Source: http://www.google.com/patents/US6945046?dq=7,321,221
Timestamp: 2014-10-02 01:35:58
Document Index: 282889297

Matched Legal Cases: ['art 1', 'art 1', 'art 1', 'art 1', 'arts 1', 'art 1', 'art 1', 'art 1', 'art 1']

Patent US6945046 - Turbine casing for an exhaust turbocharger made by casting - Google PatentsSearch Images Maps Play YouTube News Gmail Drive More »Sign in<nobr>Advanced Patent Search</nobr>PatentsThe invention concerns a casing aggregate for the turbine of an exhaust turbocharger. The invention is identified by the following characteristics: a spiral casing adapted for surround the running wheel of the turbine; a tongue-like wall part (tongue) in the inside of the spiral casing; an inlet connection;...http://www.google.com/patents/US6945046?utm_source=gb-gplus-sharePatent US6945046 - Turbine casing for an exhaust turbocharger made by castingAdvanced Patent SearchPublication numberUS6945046 B2Publication typeGrantApplication numberUS 10/296,135PCT numberPCT/US2001/018274Publication dateSep 20, 2005Filing dateJun 6, 2001Priority dateJun 7, 2000Fee statusLapsedAlso published asUS20030205047Publication number10296135, 296135, PCT/2001/18274, PCT/US/1/018274, PCT/US/1/18274, PCT/US/2001/018274, PCT/US/2001/18274, PCT/US1/018274, PCT/US1/18274, PCT/US1018274, PCT/US118274, PCT/US2001/018274, PCT/US2001/18274, PCT/US2001018274, PCT/US200118274, US 6945046 B2, US 6945046B2, US-B2-6945046, US6945046 B2, US6945046B2InventorsRuediger Allmang, Hartmut Claus, Volker SimonOriginal AssigneeBorgwarner Inc.Export CitationBiBTeX, EndNote, RefManPatent Citations (9), Referenced by (8), Classifications (20), Legal Events (5) External Links: USPTO, USPTO Assignment, EspacenetTurbine casing for an exhaust turbocharger made by castingUS 6945046 B2Abstract The invention concerns a casing aggregate for the turbine of an exhaust turbocharger.
The invention is identified by the following characteristics:
a spiral casing adapted for surround the running wheel of the turbine; a tongue-like wall part (tongue) in the inside of the spiral casing; an inlet connection; an outlet connection; a flange to connect to a bearing casing; wherein the casing aggregate is manufactured of thin-walled precision casting; wherein the casing aggregate is made of at least two parts, so that at least one separation joint is present; and the separation joint is arranged as follows:
it runs in an axially perpendicular level; it runs along the apex line of the spiral casing; it extends over an arc of a circle of approximately 270 degrees; it lies outside of the area of the tongue. Images(3) Claims(2)
1. Casing aggregate for the turbine of an exhaust turbocharger, comprising:
a. a spiral casing adapted to surround the running wheel of the turbine; b. a tongue-like wall part (tongue) in the inside of the spiral casing; c. an inlet connection; d. an outlet connection; e. a flange adapted for connecting to a bearing casing of the turbocharger; f. wherein the casing aggregate is manufactured by thin-walled precision casting; g. wherein the casing aggregate is comprised of at least two parts, so that at least one separation joint is present; and h. wherein the separation joint is arranged as follows: i. it runs in an axially perpendicular level; ii. it runs along the apex line of the spiral casing; iii. it extends over an arc of a circle of approximately 270 degrees; iv. it lies outside of the area of the tongue. 2. Casing aggregate as in claim 1, wherein the parts of the casing aggregate are welded to each other along the separation joint.
CROSS REFERENCE TO RELATED APPLICATION This application is a national stage of PCT/US01/18274 filed Jun. 6, 2001 and based upon DE 100 28 161.3 filed Jun. 7, 2000 under the International Convention.
The invention concerns a casing aggregate for the turbine of an exhaust turbocharger. The invention especially concerns the spiral casing of the turbine.
