DE69006868T2 - Gasturbinenluftstrahltriebwerk. - Google Patents

Gasturbinenluftstrahltriebwerk.

Info

Publication number
DE69006868T2
DE69006868T2 DE69006868T DE69006868T DE69006868T2 DE 69006868 T2 DE69006868 T2 DE 69006868T2 DE 69006868 T DE69006868 T DE 69006868T DE 69006868 T DE69006868 T DE 69006868T DE 69006868 T2 DE69006868 T2 DE 69006868T2
Authority
DE
Germany
Prior art keywords
gas turbine
air jet
jet engine
turbine air
engine
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 - Fee Related
Application number
DE69006868T
Other languages
English (en)
Other versions
DE69006868D1 (de
Inventor
Gregory S Patterson
James B Kelly
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69006868D1 publication Critical patent/DE69006868D1/de
Application granted granted Critical
Publication of DE69006868T2 publication Critical patent/DE69006868T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/18—Control or regulation automatic
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Control Of Turbines (AREA)
DE69006868T 1989-02-27 1990-01-18 Gasturbinenluftstrahltriebwerk. Expired - Fee Related DE69006868T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/316,265 US4959955A (en) 1989-02-27 1989-02-27 Method of operating gas turbine engine with fan damage

Publications (2)

Publication Number Publication Date
DE69006868D1 DE69006868D1 (de) 1994-04-07
DE69006868T2 true DE69006868T2 (de) 1994-06-09

Family

ID=23228306

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69006868T Expired - Fee Related DE69006868T2 (de) 1989-02-27 1990-01-18 Gasturbinenluftstrahltriebwerk.

Country Status (5)

Country Link
US (1) US4959955A (de)
EP (1) EP0385912B1 (de)
KR (1) KR960010279B1 (de)
AU (1) AU626974B2 (de)
DE (1) DE69006868T2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048285A (en) * 1990-03-26 1991-09-17 Untied Technologies Corporation Control system for gas turbine engines providing extended engine life
US5211007A (en) * 1991-04-10 1993-05-18 General Electric Company Method of pressure-ratio control of gas turbine engine
US5305599A (en) * 1991-04-10 1994-04-26 General Electric Company Pressure-ratio control of gas turbine engine
GB9421047D0 (en) * 1994-10-11 1994-12-07 Ricardo Aerospace Ltd Turbines
US5622045A (en) * 1995-06-07 1997-04-22 Allison Engine Company, Inc. System for detecting and accommodating gas turbine engine fan damage
GB9624070D0 (en) * 1996-11-20 1997-01-08 Rolls Royce Plc Control system for a ducted fan gas turbine engine
GB0116193D0 (en) 2001-07-03 2001-08-22 Rolls Royce Plc An apparatus and method for detecting a damaged rotary machine aerofoil
US7465145B2 (en) * 2005-03-17 2008-12-16 United Technologies Corporation Tip clearance control system
WO2008097269A2 (en) * 2006-08-01 2008-08-14 Hal Gerard Wick Aircraft engine management for fuel conservation
US20190360353A1 (en) * 2018-05-22 2019-11-28 Gulfstream Aerospace Corporation Propulsion system for an aircraft, a nozzle for use with the propulsion system, and a method of manufacturing a propulsion system for an aircraft
US10982623B2 (en) 2018-09-14 2021-04-20 Gulfstream Aerospace Corporation Propulsion system for an aircraft, a nozzle for use with the propulsion system, and a method of manufacturing a propulsion system for an aircraft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4130872A (en) * 1975-10-10 1978-12-19 The United States Of America As Represented By The Secretary Of The Air Force Method and system of controlling a jet engine for avoiding engine surge
US4159625A (en) * 1977-02-01 1979-07-03 United Technologies Corporation Control for gas turbine engine
US4139887A (en) * 1977-04-28 1979-02-13 United Technologies Corporation Dynamic compensation for multi-loop controls
US4294069A (en) * 1978-04-26 1981-10-13 United Technologies Corporation Exhaust nozzle control and core engine fuel control for turbofan engine
DE2930956C2 (de) * 1979-07-31 1985-07-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Regelungsverfahren für eine flächenverstellbare Schubdüse eines Mantelstrom-Gasturbinenstrahltriebwerks mit Nachbrenner
US4414807A (en) * 1980-12-08 1983-11-15 United Technologies Corporation Method and apparatus for controlling a gas turbine engine
US4581889A (en) * 1984-10-01 1986-04-15 General Electric Company Gas turbine engine control

Also Published As

Publication number Publication date
DE69006868D1 (de) 1994-04-07
AU4856190A (en) 1990-08-30
US4959955A (en) 1990-10-02
KR900013182A (ko) 1990-09-03
EP0385912A3 (de) 1991-05-02
EP0385912B1 (de) 1994-03-02
KR960010279B1 (ko) 1996-07-27
AU626974B2 (en) 1992-08-13
EP0385912A2 (de) 1990-09-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee