IT1080663B - Dispositivo di controllo di spinta per un turbomotore a gas - Google Patents

Dispositivo di controllo di spinta per un turbomotore a gas

Info

Publication number
IT1080663B
IT1080663B IT25239/77A IT2523977A IT1080663B IT 1080663 B IT1080663 B IT 1080663B IT 25239/77 A IT25239/77 A IT 25239/77A IT 2523977 A IT2523977 A IT 2523977A IT 1080663 B IT1080663 B IT 1080663B
Authority
IT
Italy
Prior art keywords
control device
thrust control
turbo engine
gas turbo
engine
Prior art date
Application number
IT25239/77A
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
Application granted granted Critical
Publication of IT1080663B publication Critical patent/IT1080663B/it

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)
IT25239/77A 1976-07-06 1977-06-30 Dispositivo di controllo di spinta per un turbomotore a gas IT1080663B (it)

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
IT1080663B true IT1080663B (it) 1985-05-16

Family

ID=24821566

Family Applications (1)

Application Number Title Priority Date Filing Date
IT25239/77A IT1080663B (it) 1976-07-06 1977-06-30 Dispositivo di controllo di spinta per un turbomotore a gas

Country Status (7)

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

Families Citing this family (17)

* 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 (en) * 2006-03-24 2013-08-28 Rolls-Royce plc Method for monitoring thrust in gas turbine engines
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

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 (it) * 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 (en) * 1973-09-24 1978-02-21 Smiths Industries Limited Dual, simultaneously operating control system with fault detection
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
FR2357739B1 (it) 1983-08-12
FR2357739A1 (fr) 1978-02-03
DE2730083C2 (de) 1987-05-07
JPS5314215A (en) 1978-02-08
US4136517A (en) 1979-01-30
BE856540A (fr) 1977-10-31
GB1581889A (en) 1980-12-31
DE2730083A1 (de) 1978-01-12
JPS6110652B2 (it) 1986-03-31

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