BR112015011506A2 - dispositivo reversor de empuxo para nacela de motor turbojato e nacela de motor turbojato. - Google Patents

dispositivo reversor de empuxo para nacela de motor turbojato e nacela de motor turbojato.

Info

Publication number
BR112015011506A2
BR112015011506A2 BR112015011506A BR112015011506A BR112015011506A2 BR 112015011506 A2 BR112015011506 A2 BR 112015011506A2 BR 112015011506 A BR112015011506 A BR 112015011506A BR 112015011506 A BR112015011506 A BR 112015011506A BR 112015011506 A2 BR112015011506 A2 BR 112015011506A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
engine nacelle
reversing device
thrust reversing
nacelle
Prior art date
Application number
BR112015011506A
Other languages
English (en)
Inventor
Peyron Vincent
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BR112015011506A2 publication Critical patent/BR112015011506A2/pt

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
    • 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
    • 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
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
    • 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
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
BR112015011506A 2012-12-11 2013-12-10 dispositivo reversor de empuxo para nacela de motor turbojato e nacela de motor turbojato. BR112015011506A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1261854A FR2999240B1 (fr) 2012-12-11 2012-12-11 Systeme de synchronisation pour dispositif d'inversion de poussee
PCT/FR2013/053013 WO2014091139A1 (fr) 2012-12-11 2013-12-10 Système de synchronisation pour dispositif d'inversion de poussée

Publications (1)

Publication Number Publication Date
BR112015011506A2 true BR112015011506A2 (pt) 2017-07-11

Family

ID=47741122

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015011506A BR112015011506A2 (pt) 2012-12-11 2013-12-10 dispositivo reversor de empuxo para nacela de motor turbojato e nacela de motor turbojato.

Country Status (8)

Country Link
US (1) US20150260125A1 (pt)
EP (1) EP2932078A1 (pt)
CN (1) CN104854336A (pt)
BR (1) BR112015011506A2 (pt)
CA (1) CA2893260A1 (pt)
FR (1) FR2999240B1 (pt)
RU (1) RU2015128055A (pt)
WO (1) WO2014091139A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013226770A1 (de) * 2013-12-19 2015-06-25 Liebherr-Aerospace Lindenberg Gmbh Fluggasturbine mit einer Triebwerksverkleidung mit Schubumkehrvorrichtung
CN109715928B (zh) * 2016-05-30 2021-06-25 加拿大空客有限合伙公司 飞行器发动机组件
FR3075760B1 (fr) * 2017-12-21 2020-01-31 Safran Nacelles Nacelle de moteur d’aeronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4391409A (en) * 1980-09-30 1983-07-05 The Boeing Company Positioning and control system for fan thrust reverser cowls in a turbofan engine
US6519929B2 (en) * 2001-04-30 2003-02-18 Honeywell International, Inc. System and method for controlling the deployment of jet engine thrust reversers
FR2846375B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes
FR2932226B1 (fr) * 2008-06-06 2013-08-23 Aircelle Sa Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2962978B1 (fr) * 2010-07-22 2012-08-03 Aircelle Sa Nacelle de turboreacteur
FR2974150B1 (fr) * 2011-04-14 2013-04-12 Aircelle Sa Inverseur de poussee pour turboreacteur d'aeronef

Also Published As

Publication number Publication date
FR2999240B1 (fr) 2015-01-02
CA2893260A1 (fr) 2014-06-19
CN104854336A (zh) 2015-08-19
FR2999240A1 (fr) 2014-06-13
US20150260125A1 (en) 2015-09-17
WO2014091139A1 (fr) 2014-06-19
EP2932078A1 (fr) 2015-10-21
RU2015128055A (ru) 2017-01-18

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]