DE3264702D1 - Regulating device for a gas turbine liquid fuel supply system - Google Patents

Regulating device for a gas turbine liquid fuel supply system

Info

Publication number
DE3264702D1
DE3264702D1 DE8282400060T DE3264702T DE3264702D1 DE 3264702 D1 DE3264702 D1 DE 3264702D1 DE 8282400060 T DE8282400060 T DE 8282400060T DE 3264702 T DE3264702 T DE 3264702T DE 3264702 D1 DE3264702 D1 DE 3264702D1
Authority
DE
Germany
Prior art keywords
gas turbine
supply system
fuel supply
liquid fuel
regulating device
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
Application number
DE8282400060T
Other languages
German (de)
English (en)
Inventor
Jean-Luc Les Trois Ri Fondacci
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3264702D1 publication Critical patent/DE3264702D1/de
Expired 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/38—Control of fuel supply characterised by throttling and returning of fuel to sump

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
  • Feeding And Controlling Fuel (AREA)
DE8282400060T 1981-01-19 1982-01-14 Regulating device for a gas turbine liquid fuel supply system Expired DE3264702D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8100853A FR2509374B1 (fr) 1981-01-19 1981-01-19 Dispositif de regulation de debit pour systeme d'alimentation en combustible liquide de moteur a turbine a gaz

Publications (1)

Publication Number Publication Date
DE3264702D1 true DE3264702D1 (en) 1985-08-22

Family

ID=9254267

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8282400060T Expired DE3264702D1 (en) 1981-01-19 1982-01-14 Regulating device for a gas turbine liquid fuel supply system

Country Status (5)

Country Link
US (1) US4435957A (enExample)
EP (1) EP0056758B1 (enExample)
JP (1) JPS57137620A (enExample)
DE (1) DE3264702D1 (enExample)
FR (1) FR2509374B1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9316918U1 (de) * 1993-11-05 1994-01-13 Karl Dungs GmbH & Co, 73660 Urbach Mehrfachstellgerät mit eingangsseitigem Regler
FR2869642B1 (fr) * 2004-04-28 2006-07-21 Eurocopter France Dispositif et procede de regulation en acceleration ou en deceleration du debit carburant d'un turbomoteur
FR2874055B1 (fr) * 2004-08-04 2006-11-24 Hispano Suiza Sa Commande de dosage a deux lois de regulation dissociees pour regulateur de secours
RU2287075C1 (ru) * 2005-04-11 2006-11-10 ОАО "Омское машиностроительное конструкторское бюро" Система топливопитания и регулирования двигателя

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB592769A (en) * 1945-05-28 1947-09-29 H M Hobson Aircraft & Motor Co Improvements in servo motors applicable, for example, to fuel systems for combustionturbines
FR924558A (fr) * 1945-03-30 1947-08-08 Lucas Ltd Joseph Perfectionnements aux dispositifs d'alimentation en carburant liquide des moteurs àcombustion interne
FR1042608A (fr) * 1949-08-18 1953-11-03 Rolls Royce Perfectionnements aux appareillages d'alimentation en combustible pour moteurs à turbine à gaz
FR1045216A (fr) * 1950-11-17 1953-11-24 Lucas Ltd Joseph Dispositif de contrôle automatique de l'alimentation de moteurs en carburant liquide
US2869322A (en) 1954-02-18 1959-01-20 Sperry Rand Corp Fuel control system for gas turbine engines under steady-state operating conditions
GB773148A (en) * 1954-03-25 1957-04-24 Rolls Royce Improvements relating to fuel systems for gas turbine engine installations
US2983100A (en) * 1956-03-16 1961-05-09 Gen Motors Corp Fuel control system
US2909896A (en) * 1956-09-21 1959-10-27 United Aircraft Corp Emergency fuel control
US3106934A (en) * 1958-12-24 1963-10-15 Bendix Corp Integrating and proportional flow control apparatus
FR1311898A (fr) * 1961-10-11 1962-12-14 Rolls Royce Circuit de commande du carburant de post-combustion pour turbo-moteur à gaz
US3195308A (en) 1962-10-17 1965-07-20 Bendix Corp Fuel control for combustion engine
US3167082A (en) * 1962-12-27 1965-01-26 William J Oliphant Pressure regulating valve
US3374800A (en) 1963-03-21 1968-03-26 Holley Carburetor Co Gas turbine engine control having by-pass valve means
US3434395A (en) 1964-10-26 1969-03-25 Holley Carburetor Co Pressure responsive mechanism
GB1156796A (en) * 1965-11-26 1969-07-02 Plessey Co Ltd Improvements in or relating to Fuel Systems for Gas Turbine Engines Operating at Variable Pressure.
GB1206944A (en) * 1966-09-16 1970-09-30 Lucas Industries Ltd Fuel systems for gas turbine engines
GB1253203A (enExample) 1967-10-19 1971-11-10
FR1554025A (enExample) * 1968-01-09 1969-01-17
GB1271940A (en) * 1968-07-18 1972-04-26 Dowty Fuel Syst Ltd Pressure ratio control system for a gas turbine engine
US3777482A (en) 1971-11-30 1973-12-11 Colt Ind Operating Corp Turbine engine control system
GB1492976A (en) 1974-05-21 1977-11-23 Lucas Industries Ltd Fuel control system for gas turbine engine
US4220000A (en) 1977-06-18 1980-09-02 Lucas Industries Limited Fuel control system for a gas turbine engine

Also Published As

Publication number Publication date
US4435957A (en) 1984-03-13
EP0056758A1 (fr) 1982-07-28
FR2509374B1 (fr) 1986-02-21
FR2509374A1 (fr) 1983-01-14
JPH0218415B2 (enExample) 1990-04-25
JPS57137620A (en) 1982-08-25
EP0056758B1 (fr) 1985-07-17

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee