[go: up one dir, main page]

BE856540A - Regulateur de poussee pour un moteur a turbine a gaz - Google Patents

Regulateur de poussee pour un moteur a turbine a gaz

Info

Publication number
BE856540A
BE856540A BE179121A BE179121A BE856540A BE 856540 A BE856540 A BE 856540A BE 179121 A BE179121 A BE 179121A BE 179121 A BE179121 A BE 179121A BE 856540 A BE856540 A BE 856540A
Authority
BE
Belgium
Prior art keywords
gas turbine
turbine engine
thrust regulator
thrust
regulator
Prior art date
Application number
BE179121A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BE856540A publication Critical patent/BE856540A/fr

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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feedback Control In General (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
BE179121A 1976-07-06 1977-07-06 Regulateur de poussee pour un moteur a turbine a gaz BE856540A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/702,526 US4136517A (en) 1976-07-06 1976-07-06 Thrust control system for a gas turbine engine

Publications (1)

Publication Number Publication Date
BE856540A true BE856540A (fr) 1977-10-31

Family

ID=24821566

Family Applications (1)

Application Number Title Priority Date Filing Date
BE179121A BE856540A (fr) 1976-07-06 1977-07-06 Regulateur de poussee pour un moteur a turbine a gaz

Country Status (7)

Country Link
US (1) US4136517A (fr)
JP (1) JPS5314215A (fr)
BE (1) BE856540A (fr)
DE (1) DE2730083C2 (fr)
FR (1) FR2357739A1 (fr)
GB (1) GB1581889A (fr)
IT (1) IT1080663B (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4313167A (en) * 1979-07-27 1982-01-26 General Electric Company Thrust control system for a gas turbine engine
US4397148A (en) * 1980-07-02 1983-08-09 General Electric Company Control system for an augmented turbofan engine
US4722061A (en) * 1984-12-20 1988-01-26 United Technologies Corporation Establishing synthesis validity between two signal sources
US5285638A (en) * 1991-05-28 1994-02-15 Telectro-Mek, Inc. Method and apparatus for maximizing fuel efficiency for jet engines
US6704630B2 (en) * 2002-04-04 2004-03-09 Grazyna Balut Ostrom Thrust control malfunction accommodation system and method
DE10302074A1 (de) * 2003-01-21 2004-07-29 Rolls-Royce Deutschland Ltd & Co Kg Fehlerdetektionslogik für Triebwerke
EP1837506B1 (fr) * 2006-03-24 2013-08-28 Rolls-Royce plc Méthode de surveillance de la poussée dans un moteur à turbine à gaz
US8954228B2 (en) * 2008-12-30 2015-02-10 Rolls-Royce Corporation Gas turbine engine failure detection
US8381510B2 (en) * 2009-04-30 2013-02-26 General Electric Company Method and systems for controlling engine thrust using variable trim
US8290683B2 (en) * 2010-02-16 2012-10-16 Telectro-Mek, Inc. Apparatus and method for reducing aircraft fuel consumption
US8490404B1 (en) * 2012-02-28 2013-07-23 General Electric Company Sensor-based performance-seeking gas turbine engine control
FR2992354B1 (fr) * 2012-06-20 2015-09-18 Snecma Procede et dispositif d'ajustement d'une valeur de consigne d'un parametre influencant une poussee d'un moteur a turbine a gaz
GB201219815D0 (en) * 2012-11-05 2012-12-19 Rolls Royce Plc Engine control parameter trimming
FR3029570B1 (fr) * 2014-12-05 2019-08-30 Safran Aircraft Engines Dispositif et procede de regulation d'un moteur exploitant une mesure de poussee
US10487752B2 (en) 2015-03-11 2019-11-26 Pratt & Whitney Canada Corp. Overthrust protection system and method
GB201817939D0 (en) * 2018-11-02 2018-12-19 Rolls Royce Plc Method of calibrating a gas turbine engine
US11136134B2 (en) * 2018-12-21 2021-10-05 Pratt & Whitney Canada Corp. System and method for operating a gas turbine engine coupled to an aircraft propeller
US12140088B1 (en) * 2023-09-22 2024-11-12 Pratt & Whitney Canada Corp. Method for detecting and annunciating gas turbine engine compressor stall

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2948114A (en) * 1956-03-17 1960-08-09 Hispano Suiza Sa Engine fuel control including acceleration-biased control signal selector
JPS4936452B1 (fr) * 1970-09-14 1974-10-01
US3820321A (en) * 1972-04-17 1974-06-28 Lucas Industries Ltd Acceleration control for gas turbine engine
US3813063A (en) * 1972-07-21 1974-05-28 United Aircraft Corp Automatic aircraft engine pressure ratio control system
US3790765A (en) * 1973-02-01 1974-02-05 Chandler Evans Inc Governor with integrator reset
US3867717A (en) * 1973-04-25 1975-02-18 Gen Electric Stall warning system for a gas turbine engine
CA1026850A (fr) * 1973-09-24 1978-02-21 Smiths Industries Limited Double systeme de commande simultanee avec detecteur de panne
US3854287A (en) * 1973-12-26 1974-12-17 United Aircraft Corp Self-trimming control for turbofan engines
US3902315A (en) * 1974-06-12 1975-09-02 United Aircraft Corp Starting fuel control system for gas turbine engines

Also Published As

Publication number Publication date
FR2357739A1 (fr) 1978-02-03
FR2357739B1 (fr) 1983-08-12
DE2730083A1 (de) 1978-01-12
DE2730083C2 (de) 1987-05-07
IT1080663B (it) 1985-05-16
JPS5314215A (en) 1978-02-08
GB1581889A (en) 1980-12-31
US4136517A (en) 1979-01-30
JPS6110652B2 (fr) 1986-03-31

Similar Documents

Publication Publication Date Title
BE861363A (fr) Diffuseur perfectionne pour moteur a turbine a gaz
FR2290350A1 (fr) Nacelle pour moteur a turbine a gaz
FR2406726B1 (fr) Appareillage de combustion perfectionne pour moteur a turbine a gaz
BE860915A (fr) Systeme de refroidissement perfectionne pour moteur a turbine a gaz
FR2333953A1 (fr) Dispositif de reglage de jeu pour un moteur a turbine a gaz
FR2433639B1 (fr) Aube pour moteur a turbine a gaz
BE856540A (fr) Regulateur de poussee pour un moteur a turbine a gaz
FR2312654A1 (fr) Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz
GB2004592B (en) Combustion liner for gas turbine engine
FR2341746A1 (fr) Aube de guidage et melangeur combines pour un moteur a turbine a gaz
FR2333964A1 (fr) Tuyere de propulsion pour moteur a turbine a gaz
BE825926A (fr) Procede d'equilibrage d'un moteur a turbine a gaz
FR2333954A1 (fr) Mecanisme moteur de turbines a gaz
FR2557212B1 (fr) Structure de stator pour un moteur a turbine a gaz
FR2395402B1 (fr) Circuit perfectionne de lubrification pour moteurs a turbine a gaz
FR2460390B1 (fr) Diffuseur pour moteur a turbine a gaz
FR2315612A1 (fr) Moteur a turbine a gaz
FR2309727A1 (fr) Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz
FR2527268B1 (fr) Prediffuseur pour un moteur a turbine a gaz
BE883129A (fr) Commande de demarrage pour un moteur a turbine a gaz
GB1543032A (en) Combustion apparatus for a gas turbine engine
GB1554982A (en) Gas turbine engine lubrication system
FR2316447A1 (fr) Dispositif d'ejection pour un moteur a turbine a gaz
FR2468739B1 (fr) Moteur a turbine a gaz modulaire
BE805378A (fr) Dispositif d'allumage pour moteur a turbine a gaz