DE2730083C2 - Schubregeleinrichtung für ein Gasturbinentriebwerk - Google Patents

Schubregeleinrichtung für ein Gasturbinentriebwerk

Info

Publication number
DE2730083C2
DE2730083C2 DE2730083A DE2730083A DE2730083C2 DE 2730083 C2 DE2730083 C2 DE 2730083C2 DE 2730083 A DE2730083 A DE 2730083A DE 2730083 A DE2730083 A DE 2730083A DE 2730083 C2 DE2730083 C2 DE 2730083C2
Authority
DE
Germany
Prior art keywords
thrust
signal
fan speed
engine
δepr
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.)
Expired
Application number
DE2730083A
Other languages
German (de)
English (en)
Other versions
DE2730083A1 (de
Inventor
Harold Cincinnati Ohio Brown
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 DE2730083A1 publication Critical patent/DE2730083A1/de
Application granted granted Critical
Publication of DE2730083C2 publication Critical patent/DE2730083C2/de
Expired 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
    • F02C9/28—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)
DE2730083A 1976-07-06 1977-07-02 Schubregeleinrichtung für ein Gasturbinentriebwerk Expired DE2730083C2 (de)

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 (2)

Publication Number Publication Date
DE2730083A1 DE2730083A1 (de) 1978-01-12
DE2730083C2 true DE2730083C2 (de) 1987-05-07

Family

ID=24821566

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2730083A Expired DE2730083C2 (de) 1976-07-06 1977-07-02 Schubregeleinrichtung für ein Gasturbinentriebwerk

Country Status (7)

Country Link
US (1) US4136517A (US20090192370A1-20090730-C00001.png)
JP (1) JPS5314215A (US20090192370A1-20090730-C00001.png)
BE (1) BE856540A (US20090192370A1-20090730-C00001.png)
DE (1) DE2730083C2 (US20090192370A1-20090730-C00001.png)
FR (1) FR2357739A1 (US20090192370A1-20090730-C00001.png)
GB (1) GB1581889A (US20090192370A1-20090730-C00001.png)
IT (1) IT1080663B (US20090192370A1-20090730-C00001.png)

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 (US20090192370A1-20090730-C00001.png) * 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 (US20090192370A1-20090730-C00001.png) 1983-08-12
US4136517A (en) 1979-01-30
DE2730083A1 (de) 1978-01-12
JPS5314215A (en) 1978-02-08
IT1080663B (it) 1985-05-16
BE856540A (fr) 1977-10-31
FR2357739A1 (fr) 1978-02-03
JPS6110652B2 (US20090192370A1-20090730-C00001.png) 1986-03-31
GB1581889A (en) 1980-12-31

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee