GB2252279A - Thrust reverser - Google Patents

Thrust reverser Download PDF

Info

Publication number
GB2252279A
GB2252279A GB9102205A GB9102205A GB2252279A GB 2252279 A GB2252279 A GB 2252279A GB 9102205 A GB9102205 A GB 9102205A GB 9102205 A GB9102205 A GB 9102205A GB 2252279 A GB2252279 A GB 2252279A
Authority
GB
United Kingdom
Prior art keywords
doors
sealing member
thrust reverser
movement
deflector
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Withdrawn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
GB9102205A
Other languages
English (en)
Other versions
GB9102205D0 (en
Inventor
Leonard John Rodgers
Norman Roberts
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/de
Priority to FR9200955A priority patent/FR2672339A1/fr
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Withdrawn legal-status Critical Current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 (de) 1991-02-01 1992-01-13 Schubumkehrvorrichtung
FR9200955A FR2672339A1 (fr) 1991-02-01 1992-01-29 Inverseur de poussee.

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 GB9102205D0 (en) 1991-07-10
GB2252279A true 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 (fr)
FR (1) FR2672339A1 (fr)
GB (1) GB2252279A (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0620792A1 (fr) * 1992-01-06 1994-10-26 AERONAUTICAL CONCEPT OF EXHAUST Ltd Inverseur de poussee avec tuyere integree a surface d'echappement variable
FR2774431A1 (fr) 1998-02-04 1999-08-06 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval
FR3057617A1 (fr) * 2016-10-17 2018-04-20 Airbus Nacelle d'un turboreacteur comportant un volet inverseur
US20200003156A1 (en) * 2018-07-02 2020-01-02 Rohr, Inc. Thrust reverser with displaceable trailing edge body
US10641208B2 (en) * 2017-11-27 2020-05-05 Rohr, Inc. Translating nozzle for mixed flow turbofan engine
EP3670351A1 (fr) * 2018-12-17 2020-06-24 The Boeing Company Systèmes de frein pour aéronef et procédés associés
US10724474B2 (en) 2018-05-01 2020-07-28 Rohr, Inc. Hybrid articulating/translating trailing edge reverser

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2727468B1 (fr) * 1994-11-30 1996-12-27 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval
FR2736390B1 (fr) * 1995-07-05 1997-08-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a une coquille
FR2768773B1 (fr) * 1997-09-25 1999-11-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a coquilles internes
RU2663249C1 (ru) 2017-03-16 2018-08-03 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ изготовления секций несущей решетки реверсера тяги

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 (fr) * 1980-07-04 1985-10-04 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef
DE3844188C1 (fr) * 1988-12-29 1990-05-17 Mtu Muenchen Gmbh

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0620792A1 (fr) * 1992-01-06 1994-10-26 AERONAUTICAL CONCEPT OF EXHAUST Ltd Inverseur de poussee avec tuyere integree a surface d'echappement variable
EP0620792A4 (fr) * 1992-01-06 1995-07-19 Lair Jean Pierre Inverseur de poussee avec tuyere integree a surface d'echappement variable.
FR2774431A1 (fr) 1998-02-04 1999-08-06 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval
FR3057617A1 (fr) * 2016-10-17 2018-04-20 Airbus Nacelle d'un turboreacteur comportant un volet inverseur
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
US20200003156A1 (en) * 2018-07-02 2020-01-02 Rohr, Inc. Thrust reverser with displaceable trailing edge body
EP3591204A1 (fr) * 2018-07-02 2020-01-08 Rohr, Inc. Inverseur de poussée avec corps mobile de bord de fuite
US11053887B2 (en) 2018-07-02 2021-07-06 Rohr, Inc. Thrust reverser with displaceable trailing edge body
EP3670351A1 (fr) * 2018-12-17 2020-06-24 The Boeing Company Systèmes de frein pour aéronef et procédés associés
US11155343B2 (en) 2018-12-17 2021-10-26 The Boeing Company Brake systems for aircraft and related methods

Also Published As

Publication number Publication date
GB9102205D0 (en) 1991-07-10
DE4200645A1 (de) 1992-08-06
FR2672339A1 (fr) 1992-08-07

Similar Documents

Publication Publication Date Title
US5313788A (en) Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine
EP0315524B1 (fr) Inverseur de poussée de turboréacteur à grilles, à section variable d'éjection
CA2318373C (fr) Inverseur de poussee de turboreacteur a grilles superposables
CA1183693A (fr) Buse bidimensionnelle convergente/divergente a orifice de diametre variable
US9127623B2 (en) Thrust reverser device
CA2204823C (fr) Inverseur de poussee de turboreacteur a double flux, a obstacles lies au capot primaire
US4278220A (en) Thrust reverser for a long duct fan engine
GB2252279A (en) Thrust reverser
US4916895A (en) Thrust reverse for a turbofan engine
US4462207A (en) Thrust spoiler for aero engines
EP0790400B1 (fr) Inverseur de poussée de turboréacteur à portes associées à un panneau amont
FR2638207A1 (fr) Inverseur de poussee de turboreacteur, a portes pivotantes equilibrees
FR2804474A1 (fr) Inverseur de poussee a grilles aubagees de deviation a structure arriere fixe
US5765362A (en) Pivoting door thrust reverser with cowling mounted auxiliary panel
EP0120856A1 (fr) Assemblage de porte de blocage d'inverseur de poussee.
US11835015B2 (en) Thrust reverser with blocker door folding linkage
US5615549A (en) Thrust reverser for a fan-type turbojet engine
DE4024016A1 (de) Abgasduese
FR2561313A1 (fr) Dispositif de modulation de poussee
US5097662A (en) Apparatus for influencing the flow of air through a passageway
GB1574335A (en) Thrust reverser for a fluid flow propulsion engine
US5390879A (en) Jet pipe for supporting a thrust reverser for aircraft jet engines
FR2788564A1 (fr) Tuyere d'ejection de turboreacteur a reverse integree
US4682733A (en) Thrust reverser
EP1045130A1 (fr) Tuyère d'éjection axisymétrique, convergente divergente, à orientation par un anneau guide

Legal Events

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