 4 

5.0 4.0 

7.0 7.0 

7.0 7.0 

9.0 9.0 

7.0 7.0 

7.5 7.5 

7.5 8.0 

At Nozz 

Trial 

5 

5.0 

7.0 

7.0 

8.0 

7.0 

7.5 

8.0 

Air Flow To S 

L/min 

le Shut-off, 

# 

6 7 

5.0 

7.0 

7.0 

8.0 

7.0 

7.0 

8.0 

ensing 

5.0 

7.0 

7.0 

8.0 

7.0 

7.0 

9.0 

Port 

kPa 

8 

5.0 

7.0 

7.0 

8.0 

8.0 

7.5 

9.0 

9 

5.0 

7.0 

7.0 

8.0 

8.0 

7.0 

9.0 

10 

5.0 

7.0 

7.0 

8.0 

8.0 

7.5 

9.0 

-

X 

4.9 

7.0 

7.0 

8.4 

7.3 

7.2 

8.2 

cr 

0.3 

0 

0 

0.5 

0.4 

0.2 

0.8 

Nozzl e Diameter: 0.814 in . 
Stant 4/12/8 8 

Pg. o 

A3 

Nozzle : #2 OPW 

Flow Rate 

gal/min 

3 

5 

8 

10 

13 

15 

18 

Flow Rate 

gal/min 

3 

5 

8 

10 

13 

15 

18 

1 

4.0 

5.0 

7.5 

8.0 

9.5 

10. 

9?0 

Tria 

3.8 

5.2 

5.6 

5.6 

6.9 

6.0 

6.5 

2 

4.0 

6.0 

7.0 

8.0 

9.0 

9.0 

10. 

1 #1 

5, 

7. 

7, 

8, 

9, 

9, 

9. 

3 

.0 

.0 

.0 

.0 

.0 

.0 

.5 

Vacuum 

4 

6.0 

7.0 

7.0 

8.0 

9.0 

9.0 

10. 

Air Fl 

At Nozzle Shut-off, 

Trial # 

5 6 7 

5.0 

6.5 

7.0 

8.0 

9.0 

9.0 

9.0 

5.0 

7.0 

7.0 

8.0 

9.0 

9.0 

9.0 

.ow To Sensing 

L/min 

5.5 

7.0 

8.0 

8.0 

9.0 

9.0 

9.5 

Port 

kPa 

8 

6.0 

7.0 

•.o 

8.0 

9.0 

9.0 

9.5 

9 

5.5 

7.5 

7.0 

8.0 

9.0 

9.0 

10. 

10 

6.0 

7.0 

7.0 

8.0 

9.0 

9.0 

9.5 

m 

X 

5.2 

6.7 

7.2 

8.0 

9.0 

9.1 

9.3 

cr 

0.'. 

o.: 

o.: 

o. 

0.. 

0.. 

0.-

Nozzl e Diameter: 0.814 in . 
P.19 

Stant 4/12/8 8 

Pg. 7 

A4 

Nozzle : #3 OPW 

Flow Rate 

gal/min 

3 

5 

8 

10 

13 

15 

18 

Flow Rate 

gal/min. 

3 

5 

8 

10 

13 

15 

18 

1 

6.0 

6.0 

6.0 

9.0 

9.0 

9.0 

8.*0 

Trial 

5.6 

4.0 

4.5 

5.5 

5.5 

5.5 

4.5 

2 

6.0 

6.0 

7.0 

9.0 

9.0 

9.0 

8.0 

#1 

3 

6.0 

6.5 

7.5 

9.0 

9.0 

9.5 

8.5 

Vacuum 

4 

6.0 

6.0 

7.5 

9.0 

9,0 

10. 

8.5 

Air F] 

At Nozzle Shut-off, 

Trial # 

5 6 7 

6.5 

6.5 

8.0 

9.5 

9.0 

9.5 

9.0 

6.0 

6.0 

8.0 

9.0 

9.0 

9.5 

9.0 

.ow To Sensi 

L/min 

6.0 

6.0 

8.0 

9.0 

10. 

9.5 

9.0 

ng Port 

kPa 

8 

6.0 

7.0 

8.0 

9.0 

10. 

10. 

9.0 

9 

6.0 

7.0 

8,0 

10. 

10. 

10. 

9.0 

10 

6.0 

7.0 

9.0 

10. 

10. 

10. 

9.0 

-

X 

6.0 

6.4 

7.7 

9.2 

9.4 

9.6 

8.7 

cr 

0.1 

0.4 

0.7 

0.4 

0.5 

0.3 

0.4 

Nozzle Diameter: 0.814 in, 
P.20 

c 

z z z 

I/I a/t «n 

O O O 

•no o — ei 

a* a~\ 9 

« «•>* 

c 

Pg. 8 

Fuel Dispensing 

Nozzle 

Seal 

"2 

Sensing Port 

L 

Vapour Tube 

Test Procedure: 

Nozzle Shut-off Vacuum: Jr 7 ia\*C $" ft-1* <a* fNozzle shut-off vacuum was determined by establishing 

appropriate liquid flow then plugging vapour tube. Vacuum 

would build until the nozzle clicked off. That vacuum was 

recorded. 

