GB2319305A - Turbocharger with supplementary air drive - Google Patents

Turbocharger with supplementary air drive Download PDF

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Publication number
GB2319305A
GB2319305A GB9623279A GB9623279A GB2319305A GB 2319305 A GB2319305 A GB 2319305A GB 9623279 A GB9623279 A GB 9623279A GB 9623279 A GB9623279 A GB 9623279A GB 2319305 A GB2319305 A GB 2319305A
Authority
GB
United Kingdom
Prior art keywords
turbocharger
compressor
air
engine
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB9623279A
Other versions
GB9623279D0 (en
Inventor
Philip Gerald Bevan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB9623279A priority Critical patent/GB2319305A/en
Publication of GB9623279D0 publication Critical patent/GB9623279D0/en
Publication of GB2319305A publication Critical patent/GB2319305A/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/04Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B21/00Engines characterised by air-storage chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/04Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • F02B37/10Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/02Drives of pumps; Varying pump drive gear ratio
    • F02B39/08Non-mechanical drives, e.g. fluid drives having variable gear ratio
    • F02B39/10Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27Fluid drives
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Supercharger (AREA)

Abstract

To avoid turbine lag when the throttle 22 of a turbocharged engine is opened, supplementary air is supplied under pressure to nozzles 14, that direct the air onto the rotor of the turbocharger compressor 10, to impart drive thereto until the turbine 12, reaches full operating speed. A vehicle power supply 26, powers a separate compressor 24, that pressurises a reservoir 16, having a pressure sensor 30. A proportionate valve 18, controls flow to the nozzles 14, in response to signals from a throttle responsive switch controller 20, and an engine management system 32.

Description

Turbocharger This invention relates to a turbocharger for an internal combustion engine.
A commonly used turbocharger for internal combustion engines, especially in motor vehicles for example, comprises a compressor shaft driven from a turbine powered by the engine exhaust gases. The compressor delivers compressed air to the engine in order to boost power output.
A well known problem with such turbochargers is turbine lag. Thus, when extra power, especially from idling or near idling speed, is called for by opening of the throttle, as by depression of the accelerator pedal in a motor vehicle, it takes time for the exhaust gases, the flow of which increases due to delivery of extra fuel to the engine, to build up sufficiently to drive the turbine, and thus the compressor, at the increased speed necessary to deliver an increased amount of air under pressure to the engine. As indicated, the effect is especially noticeable when opening up the engine from idling speed, when the turbine is normally effectively inoperative.
An object of the invention is to provide a solution to the problem of turbine lag.
According to the invention, there is provided apparatus for use with a turbocharger for an internal combustion engine in a vehicle, comprising a supplementary air inlet device in the turbocharger compressor housing for delivering a stream of air for driving the compressor wheel, a separate air compressor unit powered from the vehicle power supply, a compressed air reservoir storing compressed air received from the said air compressor unit and valve means associated with operation of the engine throttle controlling supply of compressed air from the reservoir to the supplementae air inlet of the turbocharger compressor while the turbine of the turbocharger builds up speed responsively to opening of the engine throttle control.
The invention is further described with reference to the accompanying drawings, in which: Figure 1 shows the overall system diagrammatically; and Figure 2 shows the compressor of a turbocharger when fitted with the supplementary air inlet.
Referring to the drawings, Figure 1 shows a typical turbocharger for the internal combustion engine of a vehicle, comprising an air compressor 10 linked by a coupling shaft to a turbine 12. In normal use, exhaust gases are drawn into the turbine generally tangentially as indicated at A, and exhaust on-axis, as indicated at B. Within the turbine 12, the exhaust gases drive the turbine wheel, which is coupled to the compressor wheel. The compressor 10 receives air on-axis, as indicated at C, and tangentially exits air under pressure, as indicated at D, to the internal combustion engine.
There exists a problem, however, known as turbine lag, because when the throttle of the engine is opened up, it takes time for the exhaust gases to build up to the pressure required to drive the turbine, and thus the compressor, at the speed appropriate for delivery of pressurised air to the engine at the rate appropriate to the throttle opening, so that there is a delayed engine response to throttle operation. This is commonly especially noticeable when starting from idling, when the turbocharger is effectively inoperative.
In accordance with the invention, therefore, a supplementary air inlet in the form of a nozzle 14 is located in the compressor housing, as shown in Figure 2.
Referring back to Figure 1, the nozzle 14 receives air from a compressed air reservoir 16 when a valve 18 is opened. This valve 18 may conveniently be opened responsively to the operation of a switch controller 20, which could be a microswitch but is preferably a proportional controller such as a potentiometer, associated with the throttle 22, e.g. an accelerator pedal. In this way the turbocharger compressor is substantially instantly or at least very quickly brought up to speed when the throttle is opened up.
The compressed air reservoir is maintained by a separate compressor unit 24, which is powered from the vehicle power supply 26 via a suitable switch 28 which closes only when the compressor unit 24 requires to be driven to maintain pressure in the reservoir 16, for example by means of a reservoir pressure sensor 30.
As the turbine 12 of the turbocharger builds up to full operating speed responsively to increase in the pressure of the exhaust gases, in turn responsively to increased fuel delivery to the engine brought about by opening the throttle, the drive to the turbocharger compressor 10 via the supplementary air inlet or nozzle 14 requires to be gradually reduced and then stopped to allow normal operation of the turbocharger. To this end, the valve 18 is conveniently a gate valve or other proportionate valve which is gradually closed down under the control of a feedback signal from the exhaust system, or more conveniently by the engine management system 32, which detects and normally controls the behaviour of the turbocharger.
In a new vehicle, it is apparent that the engine management system may also control delivery of supply of compressed air to the nozzle 14 when the throttle is opened up. The present invention, however, is also applicable as a modification to an existing turbocharger.
The invention also relates to a modified turbocharger as aforesaid and a vehicle when fitted with said turbocharger.

