FR2111726B1 - - Google Patents

Info

Publication number
FR2111726B1
FR2111726B1 FR7137686A FR7137686A FR2111726B1 FR 2111726 B1 FR2111726 B1 FR 2111726B1 FR 7137686 A FR7137686 A FR 7137686A FR 7137686 A FR7137686 A FR 7137686A FR 2111726 B1 FR2111726 B1 FR 2111726B1
Authority
FR
France
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
FR7137686A
Other languages
French (fr)
Other versions
FR2111726A1 (https=
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.)
SECRETAIRE ETAT R UNI GB
Original Assignee
SECRETAIRE ETAT R UNI GB
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 SECRETAIRE ETAT R UNI GB filed Critical SECRETAIRE ETAT R UNI GB
Publication of FR2111726A1 publication Critical patent/FR2111726A1/fr
Application granted granted Critical
Publication of FR2111726B1 publication Critical patent/FR2111726B1/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • F02K1/70Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/76Control 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)
  • Power-Operated Mechanisms For Wings (AREA)
  • Transmissions By Endless Flexible Members (AREA)
  • Transmission Devices (AREA)
FR7137686A 1970-10-20 1971-10-20 Expired FR2111726B1 (https=)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2111726A1 FR2111726A1 (https=) 1972-06-09
FR2111726B1 true FR2111726B1 (https=) 1976-02-13

Family

ID=10453118

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7137686A Expired FR2111726B1 (https=) 1970-10-20 1971-10-20

Country Status (2)

Country Link
FR (1) FR2111726B1 (https=)
GB (1) GB1345337A (https=)

Families Citing this family (7)

* 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
US8904751B2 (en) * 2012-04-30 2014-12-09 Middle River Aircraft Systems Thrust reverser assembly and method of operation
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
EP3702603B1 (en) 2019-02-28 2023-12-13 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
FR2111726A1 (https=) 1972-06-09
DE2152031B2 (de) 1976-04-08
DE2152031A1 (de) 1972-04-27
GB1345337A (en) 1974-01-30

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse