US5943864A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Exhaust gas turbocharger for an internal combustion engine
Assignee: Mercedes-Benz AG
•
Filing: 1997-05-05
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Granted: 1999-08-31
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Expires: 2017-05-05
Abstract
Abstract In an exhaust gas turbocharger for an internal combustion engine with a turbine casing including a turbine inlet structure with two flow passages separated by a partition, a turbine control valve is arranged in the partition and is in communication with a turbine bypass flow passage, which is disposed in the partition and extends to the turbine outlet for discharging exhaust gases from at least one of the two turbine inlet flow passages to the turbine outlet under the control of the turbine bypass valve.
Inventors
- 👤 Siegfried Sumser
- 👤 Erwin Schmidt
- 👤 Helmut Finger
- 👤 Hong Son Truong
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 14:27
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/12; F02B37/18; F02B37/183; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/148; F02B37/02; F02B37/025; F02B29/00; F02B29/04; F02B29/0406; F02M; F02M26/00; F02M26/02; F02M26/04; F02M26/05; F02M26/09; F02M26/13; F02M26/37; F02M26/40; F05; F05D; F05D2220/00; F05D2220/40; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
107 words
An exhaust gas turbocharger for an internal combustion engine including a turbine with a turbine casing and a rotor disposed in said turbine casing, said turbine casing having at least two turbine inlet passages which are separated by a partition, a turbine bypass passage formed in said partition and including a control valve in communication with a branch-off line extending to a turbine outlet for removing exhaust gas from at least one of said turbine inlet passages, said control valve being capable of alternatively establishing and interrupting flow communication between one of the two turbine inlet passages or both inlet passages simultaneously and said turbine bypass passage.
Claim 2
Dependent Claim
107 words
An exhaust gas turbocharger for an internal combustion engine including a turbine with a turbine casing and a rotor disposed in said turbine casing, said turbine casing having at least two turbine inlet passages which are separated by a partition, a turbine bypass passage formed in said partition and including a control valve in communication with a branch-off line extending to a turbine outlet for removing exhaust gas from at least one of said turbine inlet passages, said control valve being capable of alternatively establishing and interrupting flow communication between one of the two turbine inlet passages or both inlet passages simultaneously and said turbine bypass passage.
Claim 3
Dependent Claim
61 words
An exhaust gas turbocharger according to claim 1, wherein a section of said turbine bypass passage formed by said partition includes openings for providing said communication between said turbine inlet passages and said control valve, said control valve comprising a closure element cooperating with said openings for controlling the flow communication between said turbine inlet passages and said turbine bypass passage.
Claim 4
Dependent Claim
45 words
An exhaust gas turbocharger according to claim 2, wherein said section of said turbine bypass passage comprises a cylindrical sleeve and said control valve includes a rotary spool, said rotary spool having flow passages which can be brought into alignment with openings in said sleeve.
Claim 5
Dependent Claim
73 words
An exhaust gas turbocharger according to claim 1, wherein said turbine inlet passages have a different flow cross-section and a group of exhaust pipes from at least two cylinders of the internal combustion engine is combined and connected to each turbine inlet passage and an exhaust gas recirculating line which is connected to a charge air intake duct of the internal combustion engine branches off the inlet passage having the smaller flow cross-section.
Claim 6
Dependent Claim
76 words
An exhaust gas turbocharger according to claim 1, wherein said two turbine inlet passages have approximately the same flow cross-section and are connected via a connecting line to a collection chamber in which the exhaust gases of the internal combustion engine are collected, a flow quantity regulating device is arranged in one of the connecting lines and an exhaust gas recirculation line extends between the other of said connecting lines and said charge air intake duct.
Claim 7
Dependent Claim
53 words
An exhaust gas turbocharger according to claim 1, wherein said turbine bypass passage extends to an annular passage which is formed in the turbine casing at the turbine outlet and from which the exhaust gas emerges approximately parallel to the main direction of flow of the exhaust gas flowing out of said rotor.
Claim 8
Dependent Claim
33 words
An exhaust gas turbocharger according to claim 1, wherein said control valve is connected to a valve control unit controlling said valve as a function of operating parameters of the internal combustion engine.
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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) | 2002-08-30 | 2003-03-01 | 2003-08-31 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2006-08-30 | 2007-03-01 | 2007-08-31 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2010-08-30 | 2011-03-01 | 2011-08-31 | $7700.00 | Window Closed / Lapsed |