Claims (9)

Claims
1. Apparatus for use with a turbocharger for an internal combustion engine in a vehicle, comprising a supplementary air inlet device in the turbocharger compressor housing for delivering a stream of air for driving the compressor wheel, a separate air compressor unit powered from the vehicle power supply, a compressed air reservoir storing compressed air received from the said air compressor unit and valve means associated with operation of the engine throttle for controlling supply of compressed air from the reservoir to the supplementary air inlet of the turbocharger compressor while the turbine of the turbocharger builds up speed responsively to opening of the engine throttle control.
2. Apparatus according to claim 1, wherein the said valve means is a proportional valve.
3. Apparatus according to claim 1 or claim 2, wherein opening of the valve means is governed by a controller operable by the engine throttle.
4. Apparatus according to claim 3, wherein the controller is a proportionate controller.
5. Apparatus according to any of claims 2 to 4, in which closing of the valve means is controlled in proportionate relationship to build up of exhaust gas pressure at the turbocharger turbine.
6. Apparatus according to any of claims 2 to 5, wherein closing of the valve is controlled by an engine management system.
7. Apparatus substantially as hereinbefore described with reference to the accompanying drawings.
8. A turbocharger equipped with the apparatus of any of claims 1 to 7.
9. A vehicle equipped with the turbocharger of claim 8.
GB9623279A 1996-11-08 1996-11-08 Turbocharger with supplementary air drive Withdrawn GB2319305A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9623279A GB2319305A (en) 1996-11-08 1996-11-08 Turbocharger with supplementary air drive

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9623279A GB2319305A (en) 1996-11-08 1996-11-08 Turbocharger with supplementary air drive

Publications (2)

Publication Number Publication Date
GB9623279D0 GB9623279D0 (en) 1997-01-08
GB2319305A true GB2319305A (en) 1998-05-20

Family

ID=10802638

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9623279A Withdrawn GB2319305A (en) 1996-11-08 1996-11-08 Turbocharger with supplementary air drive

Country Status (1)

Country Link
GB (1) GB2319305A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2789120A1 (en) * 1999-01-29 2000-08-04 Daimler Chrysler Ag INTERNAL COMBUSTION ENGINE HAVING AN EXHAUST GAS TURBOCHARGER
WO2007023326A1 (en) * 2005-08-23 2007-03-01 Shap Spa Solar Heat And Power Cogeneration plant

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0174867A2 (en) * 1984-09-14 1986-03-19 AlliedSignal Inc. Hydraulic assist turbocharger system and method for its operation
GB2170866A (en) * 1985-02-09 1986-08-13 Man B & W Diesel Gmbh Turbocharger
WO1991017347A1 (en) * 1990-05-04 1991-11-14 Allied-Signal Inc. Control logic for exhaust gas driven turbocharger
US5113658A (en) * 1990-05-21 1992-05-19 Allied-Signal, Inc. Hydraulic assist turbocharger system
GB2277129A (en) * 1993-04-13 1994-10-19 Daimler Benz Ag Exhaust gas turbocharger
US5461860A (en) * 1993-10-09 1995-10-31 Abb Management Ag Exhaust gas turbocharger and method of operation

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0174867A2 (en) * 1984-09-14 1986-03-19 AlliedSignal Inc. Hydraulic assist turbocharger system and method for its operation
GB2170866A (en) * 1985-02-09 1986-08-13 Man B & W Diesel Gmbh Turbocharger
WO1991017347A1 (en) * 1990-05-04 1991-11-14 Allied-Signal Inc. Control logic for exhaust gas driven turbocharger
US5113658A (en) * 1990-05-21 1992-05-19 Allied-Signal, Inc. Hydraulic assist turbocharger system
GB2277129A (en) * 1993-04-13 1994-10-19 Daimler Benz Ag Exhaust gas turbocharger
US5461860A (en) * 1993-10-09 1995-10-31 Abb Management Ag Exhaust gas turbocharger and method of operation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2789120A1 (en) * 1999-01-29 2000-08-04 Daimler Chrysler Ag INTERNAL COMBUSTION ENGINE HAVING AN EXHAUST GAS TURBOCHARGER
WO2007023326A1 (en) * 2005-08-23 2007-03-01 Shap Spa Solar Heat And Power Cogeneration plant

Also Published As

Publication number Publication date
GB9623279D0 (en) 1997-01-08

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