FR2284040A1 - Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed - Google Patents

Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed

Info

Publication number
FR2284040A1
FR2284040A1 FR7430817A FR7430817A FR2284040A1 FR 2284040 A1 FR2284040 A1 FR 2284040A1 FR 7430817 A FR7430817 A FR 7430817A FR 7430817 A FR7430817 A FR 7430817A FR 2284040 A1 FR2284040 A1 FR 2284040A1
Authority
FR
France
Prior art keywords
air
diesel engine
pressure control
bleed air
drive 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.)
Granted
Application number
FR7430817A
Other languages
French (fr)
Other versions
FR2284040B1 (en
Inventor
Joseph Plotkowiak
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7430817A priority Critical patent/FR2284040A1/en
Publication of FR2284040A1 publication Critical patent/FR2284040A1/en
Application granted granted Critical
Publication of FR2284040B1 publication Critical patent/FR2284040B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D23/00—Controlling engines characterised by their being supercharged
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/148—Blades with variable camber, e.g. by ejection of fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
    • F02B37/025—Multiple scrolls or multiple gas passages guiding the gas to the pump drive
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/16—Control of the pumps by bypassing charging air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • F02B37/10—Engines 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
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

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

Abstract

The turbo charger admits air to the diesel engine and is driven by a shaft which is powered by a turbine. Exhaust gases from the engine power the expansion turbine. There is an air bleed from the air inlet to the engine this bleed being controlled by a throttle valve. The air is bled from the diffuser of the turbo charger and injected from the diffuser of the expansion turbine in order to give adequate control. The control of the throttle valve is linked mechanically to a governor, to maintain a constant speed of the turbo charger. The bleed air is injected between exhaust distribution blades (25) through an annular slot (27) from an annular chamber (26). The air is injected at a small angle to the exhaust flow and increases the speed of this flow.
FR7430817A 1974-09-06 1974-09-06 Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed Granted FR2284040A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7430817A FR2284040A1 (en) 1974-09-06 1974-09-06 Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7430817A FR2284040A1 (en) 1974-09-06 1974-09-06 Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed

Publications (2)

Publication Number Publication Date
FR2284040A1 true FR2284040A1 (en) 1976-04-02
FR2284040B1 FR2284040B1 (en) 1976-12-31

Family

ID=9142997

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7430817A Granted FR2284040A1 (en) 1974-09-06 1974-09-06 Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed

Country Status (1)

Country Link
FR (1) FR2284040A1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4328672A (en) * 1979-07-11 1982-05-11 Bbc Brown, Boveri & Company Limited Bypass control apparatus for turbocharged internal-combustion engines
US4346559A (en) * 1979-07-11 1982-08-31 Bbc Brown, Boveri & Company Limited Bypass control apparatus for turbocharged internal-combustion engines
FR2503793A1 (en) * 1981-04-13 1982-10-15 Kovalevsky Evgeny Exhaust gas turbocharged automotive diesel engine - has crankshaft speed transmitter connected to addition unit input
US4367626A (en) * 1979-07-16 1983-01-11 Schwartzman Everett H Turbocharger systems
US4373336A (en) * 1979-01-31 1983-02-15 Bbc Brown, Boveri & Company, Limited Internal combustion engine having a turbo-supercharger with an automatic bypass
US4502282A (en) * 1982-07-21 1985-03-05 Usui Kokusai Sangyo Kabushiki Kaisha Turbo-charged compression ignition engine operable at small compression ratio
EP0164539A1 (en) * 1984-05-15 1985-12-18 A. S. Kongsberg Väpenfabrikk Variable flow gas turbine engine
US4674275A (en) * 1984-05-15 1987-06-23 Sigmunn Stroem Method for varying the cross-sectional flow area in a radial gas turbine inlet

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1263010A (en) * 1960-07-21 1961-06-05 M A N Turbomotoren G M B H Method and device for modifying, in fluid flow machines, the deviation given by a blade grid
FR1293459A (en) * 1961-06-28 1962-05-11 Schwitzer Corp Pressure control for turbo-compressors

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1263010A (en) * 1960-07-21 1961-06-05 M A N Turbomotoren G M B H Method and device for modifying, in fluid flow machines, the deviation given by a blade grid
FR1293459A (en) * 1961-06-28 1962-05-11 Schwitzer Corp Pressure control for turbo-compressors

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4373336A (en) * 1979-01-31 1983-02-15 Bbc Brown, Boveri & Company, Limited Internal combustion engine having a turbo-supercharger with an automatic bypass
US4328672A (en) * 1979-07-11 1982-05-11 Bbc Brown, Boveri & Company Limited Bypass control apparatus for turbocharged internal-combustion engines
US4346559A (en) * 1979-07-11 1982-08-31 Bbc Brown, Boveri & Company Limited Bypass control apparatus for turbocharged internal-combustion engines
US4367626A (en) * 1979-07-16 1983-01-11 Schwartzman Everett H Turbocharger systems
FR2503793A1 (en) * 1981-04-13 1982-10-15 Kovalevsky Evgeny Exhaust gas turbocharged automotive diesel engine - has crankshaft speed transmitter connected to addition unit input
US4502282A (en) * 1982-07-21 1985-03-05 Usui Kokusai Sangyo Kabushiki Kaisha Turbo-charged compression ignition engine operable at small compression ratio
EP0164539A1 (en) * 1984-05-15 1985-12-18 A. S. Kongsberg Väpenfabrikk Variable flow gas turbine engine
US4624104A (en) * 1984-05-15 1986-11-25 A/S Kongsberg Vapenfabrikk Variable flow gas turbine engine
US4674275A (en) * 1984-05-15 1987-06-23 Sigmunn Stroem Method for varying the cross-sectional flow area in a radial gas turbine inlet

Also Published As

Publication number Publication date
FR2284040B1 (en) 1976-12-31

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Legal Events

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TP Transmission of property
CA Change of address