FR2406079A1 - Dispositif de regulation de turbine a gaz - Google Patents

Dispositif de regulation de turbine a gaz

Info

Publication number
FR2406079A1
FR2406079A1 FR7730486A FR7730486A FR2406079A1 FR 2406079 A1 FR2406079 A1 FR 2406079A1 FR 7730486 A FR7730486 A FR 7730486A FR 7730486 A FR7730486 A FR 7730486A FR 2406079 A1 FR2406079 A1 FR 2406079A1
Authority
FR
France
Prior art keywords
gas turbine
fuel
combustion chamber
pressure drop
regulation 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.)
Granted
Application number
FR7730486A
Other languages
English (en)
Other versions
FR2406079B1 (fr
Inventor
Jean-Luc 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
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 FR7730486A priority Critical patent/FR2406079A1/fr
Priority to US05/950,045 priority patent/US4245468A/en
Priority to GB7840162A priority patent/GB2010405B/en
Priority to DE2844350A priority patent/DE2844350C2/de
Publication of FR2406079A1 publication Critical patent/FR2406079A1/fr
Application granted granted Critical
Publication of FR2406079B1 publication Critical patent/FR2406079B1/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
    • 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
    • F02C9/263—Control of fuel supply by means of fuel metering valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

Dispositif de régulation du débit de carburant fourni à la chambre de combustion d'une turbine à gaz. Une pompe volumétrique 1, entraînée à une vitesse de rotation proportionnelle à celle de la turbomachine, alimente en carburant la chambre de combustion à travers deux étranglements montés en cascade 4, 5, l'étranglement aval 5 ayant une section de passage pilotable; une soupape régulatrice 7 sensible à la chute de pression pa -pc à la traversée des deux étranglements 4, 5 règle un débit de fuite de carburant prélevé entre ceux-ci, pour maintenir cette chute de pression à une valeur constante. Application à la régulation de secours d'un turboréacteur d'aviation.
FR7730486A 1977-10-11 1977-10-11 Dispositif de regulation de turbine a gaz Granted FR2406079A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7730486A FR2406079A1 (fr) 1977-10-11 1977-10-11 Dispositif de regulation de turbine a gaz
US05/950,045 US4245468A (en) 1977-10-11 1978-10-10 Control device for a gas turbine
GB7840162A GB2010405B (en) 1977-10-11 1978-10-11 Gas turbine control systems
DE2844350A DE2844350C2 (de) 1977-10-11 1978-10-11 Brennstoffregelvorrichtung für Gasturbinentriebwerke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7730486A FR2406079A1 (fr) 1977-10-11 1977-10-11 Dispositif de regulation de turbine a gaz

Publications (2)

Publication Number Publication Date
FR2406079A1 true FR2406079A1 (fr) 1979-05-11
FR2406079B1 FR2406079B1 (fr) 1982-04-30

Family

ID=9196334

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7730486A Granted FR2406079A1 (fr) 1977-10-11 1977-10-11 Dispositif de regulation de turbine a gaz

Country Status (4)

Country Link
US (1) US4245468A (fr)
DE (1) DE2844350C2 (fr)
FR (1) FR2406079A1 (fr)
GB (1) GB2010405B (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0112198B1 (fr) * 1982-11-29 1986-09-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de commande et de régulation de la section d'ouverture d'une tuyère propulsive
FR2592102A1 (fr) * 1985-12-23 1987-06-26 United Technologies Corp Servomecanisme hydraulique a action instantanee
WO1991005947A1 (fr) * 1989-10-17 1991-05-02 Dowty Defence And Air Systems Limited System d'ecoulement de fluide
FR2970516A1 (fr) * 2011-01-18 2012-07-20 Snecma Dispositif de dosage de carburant equipe d’un dispositif de fixation de debit
WO2014140460A1 (fr) * 2013-03-12 2014-09-18 Turbomeca Dispositif de dosage d'un circuit d'alimentation en carburant d'un moteur

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2109469B (en) * 1981-10-15 1985-03-27 Ex Cell O Corp Fuel distribution valve flow trimming and locking means
US20020178051A1 (en) 1995-07-25 2002-11-28 Thomas G. Scavone Interactive marketing network and process using electronic certificates
ES2137102B1 (es) * 1997-02-27 2000-07-01 Turbo Propulsores Ind Sistema de control de dosificacion de combustible para motores de combustion.
US6666015B2 (en) * 2002-01-28 2003-12-23 Hamilton Sundstrand Simplified fuel control for use with a positive displacement pump
US8775245B2 (en) 2010-02-11 2014-07-08 News America Marketing Properties, Llc Secure coupon distribution
US9435311B2 (en) * 2014-05-07 2016-09-06 Woodward, Inc. Regulator flow damping

