FR2146109A1 - - Google Patents

Info

Publication number
FR2146109A1
FR2146109A1 FR7126273A FR7126273A FR2146109A1 FR 2146109 A1 FR2146109 A1 FR 2146109A1 FR 7126273 A FR7126273 A FR 7126273A FR 7126273 A FR7126273 A FR 7126273A FR 2146109 A1 FR2146109 A1 FR 2146109A1
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.)
Withdrawn
Application number
FR7126273A
Other languages
French (fr)
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7126273A priority Critical patent/FR2146109A1/fr
Publication of FR2146109A1 publication Critical patent/FR2146109A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR7126273A 1971-07-19 1971-07-19 Withdrawn FR2146109A1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7126273A FR2146109A1 (de) 1971-07-19 1971-07-19

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7126273A FR2146109A1 (de) 1971-07-19 1971-07-19

Publications (1)

Publication Number Publication Date
FR2146109A1 true FR2146109A1 (de) 1973-03-02

Family

ID=9080529

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7126273A Withdrawn FR2146109A1 (de) 1971-07-19 1971-07-19

Country Status (1)

Country Link
FR (1) FR2146109A1 (de)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499158A1 (fr) * 1981-02-05 1982-08-06 Snecma Dispositif de reduction de poussee residuelle pour turboreacteur
FR2506843A1 (fr) * 1981-05-29 1982-12-03 Hurel Dubois Avions Dispositif d'inversion de poussee pour turboreacteur d'avion
EP0654598A1 (de) * 1993-11-24 1995-05-24 Hispano-Suiza Schubumkehrvorrichtung für ein Bläsertriebwerk
EP0771945A1 (de) * 1995-11-02 1997-05-07 Hispano Suiza Schubumkehrvorrichtung mit Sekundärklappen für ein Bläsertriebwerk
WO2008045070A1 (en) 2006-10-12 2008-04-17 United Technologies Corporation Variable area fan nozzle thrust reverser
FR2935354A1 (fr) * 2008-09-02 2010-03-05 Airbus France Nacelle pour moteur a double flux
US8127529B2 (en) 2007-03-29 2012-03-06 United Technologies Corporation Variable area fan nozzle and thrust reverser
EP2433864A1 (de) 2010-09-23 2012-03-28 Airbus Operations Vorrichtung zum Ableiten von Luft für ein Zweistromturbotriebwerk eines Flugzeugs
EP2548804A1 (de) 2011-07-22 2013-01-23 Airbus Operations S.A.S. Gondel für eine Antriebseinheit mit einer Düse mit variablem Querschnitt
EP2863038A1 (de) * 2013-10-17 2015-04-22 Rohr, Inc. Fanrampe mit Einbuchtung für eine Blockierklappe einer Schubumkehrvorrichtung
EP3670351A1 (de) * 2018-12-17 2020-06-24 The Boeing Company Bremsensysteme für flugzeug und zugehörige verfahren

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499158A1 (fr) * 1981-02-05 1982-08-06 Snecma Dispositif de reduction de poussee residuelle pour turboreacteur
FR2506843A1 (fr) * 1981-05-29 1982-12-03 Hurel Dubois Avions Dispositif d'inversion de poussee pour turboreacteur d'avion
EP0067747A1 (de) * 1981-05-29 1982-12-22 Societe De Construction Des Avions Hurel-Dubois Schuhumkehrvorrichtung für einen Strahlmotor
EP0654598A1 (de) * 1993-11-24 1995-05-24 Hispano-Suiza Schubumkehrvorrichtung für ein Bläsertriebwerk
FR2712929A1 (fr) * 1993-11-24 1995-06-02 Hispano Suiza Sa Inverseur de poussée de turboréacteur à double flux.
US5548954A (en) * 1993-11-24 1996-08-27 Societe Hispano Suiza Turbojet engine thrust reverser with rear support structure
EP0771945A1 (de) * 1995-11-02 1997-05-07 Hispano Suiza Schubumkehrvorrichtung mit Sekundärklappen für ein Bläsertriebwerk
FR2740834A1 (fr) * 1995-11-02 1997-05-09 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux muni de portes secondaires
US5819528A (en) * 1995-11-02 1998-10-13 Societe Hispano Suiza Turbojet engine thrust reverser having dual pivoting doors
US8844261B2 (en) 2006-10-12 2014-09-30 United Technologies Corporation Variable area fan nozzle thrust reverser
US8151551B2 (en) 2006-10-12 2012-04-10 United Technologies Corporation Variable area fan nozzle thrust reverser
WO2008045070A1 (en) 2006-10-12 2008-04-17 United Technologies Corporation Variable area fan nozzle thrust reverser
US8869505B2 (en) 2007-03-29 2014-10-28 United Technologies Corporation Variable area fan nozzle and thrust reverser
US8418436B2 (en) 2007-03-29 2013-04-16 United Technologies Corporation Variable area fan nozzle and thrust reverser
US8127529B2 (en) 2007-03-29 2012-03-06 United Technologies Corporation Variable area fan nozzle and thrust reverser
US8162257B2 (en) 2008-02-09 2012-04-24 Airbus Operations Sas Nacelle for double flow engine
FR2935354A1 (fr) * 2008-09-02 2010-03-05 Airbus France Nacelle pour moteur a double flux
EP2433864A1 (de) 2010-09-23 2012-03-28 Airbus Operations Vorrichtung zum Ableiten von Luft für ein Zweistromturbotriebwerk eines Flugzeugs
US8925295B2 (en) 2010-09-23 2015-01-06 Airbus Operations Air discharging device for an aircraft double-flow turbine engine
EP2548804A1 (de) 2011-07-22 2013-01-23 Airbus Operations S.A.S. Gondel für eine Antriebseinheit mit einer Düse mit variablem Querschnitt
FR2978126A1 (fr) * 2011-07-22 2013-01-25 Airbus Operations Sas Nacelle pour ensemble propulsif a tuyere a section variable
EP2863038A1 (de) * 2013-10-17 2015-04-22 Rohr, Inc. Fanrampe mit Einbuchtung für eine Blockierklappe einer Schubumkehrvorrichtung
EP3670351A1 (de) * 2018-12-17 2020-06-24 The Boeing Company Bremsensysteme für flugzeug und zugehörige verfahren
US11155343B2 (en) 2018-12-17 2021-10-26 The Boeing Company Brake systems for aircraft and related methods

Similar Documents

Publication Publication Date Title
AU477054B2 (de)
ATA136472A (de)
FR2146109A1 (de)
FR2167080A5 (de)
AU2658571A (de)
AU2485671A (de)
AU2894671A (de)
AU2684071A (de)
AU2941471A (de)
AU2952271A (de)
AU3005371A (de)
AU2564071A (de)
AU2486471A (de)
AU2503871A (de)
AU2836771A (de)
AU2907471A (de)
AU2473671A (de)
AU2456871A (de)
AU2455871A (de)
AU2415871A (de)
AU2837671A (de)
AU2399971A (de)
AU1109576A (de)
AU2854371A (de)
AU2875571A (de)

Legal Events

Date Code Title Description
ST Notification of lapse