FR2367917A1 - Dispositif de commande de carburant pour moteurs d'avion - Google Patents

Dispositif de commande de carburant pour moteurs d'avion

Info

Publication number
FR2367917A1
FR2367917A1 FR7721881A FR7721881A FR2367917A1 FR 2367917 A1 FR2367917 A1 FR 2367917A1 FR 7721881 A FR7721881 A FR 7721881A FR 7721881 A FR7721881 A FR 7721881A FR 2367917 A1 FR2367917 A1 FR 2367917A1
Authority
FR
France
Prior art keywords
aircraft engines
fuel
control device
fuel control
measures
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
FR7721881A
Other languages
English (en)
Other versions
FR2367917B1 (fr
Inventor
Peter David Toot
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2367917A1 publication Critical patent/FR2367917A1/fr
Application granted granted Critical
Publication of FR2367917B1 publication Critical patent/FR2367917B1/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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F02K1/48—Corrugated nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Regulation And Control Of Combustion (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

Dispositif de commande de l'alimentation en carburant du système de post-combustion d'un turboréacteur. Il comprend un détecteur de température 41 qui mesure la température à l'entrée du réacteur, un détecteur de pression 43 qui mesure la pression à la sortie du compresseur 17 et un circuit stabilisateur 39 qui agit sur la commande 38 de l'alimentation en carburant du système de post-combustion pour maintenir le fonctionnement du moteur à l'intérieur des limites de stabilité de la richesse en carburant en modifiant le programme du rapport carburant/air en réponse aux températures et pressions detectées. L'invention est applicable notamment aux moteurs d'avions à double flux et post-combustion.
FR7721881A 1976-10-18 1977-07-18 Dispositif de commande de carburant pour moteurs d'avion Granted FR2367917A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/733,093 US4128995A (en) 1976-10-18 1976-10-18 Method and apparatus for stabilizing an augmenter system

Publications (2)

Publication Number Publication Date
FR2367917A1 true FR2367917A1 (fr) 1978-05-12
FR2367917B1 FR2367917B1 (fr) 1984-06-08

Family

ID=24946199

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7721881A Granted FR2367917A1 (fr) 1976-10-18 1977-07-18 Dispositif de commande de carburant pour moteurs d'avion

Country Status (6)

Country Link
US (1) US4128995A (fr)
JP (1) JPS5351323A (fr)
CA (1) CA1083836A (fr)
DE (1) DE2732039A1 (fr)
FR (1) FR2367917A1 (fr)
GB (1) GB1580503A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0616118A1 (fr) * 1993-03-16 1994-09-21 ROLLS-ROYCE plc Protection contre l'extintion et/ou pompage aprês ingestion d'eau pour turbine à gaz

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4244183A (en) * 1978-04-27 1981-01-13 United Technologies Corporation Control means for an augmentor for a gas turbine engine
US4397148A (en) * 1980-07-02 1983-08-09 General Electric Company Control system for an augmented turbofan engine
JPS62255193A (ja) * 1986-04-28 1987-11-06 イビデン株式会社 Ｉｃカ−ド用プリント配線板
US5148671A (en) * 1990-10-17 1992-09-22 General Electric Company Fuel circulation control system
US5305599A (en) * 1991-04-10 1994-04-26 General Electric Company Pressure-ratio control of gas turbine engine
US5205116A (en) * 1991-07-19 1993-04-27 General Electric Company Compressor stall recovery apparatus
US5226287A (en) * 1991-07-19 1993-07-13 General Electric Company Compressor stall recovery apparatus
NO175284C (no) * 1992-04-02 1994-09-28 Franz Titulaer Ramme for utstilling av varer
US5544480A (en) * 1994-06-30 1996-08-13 The United States Of America As Represented By The Secretary Of The Air Force Augmentor light-off improvement
US6938404B2 (en) * 2003-09-23 2005-09-06 Rrc-Sgte Technologies, Llc Supercharged open cycle gas turbine engine
US7168254B2 (en) * 2004-02-17 2007-01-30 Honeywell International Inc. Control logic for fuel controls on APUs

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3205655A (en) * 1957-10-07 1965-09-14 Chandler Evans Inc Afterburner fuel regulator responsive to compressor discharge absolute pressure
DE1239526B (de) * 1960-09-13 1967-04-27 Gen Electric Brennstoffsteuervorrichtung fuer den Nachbrenner eines Strahltriebwerkes
US3293847A (en) * 1963-09-13 1966-12-27 Bendix Corp Coordinated main and afterburner fuel controls for gas turbine engines
US3513899A (en) * 1968-03-29 1970-05-26 United Aircraft Corp Fuel control deceleration mode
US3908363A (en) * 1970-04-11 1975-09-30 Mtu Muenchen Gmbh Aero gas turbine afterburner control
GB1415681A (en) * 1972-06-24 1975-11-26 Rolls Royce Flame-out control in gas turbine engine
US3867717A (en) * 1973-04-25 1975-02-18 Gen Electric Stall warning system for a gas turbine engine
US3852958A (en) * 1973-09-28 1974-12-10 Gen Electric Stall protector system for a gas turbine engine
US3854287A (en) * 1973-12-26 1974-12-17 United Aircraft Corp Self-trimming control for turbofan engines

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0616118A1 (fr) * 1993-03-16 1994-09-21 ROLLS-ROYCE plc Protection contre l'extintion et/ou pompage aprês ingestion d'eau pour turbine à gaz

Also Published As

Publication number Publication date
CA1083836A (fr) 1980-08-19
JPS5351323A (en) 1978-05-10
JPS6146655B2 (fr) 1986-10-15
GB1580503A (en) 1980-12-03
US4128995A (en) 1978-12-12
FR2367917B1 (fr) 1984-06-08
DE2732039A1 (de) 1978-04-20
DE2732039C2 (fr) 1987-07-23

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Legal Events

Date Code Title Description
ST Notification of lapse