Air Flow to Sensing Port: 

Air flow was determined by placing a rotometer flow gauge 

in series in the vapour line. Readings were made once the 

appropriate liquid flow was achieved. 
P.21 

U^U 

U.S. DEPARTMENT OF LABOR 

Occupational Safety and Health Administration 

MATERIAL SAFETY DATA SHEET 

Form Acorov*-d 

O M B NO. 44-niia7 

Required under USOL Safety and Health Regulations for Ship Repairing, 

Shipbuilding, and Shipbreaking (29 CFR 1915, 1916. 1917) 

SECTION I 

MANUFACTURER'S NAME 

Gage Products Company 

AOORESS (Number. Street. Qty, Stale, end ZIP Code) 

625 Wanda, Ferndale Mi 48220 

EMERGENCY TELEPHONE NO. 

313-564-6530 msouu 

PWIECTIO" 

ac i»l . t I«T VCA — 

CHEMICAL NAME ANO SYNONYMS 

CHEMICAL FAMILY 

Aliphati c Hydrocarbons 

FORMULA 

TRAOE NAME ANO SYNONYMS 

tg;^957 Crtrhurator Calibration 

c

n

H

2n+2 <*.hilt&:'" 

SECTION II • HAZARDOUS INGREDIENTS 

PAINTS. PRESERVATIVES. Si SOLVENTS 

PIGMENTS 

CATALYST 

VEHICLE 

SOLVENT* I 

AOOITIVES 

OTHERS 

% 

)0 

TLV 

(Unitil 

100 ppm 

ALLOYS ANO METALLIC COATINGS 

BASE METAL 

ALLOYS 

METALLIC COATINGS 

FILLER METAL 

PLUS COATING OR CORE FLUX 

OTHERS 

HAZARDOUS MIXTURES OF OTHER LIQUIDS. SOLIDS. OR GASES 

1 

% 

X 

TLV 

lUnita) 

TLV 

(Umtttl 'A 

; '.->• 

.#. 

T'. # 

•Ql' 

'•••* • 

SECTION III - PHYSICAL DATA 

•OILING POINT (°F.) 

VAPOR PRESSURE (mm Hfl.) @ £8 ° F 

VAPOR DENSITY (AIR-1) 

SOLUBILITY IN WATER 

300-410 

2.0 

4.9 

INSOL 

SPECIFIC GRAVITY (MJO-1 ) 0 gg O 

PERCENT, VOLATIL E 

BY VOLUME (%) 

EVAPORATION RATE 

( -1) 

o.788 

100 

APPEARANCE ANO OOOR Colorles s Mobil e Liqui d 

SECTION IV - FIRE AND EXPLOSION HAZARD DATA 

FLASH POINT (M«ll,oa UIMA 

100 F min. SETA 

FLAMMABLE LIMITS 

315 : 

UM 

23C 

EXTINGUISHING MEDIA u 

CO.,, foam, or dry chemical 

SPECIAL FIRE FIGHTING PROCEDURES 

j-3 

.TrU y 

•i 

Zi 

.•.-•* 

UNUSUAL FIRE ANO EXPLpSION HAZAROS 

Never use welding or cutting torch on or near drum (even empty), the product 

-t 

or any residue left in the drum can ignite explosively. 

•»AOE (1) (Continued on reverte tide) Form OSHA-20 

«•*. May It 
UNLESS OTHERWISE SPECIFIED 

TOIEIUNCE FOR DIMS i 

TOLERANCE FOR ANGLES • 

Submit Sample For Engineering Approval 

Before Production Is Run. 

Z.&O O 

SECT\ON A." A . 

; i 

i ,. 

i ; 

•ii' • 

! I 

• • • 

i' ?! 

> 

T3 

fD 

D. 

X 

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QE0META1C CHAAACTE A1STIC SYMBOiS 

S1AAIGHTNESS 

AOUHPNEIt ICIRCULAAITTI 

TOTAl KUNOOI 

CONCENTAlCITV o.p.»/.-; PUEJL D\«3Pe.M^e.P5, 

OATI 

-X - \-z. - e>8 

CHINDniClTV 

PROFI U O' A im i 

MO'II I or A tuft'AC C 

PARAUILIftM 

Pf APfNCHCULAftlTV 

AN0UAM1Y 

ClRCUlAH RUNOUT 

• ASIC DIMENSION 

SL 

cm Stant Inc Connersville. Indiana 

MAXIMUM MATERIAL 

CONIXTION IMMCI 

AEOAKOltll OF 

FEAtuAE SIM lAFt) 

FfTO-fECtEO TOICAANCE 

luaat tl MFO 

APP. 

Rtl. 

OATI 

«EF. 

NO. 

SCALE 

FULL. 

FART NO. 

.OQ 
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