Exhaust turbochargers are a must in modern vehicles. The most important components include a turbine and a compressor. These two components are located on one and the same shaft. The exhaust of the internal combustion engine is conducted to the turbine. The exhaust powers the turbine. Then the turbine in turn powers the compressor. This takes in air from the environment and compresses it. The compressed air is then used for combustion in the engine. The purpose of exhaust turbochargers is to minimize the exhaust emissions as well as to increase the efficiency of the engine and its torque. They also have an important function in regards to the efficiency of the catalytic converter.
The following requirements are generally demanded of an exhaust turbocharger: They should fulfill the mentioned functions regarding the exhaust emission, the efficiency level and torque of the engine in the most optimal manner possible. In doing so, they should have minimal weight and minimal construction volume. The design should be simple and easy to assemble, so that manufacturing costs are held to minimal levels. They should be compatible with catalytic converters.
The known exhaust turbochargers do not fill all these functions, or only to a certain point. That is, lowering pollutant emissions during the cold start phase leaves much to be desired, and weight and space demands are unreasonably high.
The task of the invention is to design a casing aggregate of the type mentioned in such a manner that significant improvements are made in the mentioned parameters. This task is accomplished by the characteristics of claim 1.
In accomplishing the task, the inventors stuck with the tried and true execution of the casing aggregate by casting. For this, however, they departed from the conventional method of casting steel in a sand mold, and switched to a thin-walled fine casting, also known as precision casting. This allows the wall thickness to be greatly reduced. This also greatly decreases the weight of the aggregate. The casing aggregate now has a substantially lower mass, so that only relativey small heat energy can be removed from the exhaust in the cold start phase. Thus the thermal inertia is very minimal.
As an additional measure, the casing aggregate is assembled from at least two parts. Therefore, the casing aggregate has at least one separation joint. The separation joint is arranged as follows:
it extends in an axially perpendicular level, it runs along the apex line of the spiral casing, it extends over an arc of a circle of approximately 270 degrees, and it lies outside of the area of the tongue. Thus in any case, the spiral casing is in at least two parts. In doing so, the division into two on the basis of the separation joint described above, occurs in such a manner that the two following benefits result:
For one thing, each of the two parts of the spiral casing can be cast without requiring the use of casting cores. The shapes of the two spiral casing parts don't require any undercutting.
In addition, the separation joint is positioned in such a manner that the area of the tongue lies outside of the separation joint. The tongue area is that area this is thermally stressed the most. When the two cast parts of the spiral casing are put together, the tongue area, therefore, consists of a single piece without separation joint, which takes into account the high thermal stress and, therefore, the high demands of rigidity in this area.
The two parts can be joined, for example, using any type of welding, for example using laser welding or micro-plasma welding.
By avoiding casting cores, positional tolerances don't need to be considered while casting. This means that the wall thickness can already be less for this reason than with the classical method of using casting cores. This already results in considerable weight reduction. A multiple-part turbine casing cast in precision casting has an average wall thickness of approximately 2 mm. This means a-mass reduction of 40 to 60% in comparison to execution in cast steel in sand. In addition, the manufacturing costs of a spiral casing based on the invention are lower than before. In general, a heat resistant cast steel for exhaust temperatures of 1050� C. is considered suitable as a material.
The finish and dimensional accuracy are optimal. This leads to higher efficiency levels. The manufacturing costs will already be lower because refinishing is unnecessary.
The invention is further explained in the drawings. The following details are represented:
FIG. 1 shows an exhaust turbocharger in axial section.
FIG. 2 shows an enlarged section through the spiral casing of the turbine of FIG. 1.
The turbocharger shown in FIG. 1 has the following components as its most important elements:
A turbine 1 with turbine wheel 1.1, a compressor 2 with compressor wheel 2.1, a bearing 3, and a shaft 4 on which the turbine wheel 1.1 and the compressor wheel 2.1 are seated.
The turbine casing is executed in known fashion as a spiral casing. It is made of two main parts, namely a part 1.2�herein referred to as the �inner part�, and a part 1.3�herein referred to as the �outer part�. An outer exhaust support 1.4 is a component of the outer part 1.3. This could however also be separate from the outer part 1.3.
