FR2411308A1 - Commande et procede pour obtenir des augmentations rapides de la poussee dans une turbo-soufflante - Google Patents

Commande et procede pour obtenir des augmentations rapides de la poussee dans une turbo-soufflante

Info

Publication number
FR2411308A1
FR2411308A1 FR7834644A FR7834644A FR2411308A1 FR 2411308 A1 FR2411308 A1 FR 2411308A1 FR 7834644 A FR7834644 A FR 7834644A FR 7834644 A FR7834644 A FR 7834644A FR 2411308 A1 FR2411308 A1 FR 2411308A1
Authority
FR
France
Prior art keywords
control
turbo
blower
thrust increases
obtaining rapid
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
FR7834644A
Other languages
English (en)
Other versions
FR2411308B1 (fr
Inventor
Jack Edward Cornett
Ralph Conner Corley
Thomas Orison Fraley
Andrew Axel Saunders Jr
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 FR2411308A1 publication Critical patent/FR2411308A1/fr
Application granted granted Critical
Publication of FR2411308B1 publication Critical patent/FR2411308B1/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
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F02C9/54—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by throttling the working fluid, by adjusting vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

COMMANDE PERMETTANT DE MAINTENIR UNE VITESSE DONNEE DE LA SOUFFLANTE ET UN NIVEAU DONNE DE LA POUSSEE. ELLE COMPREND UN DISPOSITIF PRODUISANT UN SIGNAL DE RECALAGE FONCTION DE LA POSITION DE LA MANETTE DES GAZ, ET LA MODIFICATION DE CET ANGLE DE STATOR PAR APPLICATION DE CE SIGNAL DE RECALAGE A CETTE COMMANDE DE STATOR. APPLICATION AUX TURBINES A GAZ D'AVION.
FR7834644A 1977-12-09 1978-12-08 Commande et procede pour obtenir des augmentations rapides de la poussee dans une turbo-soufflante Granted FR2411308A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/858,936 US4184327A (en) 1977-12-09 1977-12-09 Method and apparatus for rapid thrust increases in a turbofan engine

Publications (2)

Publication Number Publication Date
FR2411308A1 true FR2411308A1 (fr) 1979-07-06
FR2411308B1 FR2411308B1 (fr) 1983-10-28

Family

ID=25329549

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7834644A Granted FR2411308A1 (fr) 1977-12-09 1978-12-08 Commande et procede pour obtenir des augmentations rapides de la poussee dans une turbo-soufflante

Country Status (6)

Country Link
US (1) US4184327A (fr)
JP (1) JPS5495819A (fr)
DE (1) DE2852911A1 (fr)
FR (1) FR2411308A1 (fr)
GB (1) GB2009858B (fr)
IT (1) IT1100530B (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4928482A (en) * 1988-09-20 1990-05-29 United Technologies Corporation Control of high compressor vanes and fuel for a gas turbine engine
US5133182A (en) * 1988-09-20 1992-07-28 United Technologies Corporation Control of low compressor vanes and fuel for a gas turbine engine
US4947643A (en) * 1988-09-20 1990-08-14 United Technologies Corporation Active geometry control system for gas turbine engines
US6735955B2 (en) * 2001-10-10 2004-05-18 Goodrich Pump & Engine Control Systems, Inc. Control system for positioning compressor inlet guide vanes
US6688097B2 (en) * 2001-12-19 2004-02-10 Honeywell International Inc. Multivariant set point using N1 and N2 for engine control
DE102007012119A1 (de) * 2007-03-13 2008-09-18 Rolls-Royce Deutschland Ltd & Co Kg Drosselgradabhängige Schaufelverstellung bei Strömungsarbeitsmaschinen
US8954228B2 (en) * 2008-12-30 2015-02-10 Rolls-Royce Corporation Gas turbine engine failure detection
US9021780B2 (en) * 2008-12-31 2015-05-05 Rolls-Royce Corporation Energy extraction and transfer system for a gas turbine engine
FR2950927B1 (fr) * 2009-10-06 2016-01-29 Snecma Systeme de commande de la position angulaire d'aubes de stator et procede d'optimisation de ladite position angulaire
US9512784B2 (en) * 2010-01-29 2016-12-06 Pratt & Whitney Canada Corp. Free gas turbine with constant temperature-corrected gas generator speed
GB201112577D0 (en) * 2011-07-22 2011-08-31 Rolls Royce Plc Method of inhibiting ice accretion within a turbine engine and control system therefor
US8742973B1 (en) * 2011-09-22 2014-06-03 Rockwell Collins, Inc. System and method of determining increased turbulence susceptibility with elapsed flight time