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2086031A1 (fr) * 1970-04-13 1971-12-31 Aviat Supply R Uni

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3131750A (en) * 1960-12-02 1964-05-05 Plessey Co Ltd Acceleration-control devices for use in liquid-fuel supply systems, more particularly of gas turbines
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.
US3514948A (en) * 1968-06-06 1970-06-02 Lucas Industries Ltd Fuel control systems for gas turbine engines
US3540217A (en) * 1968-06-27 1970-11-17 Bendix Corp Combustion engine fuel control
US3726086A (en) * 1971-04-09 1973-04-10 Rolls Royce Engine fuel supply control system
US3713290A (en) * 1971-05-28 1973-01-30 Nasa Gas turbine engine fuel control

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2086031A1 (fr) * 1970-04-13 1971-12-31 Aviat Supply R Uni

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0112198B1 (fr) * 1982-11-29 1986-09-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de commande et de régulation de la section d'ouverture d'une tuyère propulsive
FR2592102A1 (fr) * 1985-12-23 1987-06-26 United Technologies Corp Servomecanisme hydraulique a action instantanee
WO1991005947A1 (fr) * 1989-10-17 1991-05-02 Dowty Defence And Air Systems Limited System d'ecoulement de fluide
US5235806A (en) * 1989-10-17 1993-08-17 Pickard Gerald W Fuel flow system for a gas turbine engine
FR2970516A1 (fr) * 2011-01-18 2012-07-20 Snecma Dispositif de dosage de carburant equipe d’un dispositif de fixation de debit
WO2014140460A1 (fr) * 2013-03-12 2014-09-18 Turbomeca Dispositif de dosage d'un circuit d'alimentation en carburant d'un moteur
FR3003302A1 (fr) * 2013-03-12 2014-09-19 Turbomeca Dispositif de dosage d'un circuit d'alimentation en carburant d'un moteur

Also Published As

Publication number Publication date
DE2844350C2 (de) 1983-05-26
FR2406079B1 (fr) 1982-04-30
US4245468A (en) 1981-01-20
DE2844350A1 (de) 1979-04-12
GB2010405A (en) 1979-06-27
GB2010405B (en) 1982-03-24

Similar Documents

Publication Publication Date Title
FR2406079A1 (fr) Dispositif de regulation de turbine a gaz
FR2375729A1 (fr) Systeme regulateur de debit pour une pile a combustible
US2430264A (en) Continuous fuel injection
FR2384952A1 (fr) Circuit de distribution de combustible
US2440567A (en) Fuel supply system for internal-combustion engines
FR2450350A1 (fr) Dispositif de vanne d'arret pour un systeme de carburant de moteur a turbine a gaz
US2443527A (en) Fuel supply system
US2456605A (en) Fuel supply system
US2400415A (en) Automatic fuel control
ES460020A1 (es) Aparato de bombeo para la inyeccion de combustible destinadoal suministro de combustible a los motores de combustion in-terna.
GB1032767A (en) Improvements in or relating to control systems for liquid-fuel supply for engines
US2697909A (en) Fuel control for turbojet engines
US3514946A (en) Fuel systems for gas turbine engines
US2958376A (en) Starting control for internal combustion engines
GB1138752A (en) Improvements in and relating to hydraulic fuel control
US3563262A (en) Hydraulic speed governors
FR2363702A1 (fr) Installation de regulation du rapport des debits d'air et de carburant du melange de fonctionnement amene dans les chambres de combustion d'un moteur a combustion interne
US2683084A (en) Gaseous fuel equalizing system for nonuniformly firing engines
GB777960A (en) Improvements in or relating to gas-turbine engine fuel systems
GB785803A (en) Arrangement for regulating the flow of after-burning fuel in jet propulsion engines having a two stage combustion system
GB1212745A (en) Fuel flow control apparatus, particularly for gas turbine engines
GB760806A (en) Improvements in or relating to gas-turbine engines
GB1416767A (en) Fuel flow regulator especially for the combustion chamber of an aircraft jet engine
US2502574A (en) Control apparatus for internalcombustion engines
FR2392235A1 (fr) Installation pour regler le rapport des debits air/carburant du melange alimentant un moteur a combustion interne

Legal Events

Date Code Title Description
CL Concession to grant licences
ST Notification of lapse