GB8506257D0 - Thrust modulation device - Google Patents

Thrust modulation device

Info

Publication number
GB8506257D0
GB8506257D0 GB858506257A GB8506257A GB8506257D0 GB 8506257 D0 GB8506257 D0 GB 8506257D0 GB 858506257 A GB858506257 A GB 858506257A GB 8506257 A GB8506257 A GB 8506257A GB 8506257 D0 GB8506257 D0 GB 8506257D0
Authority
GB
United Kingdom
Prior art keywords
modulation device
thrust modulation
thrust
modulation
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.)
Withdrawn
Application number
GB858506257A
Other versions
GB2156004A (en
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 GB8506257D0 publication Critical patent/GB8506257D0/en
Publication of GB2156004A publication Critical patent/GB2156004A/en
Withdrawn legal-status Critical Current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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Analysing Materials By The Use Of Radiation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
GB08506257A 1984-03-15 1985-03-11 Thrust modulation device for a gas turbine engine Withdrawn GB2156004A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US58983584A 1984-03-15 1984-03-15

Publications (2)

Publication Number Publication Date
GB8506257D0 true GB8506257D0 (en) 1985-04-11
GB2156004A GB2156004A (en) 1985-10-02

Family

ID=24359755

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08506257A Withdrawn GB2156004A (en) 1984-03-15 1985-03-11 Thrust modulation device for a gas turbine engine

Country Status (5)

Country Link
JP (1) JPS60237149A (en)
DE (1) DE3508723A1 (en)
FR (1) FR2561313A1 (en)
GB (1) GB2156004A (en)
IT (1) IT1185058B (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2734323A1 (en) * 1985-04-17 1996-11-22 Snecma Two-dimensional jet engine outlet control system
GB2182724B (en) * 1985-10-08 1988-12-07 Rolls Royce Gas turbine engine thrust reverser
GB2189550A (en) * 1986-04-25 1987-10-28 Rolls Royce A gas turbine engine powerplant with flow control devices
FR2618853B1 (en) * 1987-07-29 1989-11-10 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER WITH MOBILE DOOR DEFLECTOR
FR2618852B1 (en) * 1987-07-29 1989-11-10 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER PROVIDED WITH A FLOW RECTIFIER DEVICE
US4807434A (en) * 1987-12-21 1989-02-28 The Boeing Company Thrust reverser for high bypass jet engines
US5094070A (en) * 1989-04-14 1992-03-10 Mtu Motoren- Und Turbinen Union Munchin Gmbh Propelling nozzle for a hypersonic jet plane
ES2075782B1 (en) * 1992-02-20 1998-03-16 Sener Ing & Sist ADJUSTABLE VARIABLE GEOMETRY NOZZLE FOR GAS TURBINES.
US5575147A (en) * 1994-12-22 1996-11-19 United Technologies Corporation Compact thrust reverser
GB0616740D0 (en) 2006-08-24 2006-10-04 Short Brothers Plc Aircraft engine thrust reverser
FR2978802B1 (en) * 2011-08-05 2017-07-14 Aircelle Sa INVERTER WITH MOBILE GRIDS AND VARIABLE TUBE BY TRANSLATION
FR3006715B1 (en) * 2013-06-07 2015-06-05 Aircelle Sa THRUST INVERTER OF A TURBOJET NACELLE COMPRISING GRIDS FIXED TO MOBILE HOODS
US10208708B2 (en) * 2015-01-29 2019-02-19 Rohr, Inc. Translating cascade hidden blocker door thrust reverser
US20180045140A1 (en) * 2016-08-09 2018-02-15 Rolls-Royce Plc Aircraft gas turbine engine nacelle
FR3082889A1 (en) * 2018-06-26 2019-12-27 Airbus Operations TURBOREACTOR COMPRISING A NACELLE EQUIPPED WITH REVERSING SHUTTERS PROVIDED WITH MEANS FOR GENERATING VORTS
US11840987B2 (en) 2022-04-05 2023-12-12 General Electric Company Cascade thrust reverser assembly for a gas turbine engine
FR3136517A1 (en) * 2022-06-14 2023-12-15 Airbus Operations Aircraft engine nacelle provided with a thrust reverser with a movable ejection structure.
US12000359B2 (en) 2022-08-18 2024-06-04 General Electric Company Cascade thrust reverser actuation assembly for a turbofan engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE557040A (en) * 1956-04-27
GB1142660A (en) * 1963-08-07 1969-02-12 Gen Electric Improvements in combination jet exhaust nozzle and thrust reverser
DE1964976C3 (en) * 1969-12-24 1973-01-04 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Thrust reverser for a turbine jet engine of an aircraft
GB1386232A (en) * 1971-03-31 1975-03-05 Short Brothers & Harland Ltd Fluid propulsion systems

Also Published As

Publication number Publication date
FR2561313A1 (en) 1985-09-20
IT1185058B (en) 1987-11-04
GB2156004A (en) 1985-10-02
DE3508723A1 (en) 1985-09-26
IT8519865A0 (en) 1985-03-12
JPS60237149A (en) 1985-11-26

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)