JPH052821B2 - - Google Patents

Info

Publication number
JPH052821B2
JPH052821B2 JP61188360A JP18836086A JPH052821B2 JP H052821 B2 JPH052821 B2 JP H052821B2 JP 61188360 A JP61188360 A JP 61188360A JP 18836086 A JP18836086 A JP 18836086A JP H052821 B2 JPH052821 B2 JP H052821B2
Authority
JP
Japan
Prior art keywords
fuel
chamber
piston
servo
valve
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.)
Expired - Lifetime
Application number
JP61188360A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6258021A (ja
Inventor
Boogan Rutsukusu Jon
Aran Rotsukusurei Ratsuseru
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of JPS6258021A publication Critical patent/JPS6258021A/ja
Publication of JPH052821B2 publication Critical patent/JPH052821B2/ja
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/22—Fuel supply systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00—Rotary-piston machines or pumps
    • F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C2/12—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C2/14—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C2/18—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with similar tooth forms

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
JP61188360A 1985-09-04 1986-08-11 ガスタ−ビンエンジンの燃料系 Granted JPS6258021A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8521993 1985-09-04
GB8521993A GB2180005B (en) 1985-09-04 1985-09-04 Fuel systems for gas turbine engines

Publications (2)

Publication Number Publication Date
JPS6258021A JPS6258021A (ja) 1987-03-13
JPH052821B2 true JPH052821B2 (OSRAM) 1993-01-13

Family

ID=10584724

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61188360A Granted JPS6258021A (ja) 1985-09-04 1986-08-11 ガスタ−ビンエンジンの燃料系

Country Status (5)

Country Link
US (1) US4760696A (OSRAM)
JP (1) JPS6258021A (OSRAM)
DE (1) DE3628815A1 (OSRAM)
FR (1) FR2586755B1 (OSRAM)
GB (1) GB2180005B (OSRAM)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4928491A (en) * 1988-06-29 1990-05-29 United States Of America As Represented By The Secretary Of Air Force Fuel supply device for supplying fuel to an engine combustor
US4876857A (en) * 1988-08-15 1989-10-31 Allied-Signal Inc. Shut off/pressure regulating valve for turbine engine
GB8906060D0 (en) * 1989-03-16 1989-07-05 Lucas Ind Plc Gas turbine engine fuel control system,and metering valve therefor
GB9022387D0 (en) * 1990-10-16 1990-11-28 Lucas Ind Plc Fuel control system for a gas turbine engine
GB9203770D0 (en) * 1992-02-21 1992-04-08 Lucas Ind Plc Fuel control system
US5241826A (en) * 1992-07-21 1993-09-07 Stearns Charles F Fixed geometry variable displacement pump system
US5896737A (en) * 1997-06-16 1999-04-27 United Technologies Corporation Combined pressure regulating and fuel flow system
EP2295768B1 (en) 1998-01-08 2012-10-31 United Technologies Corporation Bi-level hydraulic pressurizing system
US6675570B2 (en) 2000-06-15 2004-01-13 Argo-Tech Corporation Low-cost general aviation fuel control system
FR2816005B1 (fr) * 2000-10-26 2003-01-17 Snecma Moteurs Circuit economiseur de debit de carburant
US6931831B2 (en) * 2002-06-18 2005-08-23 Jansen's Aircraft Systems Controls, Inc. Distributor purge valve
US7527068B2 (en) 2002-06-18 2009-05-05 Jansen's Aircraft Systems Controls, Inc. Valve with swirling coolant
US7200985B2 (en) * 2003-07-15 2007-04-10 Honeywell International Inc. Fuel delivery system having an ecology valve
US20060053796A1 (en) * 2004-09-10 2006-03-16 Honeywell International Inc. Method and apparatus for adding a secondary fluid flow to a gas turbine engine control fuel line
EP1825115A1 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
FR2931885B1 (fr) * 2008-05-29 2013-09-27 Hispano Suiza Sa Circuit de carburant de turbomachine
US8739811B2 (en) 2011-02-07 2014-06-03 Honeywell International Inc. Direct metering fuel system with constant servo flow
FR2974149B1 (fr) * 2011-04-14 2015-09-25 Snecma Circuit de carburant comportant des moyens de controle d'une pompe
US8567201B2 (en) * 2011-06-28 2013-10-29 Triumph Engine Control Systems, Llc Ecology system for draining the manifold of a gas turbine engine
US20140175027A1 (en) * 2012-12-21 2014-06-26 United Technologies Corporation Fuel system with electrically heated filter screen
FR3010141B1 (fr) * 2013-09-03 2018-01-05 Safran Aircraft Engines Systeme carburant a injecteurs multipoints pour une turbomachine
FR3035155B1 (fr) * 2015-04-17 2018-05-11 Safran Aircraft Engines Circuit de distribution de carburant de turbomachine a encombrement reduit
FR3040440B1 (fr) * 2015-09-01 2019-07-05 Safran Aircraft Engines Dispositif d'alimentation d'un moteur en carburant, dote d'un systeme de protection reduit contre les surpressions
US12372032B1 (en) 2024-08-01 2025-07-29 Rtx Corporation Gas turbine engine with controlled return of fuel to power accessories and retrofitting method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126942A (en) * 1964-03-31 X f fuel supply systems for spill burner nozzles
US2835323A (en) * 1953-10-13 1958-05-20 Plessey Co Ltd Fuel systems for internal combustion engines and gas turbines
US3332234A (en) * 1966-03-24 1967-07-25 John P Lavash Fuel delivery systems
US3858390A (en) * 1973-06-04 1975-01-07 Garrett Corp Power turbine nozzle control system
GB1485412A (en) * 1975-01-27 1977-09-14 Rolls Royce Fuel systems for gas turbine engines
US4245964A (en) * 1978-11-08 1981-01-20 United Technologies Corporation Efficiency fluid pumping system including sequential unloading of a plurality of pumps by a single pressure responsive control valve
US4607486A (en) * 1983-12-02 1986-08-26 United Technologies Corporation Centrifugal main fuel pump

