GB1345337A - Gas turbine engine having a thrust reverser - Google Patents

Gas turbine engine having a thrust reverser

Info

Publication number
GB1345337A
GB1345337A GB1345337DA GB1345337A GB 1345337 A GB1345337 A GB 1345337A GB 1345337D A GB1345337D A GB 1345337DA GB 1345337 A GB1345337 A GB 1345337A
Authority
GB
United Kingdom
Prior art keywords
chain
door
cam track
doors
gas turbine
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
Other languages
English (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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of GB1345337A publication Critical patent/GB1345337A/en
Expired 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
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • 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
    • F02K1/76—Control or regulation of thrust reversers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmissions By Endless Flexible Members (AREA)
  • Transmission Devices (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
GB1345337D 1970-10-20 1971-10-28 Gas turbine engine having a thrust reverser Expired GB1345337A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4966270 1970-10-20

Publications (1)

Publication Number Publication Date
GB1345337A true GB1345337A (en) 1974-01-30

Family

ID=10453118

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1345337D Expired GB1345337A (en) 1970-10-20 1971-10-28 Gas turbine engine having a thrust reverser

Country Status (2)

Country Link
FR (1) FR2111726B1 (fr)
GB (1) GB1345337A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013231432A (ja) * 2012-04-30 2013-11-14 Mra Systems Inc 逆推力装置アセンブリおよび動作の方法
EP3034848A1 (fr) * 2014-12-15 2016-06-22 United Technologies Corporation Moteur à turbine à gaz et son ensemble d'inverseur de poussée
GB2564891A (en) * 2017-07-26 2019-01-30 Short Brothers Plc Nacelle with thrust reverser
EP3702603A1 (fr) * 2019-02-28 2020-09-02 Airbus Operations GmbH Ensemble d'inverseur de poussée pour une nacelle de moteur d'avion
US10995701B2 (en) * 2019-09-05 2021-05-04 Rohr, Inc. Translating sleeve thrust reverser assembly

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2697292B1 (fr) * 1992-10-27 1994-12-30 Hurel Dubois Avions Ensemble d'inversion de poussée pour moteur d'avion à réaction ménageant un espace de fuite axial en position d'inversion et moteur équipé d'un tel ensemble.
FR2752017B1 (fr) * 1996-08-01 1998-10-16 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes formant ecopes

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013231432A (ja) * 2012-04-30 2013-11-14 Mra Systems Inc 逆推力装置アセンブリおよび動作の方法
EP3034848A1 (fr) * 2014-12-15 2016-06-22 United Technologies Corporation Moteur à turbine à gaz et son ensemble d'inverseur de poussée
US10648427B2 (en) 2014-12-15 2020-05-12 United Technologies Corporation Gas turbine engine and thrust reverser assembly therefore
GB2564891A (en) * 2017-07-26 2019-01-30 Short Brothers Plc Nacelle with thrust reverser
WO2019020995A1 (fr) * 2017-07-26 2019-01-31 Short Brothers Plc Nacelle comprenant un inverseur de poussée
US11230994B2 (en) 2017-07-26 2022-01-25 Short Brothers Plc Nacelle with thrust reverser
EP3702603A1 (fr) * 2019-02-28 2020-09-02 Airbus Operations GmbH Ensemble d'inverseur de poussée pour une nacelle de moteur d'avion
US11319898B2 (en) 2019-02-28 2022-05-03 Airbus Operations Gmbh Thrust reverser assembly for an engine nacelle of an aircraft
US10995701B2 (en) * 2019-09-05 2021-05-04 Rohr, Inc. Translating sleeve thrust reverser assembly

Also Published As

Publication number Publication date
DE2152031A1 (de) 1972-04-27
FR2111726A1 (fr) 1972-06-09
DE2152031B2 (de) 1976-04-08
FR2111726B1 (fr) 1976-02-13

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Legal Events

Date Code Title Description
PS Patent sealed
PLE Entries relating assignments, transmissions, licences in the register of patents
PCNP Patent ceased through non-payment of renewal fee