GB9102205D0 - Thrust reverser - Google Patents

Thrust reverser

Info

Publication number
GB9102205D0
GB9102205D0 GB919102205A GB9102205A GB9102205D0 GB 9102205 D0 GB9102205 D0 GB 9102205D0 GB 919102205 A GB919102205 A GB 919102205A GB 9102205 A GB9102205 A GB 9102205A GB 9102205 D0 GB9102205 D0 GB 9102205D0
Authority
GB
United Kingdom
Prior art keywords
thrust reverser
reverser
thrust
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Withdrawn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
GB919102205A
Other versions
GB2252279A (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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB9102205A priority Critical patent/GB2252279A/en
Publication of GB9102205D0 publication Critical patent/GB9102205D0/en
Priority to DE19924200645 priority patent/DE4200645A1/en
Priority to FR9200955A priority patent/FR2672339A1/en
Publication of GB2252279A publication Critical patent/GB2252279A/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Withdrawn legal-status Critical Current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
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow

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)
GB9102205A 1991-02-01 1991-02-01 Thrust reverser Withdrawn GB2252279A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB9102205A GB2252279A (en) 1991-02-01 1991-02-01 Thrust reverser
DE19924200645 DE4200645A1 (en) 1991-02-01 1992-01-13 DRAWER REVERSE
FR9200955A FR2672339A1 (en) 1991-02-01 1992-01-29 PUSH INVERTER.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9102205A GB2252279A (en) 1991-02-01 1991-02-01 Thrust reverser

Publications (2)

Publication Number Publication Date
GB9102205D0 true GB9102205D0 (en) 1991-07-10
GB2252279A GB2252279A (en) 1992-08-05

Family

ID=10689378

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9102205A Withdrawn GB2252279A (en) 1991-02-01 1991-02-01 Thrust reverser

Country Status (3)

Country Link
DE (1) DE4200645A1 (en)
FR (1) FR2672339A1 (en)
GB (1) GB2252279A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5181676A (en) * 1992-01-06 1993-01-26 Lair Jean Pierre Thrust reverser integrating a variable exhaust area nozzle
FR2727468B1 (en) * 1994-11-30 1996-12-27 Hispano Suiza Sa DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER
FR2736390B1 (en) * 1995-07-05 1997-08-08 Hispano Suiza Sa PUSH INVERTER OF A SHELL TURBOREACTOR
FR2768773B1 (en) * 1997-09-25 1999-11-05 Hispano Suiza Sa INTERNAL SHELL TURBOREACTOR DRIVE INVERTER
FR2774431B1 (en) 1998-02-04 2000-03-03 Hispano Suiza Sa DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER
FR3057617B1 (en) * 2016-10-17 2020-10-16 Airbus NACELLE OF A TURBOREACTOR CONTAINING A INVERTER FLAP
RU2663249C1 (en) 2017-03-16 2018-08-03 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Method for manufacturing sections of a thrust reverser bearing grid
US10641208B2 (en) * 2017-11-27 2020-05-05 Rohr, Inc. Translating nozzle for mixed flow turbofan engine
US10724474B2 (en) 2018-05-01 2020-07-28 Rohr, Inc. Hybrid articulating/translating trailing edge reverser
US11053887B2 (en) * 2018-07-02 2021-07-06 Rohr, Inc. Thrust reverser with displaceable trailing edge body
US11155343B2 (en) 2018-12-17 2021-10-26 The Boeing Company Brake systems for aircraft and related methods

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020712A (en) * 1959-06-22 1962-02-13 Boeing Co Reversible-thrust sound suppression jet nozzles with movable ejector rings
GB1062839A (en) * 1965-11-26 1967-03-22 Rolls Royce Improvements relating to thrust reversers
GB1150012A (en) * 1966-09-12 1969-04-30 Rolls Royce Fluid Flow Duct Including Thrust Reversing Means
US4340178A (en) * 1980-05-05 1982-07-20 Rohr Industries, Inc. Thrust reverser - cascade type
FR2486153B1 (en) * 1980-07-04 1985-10-04 Hurel Dubois Avions DRIVE INVERTER FOR A REACTION ENGINE, IN PARTICULAR FOR EQUIPPING AN AIRCRAFT
DE3844188C1 (en) * 1988-12-29 1990-05-17 Mtu Muenchen Gmbh

Also Published As

Publication number Publication date
FR2672339A1 (en) 1992-08-07
GB2252279A (en) 1992-08-05
DE4200645A1 (en) 1992-08-06

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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)