US4833886A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Internal combustion engine supercharged by means of an exhaust gas turbocharger
Assignee: BBC Brown Boveri AG Switzerland
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Filing: 1988-09-07
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Granted: 1989-05-30
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Expires: 2008-09-07
Abstract
Abstract In a diesel engine (1) supercharged by an exhaust gas turbocharger, both the compressor (4) and the turbine (3) of the supercharger are designed for full engine power and speed. A by-pass duct (8) provided with a non-return valve (9) and a control device (10) is connected between the exhaust gas duct (9) and the boost air duct (5). The turbine (3) is equipped with means (11, 12, 13) for varying the turbine equivalent cross-section. At part load, the equivalent cross-section and, simultaneously, the by-pass duct cross-section are varied in order to operate as near as possible to the surge limit of the compressor (4).
Inventors
- 👤 Erwin Meier
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 00:47
CPC Classifications
F; F02; F02B; F02B37/00; F02B37/04; F02B37/10; F02B37/12; F02B37/16; F02B37/22; F02B3/00; F02B3/06; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
203 words
Reciprocating internal combustion engine of the type supercharged by means of an exhaust gas turbocharger, comprising: a compressor having predetermined pressure mass flow characteristics and a bypass duct for matching the pressure mass flow characteristics to predetermined operating characteristics of the engine so as to effect stable compressor operation and optimum compressor efficiency at maximum speed and power of the engine, said bypass duct connected to a boost air duct and an exhaust gas duct, said boost air duct connected to the compressor outlet and an engine inlet, said exhaust gas duct connected to an engine outlet and to a plurality of inlet ducts, each of said plurality of inlet ducts having a first end directly connected only to said exhaust gas duct, said plurality of inlet ducts having a second end directly connected only to a plurality of nozzle segments connected to said turbine, said bypass duct being provided with a control device and a nonreturn valve, and a sector regulator for varying admission of exhaust gases to the turbine, wherein the turbine has an equivalent nozzle area for obtaining optimum turbine power output and boost pressure at said maximum engine power and speed and is driven only by said exhaust gases.
Claim 2
Dependent Claim
203 words
Reciprocating internal combustion engine of the type supercharged by means of an exhaust gas turbocharger, comprising: a compressor having predetermined pressure mass flow characteristics and a bypass duct for matching the pressure mass flow characteristics to predetermined operating characteristics of the engine so as to effect stable compressor operation and optimum compressor efficiency at maximum speed and power of the engine, said bypass duct connected to a boost air duct and an exhaust gas duct, said boost air duct connected to the compressor outlet and an engine inlet, said exhaust gas duct connected to an engine outlet and to a plurality of inlet ducts, each of said plurality of inlet ducts having a first end directly connected only to said exhaust gas duct, said plurality of inlet ducts having a second end directly connected only to a plurality of nozzle segments connected to said turbine, said bypass duct being provided with a control device and a nonreturn valve, and a sector regulator for varying admission of exhaust gases to the turbine, wherein the turbine has an equivalent nozzle area for obtaining optimum turbine power output and boost pressure at said maximum engine power and speed and is driven only by said exhaust gases.
Claim 3
Dependent Claim
194 words
Reciprocating internal combustion engine of the type supercharged by means of an exhaust gas turbocharger, comprising: a compressor having predetermined pressure mass flow characteristics and a bypass duct for matching the pressure mass flow characteristics to predetermined operating characteristics of the engine so as to effect stable compressor operation and optimum compressor efficiency at maximum speed and power of the engine, said bypass duct connected to a boost air duct and an exhaust gas duct, said boost air duct connected to the compressor outlet and an engine outlet and to a plurality of inlet ducts, each of said plurality of inlet ducts having a first end directly connected only to said exhaust gas duct, said plurality of inlet ducts having a second end directly connected only to a plurality of nozzle segments connected to said turbine, said bypass duct being provided with a control device and a nonreturn valve, and a sector regulator for varying admission of exhaust gases to the turbine, wherein the turbine has an equivalent nozzle area for obtaining optimum turbine power output and boost pressure at said maximum engine power and speed and is driven only by said exhaust gases.
Claim 4
Dependent Claim
194 words
Reciprocating internal combustion engine of the type supercharged by means of an exhaust gas turbocharger, comprising: a compressor having predetermined pressure mass flow characteristics and a bypass duct for matching the pressure mass flow characteristics to predetermined operating characteristics of the engine so as to effect stable compressor operation and optimum compressor efficiency at maximum speed and power of the engine, said bypass duct connected to a boost air duct and an exhaust gas duct, said boost air duct connected to the compressor outlet and an engine outlet and to a plurality of inlet ducts, each of said plurality of inlet ducts having a first end directly connected only to said exhaust gas duct, said plurality of inlet ducts having a second end directly connected only to a plurality of nozzle segments connected to said turbine, said bypass duct being provided with a control device and a nonreturn valve, and a sector regulator for varying admission of exhaust gases to the turbine, wherein the turbine has an equivalent nozzle area for obtaining optimum turbine power output and boost pressure at said maximum engine power and speed and is driven only by said exhaust gases.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-05-29 | 1992-11-28 | 1993-05-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-05-29 | 1996-11-28 | 1997-05-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-05-29 | 2000-11-28 | 2001-05-30 | $7700.00 | Window Closed / Lapsed |