US5758500A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Exhaust gas turbochanger for an internal combustion engine
Assignee: Mercedes Benz Group AG
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Filing: 1997-04-17
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Granted: 1998-06-02
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Expires: 2017-04-17
Abstract
Abstract In an exhaust gas turbocharger for an internal combustion engine comprising a compressor and a turbine with an impeller and a turbine wheel mounted on a common shaft, the exhaust turbine includes radial and semi-axial flow passages through which the exhaust gas is conducted to the turbine wheel and which are separated by a guide ring, and an annular sleeve is mounted in the turbine housing so as to be slideable therein along the axis of the turbine wheel across the radial flow passage for closing the radial flow passage of the turbine.
Inventors
- 👤 Siegfried Sumser
- 👤 Horst Hanauer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 23:31
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/167; F01D17/141; F02; F02B; F02B37/00; F02B37/02; F02B37/025; F02B37/12; F02B37/24; F05; F05D; F05D2220/00; F05D2220/40; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
198 words
An exhaust gas turbocharger for an internal combustion engine, comprising a compressor having an impeller and a turbine having a turbine wheel and being mounted on opposite sides of a turbine housing, said impeller and said turbine wheel being mounted on a common shaft rotatably supported in said turbine housing, said exhaust gas turbine having a housing with radial and semi-axial flow passages having annular nozzles leading to said turbine wheel and being separated by a flow guide ring, an annular sleeve mounted in said turbine housing so as to be slideable therein along the axis of said turbine wheel so as to extend across and block at least one of said flow passages for controlling the exhaust gas flow through said at least one flow passage, a guide blade ring disposed at an end face of said annular sleeve adjacent said flow guide ring such that the guide blades of said guide blade ring are normally disposed in said one flow passage for guiding the exhaust gas onto said turbine wheel, said flow guide ring having an axially extending annular recess structure receiving said guide blade ring when said annular sleeve is in a nozzle closing position.
Claim 2
Dependent Claim
198 words
An exhaust gas turbocharger for an internal combustion engine, comprising a compressor having an impeller and a turbine having a turbine wheel and being mounted on opposite sides of a turbine housing, said impeller and said turbine wheel being mounted on a common shaft rotatably supported in said turbine housing, said exhaust gas turbine having a housing with radial and semi-axial flow passages having annular nozzles leading to said turbine wheel and being separated by a flow guide ring, an annular sleeve mounted in said turbine housing so as to be slideable therein along the axis of said turbine wheel so as to extend across and block at least one of said flow passages for controlling the exhaust gas flow through said at least one flow passage, a guide blade ring disposed at an end face of said annular sleeve adjacent said flow guide ring such that the guide blades of said guide blade ring are normally disposed in said one flow passage for guiding the exhaust gas onto said turbine wheel, said flow guide ring having an axially extending annular recess structure receiving said guide blade ring when said annular sleeve is in a nozzle closing position.
Claim 3
Dependent Claim
30 words
An exhaust gas turbocharger according to claim 1, wherein said annular sleeve is movable axially into firm engagement with said flow guide ring for firmly closing said one flow passage.
Claim 4
Dependent Claim
22 words
An exhaust gas turbocharger according to claim 2, wherein said flow passage controllable by said annular sleeve is said radial flow passage.
Claim 5
Dependent Claim
37 words
An exhaust gas turbocharger according to claim 1, wherein said guide blade ring is sufficiently wide that its front end remains disposed in said recess even when said annular sleeve is in a flow passage opening position.
Claim 6
Dependent Claim
30 words
An exhaust gas turbocharger according to claim 1, wherein said flow guide ring is mounted on the end of a stationary guide blade ring mounted in said semi-axial flow passage.
Claim 7
Dependent Claim
20 words
An exhaust gas turbocharger according to claim 1, wherein said flow guide ring has a radial symmetrical outer surface shape.
Claim 8
Dependent Claim
38 words
An exhaust gas turbocharger according to claim 1, wherein said annular sleeve extends axially downstream of said turbine wheel and has, downstream of said turbine wheel, a slightly conical inner shape so as to form a diffuser structure.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2001-06-01 | 2001-12-01 | 2002-06-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2005-06-01 | 2005-12-01 | 2006-06-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2009-06-01 | 2009-12-01 | 2010-06-02 | $7700.00 | Window Closed / Lapsed |