US5528902A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Support housing for exhaust gas turbochargers
Assignee: Rolls Royce Solutions GmbH
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Filing: 1993-06-01
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Granted: 1996-06-25
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Expires: 2013-06-01
Abstract
Abstract A support housing for the fastening of the exhaust gas turbochargers of an internal-combustion engine is provided. The support housing encloses a hollow space which is used for receiving the turbines of the exhaust gas turbochargers while the compressors are situated outside the hollow space. In order to simplify the manufacturing and assembly and to reduce the costs, bearing housings of the exhaust gas turbochargers are integrated in the support housing. The manufacturing and the assembly may also be simplified and rendered less expensive by the fact that the support housing is divided into two symmetrical housing parts along a plane extending through the perpendicular axis in the center of the support housing. In this case, the two housing parts are preferably constructed to be centrically symmetrical with respect to the central perpendicular axis.
Inventors
- 👤 Guenther Hoerl
- 👤 Edmund Eberhardt
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 12:42
CPC Classifications
F; F02; F02B; F02B39/00; F02B39/005; F01; F01D; F01D25/00; F01D25/08; F01D25/14; F01D25/145; F02B37/00; F02B37/004; F02B37/007; F02B37/013; F02B39/14; F02B67/00; F02B67/08; F02B67/10; F02C; F02C7/00; F02C7/24; F02F; F02F7/00; F02F7/006; F05; F05D; F05D2220/00; F05D2220/40; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
218 words
Support housing for at least two exhaust gas turbochargers arrangeable on an internal-combustion engine, the exhaust gas turbochargers each having two blade wheels arranged on a common shaft, one of said two blade wheels being arranged in a compressor housing and the other of said two blade wheels being arranged in a turbine housing, comprising: a bearing housing arranged between the compressor housing and the turbine housing having the common shaft disposed therein for each exhaust gas turbocharger; wherein the turbine housings of the exhaust gas turbochargers form flow spaces, each of said flow spaces including a spiral duct, an adjoining, radially interior blade wheel duct, and an axially directed outlet duct; wherein the support housing is constructed as a box-type supporting device forming a hollow space therein, said exhaust gas turbochargers being fastened on said box-type supporting device such that the compressor housings are arranged outside the hollow space and the turbine housings are arranged inside the hollow space; recesses for in walls of the support housing, said common shafts of the exhaust gas turbochargers extending through said recesses; openings provided in said walls for feeding and removing exhaust gases to and from the turbine housings; wherein the bearing housings of the exhaust gas turbochargers are formed integrally in one-piece with said walls of the support housing.
Claim 2
Dependent Claim
218 words
Support housing for at least two exhaust gas turbochargers arrangeable on an internal-combustion engine, the exhaust gas turbochargers each having two blade wheels arranged on a common shaft, one of said two blade wheels being arranged in a compressor housing and the other of said two blade wheels being arranged in a turbine housing, comprising: a bearing housing arranged between the compressor housing and the turbine housing having the common shaft disposed therein for each exhaust gas turbocharger; wherein the turbine housings of the exhaust gas turbochargers form flow spaces, each of said flow spaces including a spiral duct, an adjoining, radially interior blade wheel duct, and an axially directed outlet duct; wherein the support housing is constructed as a box-type supporting device forming a hollow space therein, said exhaust gas turbochargers being fastened on said box-type supporting device such that the compressor housings are arranged outside the hollow space and the turbine housings are arranged inside the hollow space; recesses for in walls of the support housing, said common shafts of the exhaust gas turbochargers extending through said recesses; openings provided in said walls for feeding and removing exhaust gases to and from the turbine housings; wherein the bearing housings of the exhaust gas turbochargers are formed integrally in one-piece with said walls of the support housing.
Claim 3
Dependent Claim
43 words
Support housing according to claim 1, wherein the support housing comprises at least two housing parts, a dividing joint extending between said housing parts being located so as not to extend through said recesses in said walls for receiving the exhaust gas turbochargers.
Claim 4
Dependent Claim
57 words
Support housing according to claim 2, wherein the support housing is divided in planes extending in parallel to an axis extending in a direction of a common surface normal line from planes defined by longitudinal axes of said exhaust gas turbochargers, and wherein the exhaust gas turbochargers are fastened to lateral walls of said box-type supporting device.
Claim 5
Dependent Claim
46 words
Support housing according to claim 1, wherein the support housing is divided into two substantially symmetrical housing parts along a plane extending through an axis extending in a direction of a common surface normal line from planes defined by longitudinal axes of said exhaust gas turbochargers.
Claim 6
Dependent Claim
67 words
Support housing according claim 1, wherein the support housing is formed of two housing parts centrically symmetrical with respect to an axis extending in a direction of a common surface normal line from planes defined by longitudinal axes of said exhaust gas turbochargers, the exhaust gas turbochargers being arranged on said centrically symmetrical housing parts in a centrically symmetrical manner with respect to the central perpendicular axis.
Claim 7
Dependent Claim
73 words
Support housing according to claim 2, wherein exhaust gas turbochargers for a two-stage charging are assigned to each of the housing parts respectively, and wherein in the direction of an axis extending in a direction of a common surface normal line from planes defined by longitudinal axes of said exhaust gas turbochargers, horizontally extending longitudinal axed of the exhaust gas turbochargers are each disposed at an acute angle with respect to one another.
Claim 8
Dependent Claim
126 words
A support for exhaust gas turbochargers which is arranged on an internal-combustion engine, the exhaust gas turbochargers each having two blade wheels arranged on a common shaft, one of said two blade wheels being arranged in a compressor housing and the other of said two blade wheels being arranged in a turbine housing, comprising: a support housing constructed as a box-type supporting device forming a hollow space therein, said exhaust gas turbochargers being fastened on said box-type supporting device such that the compressor housings are arranged outside said hollows space and the turbine housings are arranged inside said hollow space; and wherein said box-type supporting device has a bearing housing portion formed integrally therewith for supporting the common shaft of each of said exhaust gas turbochargers.
Claim 9
Dependent Claim
126 words
A support for exhaust gas turbochargers which is arranged on an internal-combustion engine, the exhaust gas turbochargers each having two blade wheels arranged on a common shaft, one of said two blade wheels being arranged in a compressor housing and the other of said two blade wheels being arranged in a turbine housing, comprising: a support housing constructed as a box-type supporting device forming a hollow space therein, said exhaust gas turbochargers being fastened on said box-type supporting device such that the compressor housings are arranged outside said hollows space and the turbine housings are arranged inside said hollow space; and wherein said box-type supporting device has a bearing housing portion formed integrally therewith for supporting the common shaft of each of said exhaust gas turbochargers.
References Cited (Backward Citations)
US2582916A
Cited
US3673798A
Cited
FR2363699A1
Cited
EP0014778A1
Cited
US4344289A
Cited
DE3005655A1
Cited
US4400945A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1999-06-25 | 1999-12-25 | 2000-06-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2003-06-25 | 2003-12-25 | 2004-06-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2007-06-25 | 2007-12-25 | 2008-06-25 | $7700.00 | Window Closed / Lapsed |