The following is decisive:
The two main parts 1.2 and 1.3 of the spiral casing of the turbine are separated along a separation joint. The separation joint runs in an axially perpendicular level. It runs along the apex line of the spiral casing.
As can be seen in FIG. 2, the separation joint extends over an angle of 270 degrees. It lies outside of the tongue area 1.5 of the spiral casing. This area is highly thermally stressed.
FIG. 2 shows part 1.3. Part 1.2 is removed.
The separation joint extends from point A to point B. The area of the tongue 1.5 remains undisturbed. This means that the spiral casing is one part in the tongue area. For the purpose of assembly, part 1.2 is seated over the area of the separation joint between point A and B on part 1.3.
Patent CitationsCited PatentFiling datePublication dateApplicantTitleUS3310940 *Oct 7, 1965Mar 28, 1967Stalker CorpGas turbinesUS3396906 *Feb 6, 1968Aug 13, 1968Trane CoPump housing seal arrangementUS4147467 *Aug 16, 1977Apr 3, 1979Motoren- Und Turbinen-Union Friedrichshafen GmbhExhaust gas turbochargerUS4384821 *Oct 14, 1981May 24, 1983Wallace Murray CorporationFree floating divider wall turbine housingUS4927336 *Dec 7, 1987May 22, 1990Mtu Motoren-Und Turbinen-Union Muenchen GmbhDrive system including an engine and a turbo-chargerUS5810556 *Mar 4, 1997Sep 22, 1998The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationCarbon-carbon turbocharger housing unit for intermittent combustion enginesUS5947682 *Aug 21, 1996Sep 7, 1999Daewoo Electronics Co., Ltd.Pump housing and a manufacturing method thereforGB1199158A * Title not availableGB1263932A * Title not available* Cited by examinerReferenced byCiting PatentFiling datePublication dateApplicantTitleUS8206133Aug 12, 2008Jun 26, 2012GM Global Technology Operations LLCTurbocharger housing with integral inlet and outlet openingsUS8347499 *Nov 13, 2008Jan 8, 2013Alstom Technology LtdMethod for producing a turbine casingUS20090126190 *Nov 13, 2008May 21, 2009Alstom Technology LtdMethod for producing a turbine casingUS20100310362 *Aug 12, 2008Dec 9, 2010Daimler AgHousing for a Blade WheelUS20100310364 *Aug 12, 2010Dec 9, 2010Siegfried BotschTurbine housing and method for producing a turbine housingUS20110091318 *Nov 27, 2010Apr 21, 2011Kraetschmer StephanTurbine housing for an exhaust gas turbocharger of an internal combustion engineUS20110318177 *Aug 3, 2011Dec 29, 2011Siegfried BotschTurbine housing for an exhaust gas turbocharger and method for producing turbine housingWO2010033996A2 *Sep 22, 2009Mar 25, 2010Metaldyne Company LlcFabricated turbine housing* Cited by examinerClassifications U.S. Classification60/602, 415/915, 415/136, 415/215.1, 415/200, 415/205, 415/138, 60/605.1, 417/407, 415/184International ClassificationF01D9/02, F01D25/24Cooperative ClassificationF05D2230/232, F01D25/24, F01D9/026, F05D2230/21, F05D2220/40, Y10S415/915European ClassificationF01D9/02C, F01D25/24Legal EventsDateCodeEventDescriptionNov 12, 2013FPExpired due to failure to pay maintenance feeEffective date: 20130920Sep 20, 2013LAPSLapse for failure to pay maintenance feesMay 3, 2013REMIMaintenance fee reminder mailedSep 30, 2008FPAYFee paymentYear of fee payment: 4Mar 31, 2003ASAssignmentOwner name: BORGWARNER INC., MICHIGANFree format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:ALLMANG, RUEDIGER;CLAUS, HARTMUT;SIMON, VOLKER;REEL/FRAME:013908/0736;SIGNING DATES FROM 20030304 TO 20030305RotateOriginal ImageGoogle Home - Sitemap - USPTO Bulk Downloads - Privacy Policy - Terms of Service - About Google Patents - Send FeedbackData provided by IFI CLAIMS Patent Services©2012 Google