Also Published As

Publication number Publication date
FR2586755A1 (fr) 1987-03-06
US4760696A (en) 1988-08-02
GB2180005B (en) 1989-03-01
GB8521993D0 (en) 1985-10-09
FR2586755B1 (fr) 1994-03-11
GB2180005A (en) 1987-03-18
DE3628815A1 (de) 1987-03-05
JPS6258021A (ja) 1987-03-13

Similar Documents

Publication Publication Date Title
JPH052821B2 (OSRAM)
US5116362A (en) Fuel metering and actuation system
US5996331A (en) Passive turbine coolant regulator responsive to engine load
US4452037A (en) Air purge system for gas turbine engine
US7234293B2 (en) Fuel supply system
US4305255A (en) Combined pilot and main burner
US7966995B2 (en) Dual level pressurization control based on fuel flow to one or more gas turbine engine secondary fuel loads
US2619162A (en) Fuel system for compressor gas turbine plants
JPH06504602A (ja) ガスタービン流体用熱交換装置
EP3735560B1 (en) Gas turbine combustor comprising a torch igniter and method of delivering fuel to a torch igniter
JPH0135162B2 (OSRAM)
JPS592773B2 (ja) 燃料供給制御装置
EP3922830B1 (en) Fuel metering system
US4433539A (en) Means for controlling air scavenge pressure in the bearing compartment of gas turbines
US4344281A (en) Manually operated metering valve for a fuel control
US3486458A (en) Centrifugal pumping apparatus
US3834160A (en) Light-off transient control for an augmented gas turbine engine
US3390522A (en) Fuel systems for gas turbine engines operating at variable pressure
RU2272964C2 (ru) Способ и устройство для подачи топлива в камеру сгорания
US3921390A (en) Fuel controller for gas turbine engine
PL115576B1 (en) Apparatus for combustion engine supercharging in particular for self-ignited combustion engines
US3508395A (en) Control system for motor vehicle type gas turbine engine
US20070051089A1 (en) Augmentor flow control with thermal recirculation function and method of thermal recirculation control using augmentor valves
US3613375A (en) Rocket engine propellant feeding and control system
JP2002201967A (ja) 燃料計量ユニットによって制御される２レベル加圧バルブ