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657881A (en) * 1969-09-02 1972-04-25 Gen Motors Corp Gas turbine control with prewhirl of air entering the compressor
US3686859A (en) * 1970-09-25 1972-08-29 Chandler Evans Inc Turbine engine starting circuit
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system
US3952502A (en) * 1974-03-04 1976-04-27 General Motors Corporation Gas turbine control

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1102493B (de) * 1957-12-30 1961-03-16 Rolls Royce Zweikreisgasturbinenstrahltriebwerk

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3657881A (en) * 1969-09-02 1972-04-25 Gen Motors Corp Gas turbine control with prewhirl of air entering the compressor
US3686859A (en) * 1970-09-25 1972-08-29 Chandler Evans Inc Turbine engine starting circuit
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system
US3952502A (en) * 1974-03-04 1976-04-27 General Motors Corporation Gas turbine control

Also Published As

Publication number Publication date
JPS5495819A (en) 1979-07-28
FR2411308B1 (fr) 1983-10-28
IT7830454A0 (it) 1978-12-01
US4184327A (en) 1980-01-22
GB2009858A (en) 1979-06-20
GB2009858B (en) 1982-02-24
DE2852911C2 (fr) 1991-03-28
IT1100530B (it) 1985-09-28
DE2852911A1 (de) 1979-06-13
JPS6130142B2 (fr) 1986-07-11

Similar Documents

Publication Publication Date Title
FR2411308A1 (fr) Commande et procede pour obtenir des augmentations rapides de la poussee dans une turbo-soufflante
FR2415724A1 (fr) Appareil et procede pour la commande de la poussee d'un moteur a turbine a gaz
IE801648L (en) Controlling the operation of a pump
JPS5459525A (en) Control method and apparatus for fuel injection
JPS5430358A (en) Automatic velocity-ratio controlling apparatus of stepless change gear for a car
FR2462564A1 (fr) Installation de regulation de tuyeres de poussee reglables de turboreacteurs a double flux
SE8303152L (sv) Bladflojlingsanordning for vindturbiner
EP0006120A1 (fr) Cabine de peinture
EP0006873A1 (fr) Procédé de commande d'un moteur à combustion interne.
FR2368623A1 (fr) Dispositif de commande des volets de prelevement d'air d'une turbomachine
JPS57102527A (en) Fuel injection nozzle unit
FR2357739A1 (fr) Regulateur de poussee pour un moteur a turbine a gaz
IE45720L (en) Controlling the exhaust nozzle aperature of a gas turbine¹engine
FR2281795A1 (fr) Installation de distribution de produit d'epandage
FR2398185A1 (fr) Commande de secours pour systeme de commande de moteur a turbine a gaz
JPS5644433A (en) Method of adjusting idling revolution speed
JPS57124062A (en) Electronic control type carburetter
GB1356275A (en) Method for regulating fuel flow of a gas turbine engine
ES370344A1 (es) Un metodo de control automatico de la carga de motores nava-les.
US2612225A (en) Engine pressure and speed control device
ES413344A1 (es) Mejoras en los aparatos para alimentar motores con combus- tible.
JPS57328A (en) Turbosupercharge spark ignition engine
FR2407094A1 (fr) Dispositif de reglage de la vitesse d'un vehicule
FR2356001A1 (fr) Systeme de commande de circuit de carburant pour turboreacteur d'avion
SE9102631L (sv) Foerfarande vid justering av luft/braenslefoerhaallande under drift foer en foerbraenningsmotor och anordning daertill

Legal Events

Date Code Title Description
ST Notification of lapse