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BR112015005181A2 - dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato. - Google Patents

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

Info

Publication number
BR112015005181A2
BR112015005181A2 BR112015005181A BR112015005181A BR112015005181A2 BR 112015005181 A2 BR112015005181 A2 BR 112015005181A2 BR 112015005181 A BR112015005181 A BR 112015005181A BR 112015005181 A BR112015005181 A BR 112015005181A BR 112015005181 A2 BR112015005181 A2 BR 112015005181A2
Authority
BR
Brazil
Prior art keywords
turbojet engine
engine nacelle
reversing device
thrust reversing
nacelle
Prior art date
Application number
BR112015005181A
Other languages
English (en)
Inventor
Bellanger Alexandre
Bunel Serge
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 BR112015005181A2 publication Critical patent/BR112015005181A2/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
    • F02K1/64—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
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
BR112015005181A 2012-09-19 2013-09-17 dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato. BR112015005181A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1258769A FR2995637B1 (fr) 2012-09-19 2012-09-19 Structure fixe de dispositif d'inversion de poussee
PCT/FR2013/052135 WO2014044964A1 (fr) 2012-09-19 2013-09-17 Structure fixe de dispositif d'inversion de poussée

Publications (1)

Publication Number Publication Date
BR112015005181A2 true BR112015005181A2 (pt) 2017-10-10

Family

ID=47624221

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015005181A BR112015005181A2 (pt) 2012-09-19 2013-09-17 dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.

Country Status (8)

Country Link
US (1) US10544754B2 (pt)
EP (1) EP2898211B1 (pt)
CN (1) CN104641096B (pt)
BR (1) BR112015005181A2 (pt)
CA (1) CA2882166C (pt)
FR (1) FR2995637B1 (pt)
RU (1) RU2650982C2 (pt)
WO (1) WO2014044964A1 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3023325B1 (fr) * 2014-07-04 2016-07-15 Aircelle Sa Cadre arriere pour une structure d'inverseur de poussee a grilles de deviation
FR3031727B1 (fr) 2015-01-21 2019-07-12 Safran Nacelles Dispositif d’inversion de poussee a grilles mobiles et berceau pour nacelle pour mat du type corps
FR3031728B1 (fr) * 2015-01-21 2017-04-28 Aircelle Sa Dispositif d’inversion de poussee a grilles mobiles et berceau
FR3031726B1 (fr) * 2015-01-21 2017-02-24 Aircelle Sa Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef
FR3073572B1 (fr) 2017-11-16 2020-10-02 Safran Nacelles Inverseur de poussee a grilles mobiles pour ensemble propulsif d’aeronef et procedes de montage et demontage s’y rapportant
US11085395B2 (en) 2017-12-22 2021-08-10 Airbus Operations S.A.S. Nacelle system and methods of operation
FR3087498B1 (fr) * 2018-10-22 2021-03-05 Airbus Operations Sas Turboreacteur comportant une nacelle equipee d’un systeme d’inversion de poussee mobile en translation et d’un carter de soufflante equipe de supports
US10906661B2 (en) * 2018-11-05 2021-02-02 Rohr, Inc. Nacelle cowl hinge
FR3110639B1 (fr) * 2020-05-20 2022-09-16 Safran Nacelles Inverseur de poussee pour une nacelle d’un turboreacteur a double flux d’aeronef
AT523287B1 (de) 2020-07-13 2021-07-15 Facc Ag Kaskadenelement für ein Schubumkehrsystem eines Triebwerks
CN115342005B (zh) * 2022-07-29 2025-05-02 中国航发沈阳发动机研究所 一种反推力装置锁扣梁

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3599432A (en) * 1970-04-02 1971-08-17 Rohr Corp Thrust reversing apparatus for turbo-fan propulsion unit
US4278220A (en) * 1979-03-30 1981-07-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thrust reverser for a long duct fan engine
UA26001C2 (uk) * 1994-08-23 1999-02-26 Запорізьке Машинобудівне Конструкторське Бюро "Прогрес" Ім. Академіка О.Г. Івченка Пристрій кріплеhhя капота реактивhого двигуhа літальhого апарата
US7484356B1 (en) * 2005-07-26 2009-02-03 Aeronautical Concepts Of Exhaust, Llc Cascade reverser without blocker doors
US20080010969A1 (en) * 2006-07-11 2008-01-17 Thomas Anthony Hauer Gas turbine engine and method of operating same
FR2908109B1 (fr) * 2006-11-03 2008-12-12 Aircelle Sa Element de nacelle de turboreacteur
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
FR2938878B1 (fr) * 2008-11-26 2013-11-08 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur a double flux
US20110120078A1 (en) * 2009-11-24 2011-05-26 Schwark Jr Fred W Variable area fan nozzle track
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
US8511973B2 (en) * 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly

Also Published As

Publication number Publication date
US10544754B2 (en) 2020-01-28
US20160273489A1 (en) 2016-09-22
CN104641096A (zh) 2015-05-20
FR2995637B1 (fr) 2018-05-11
RU2015110475A (ru) 2016-11-10
CA2882166A1 (fr) 2014-03-27
FR2995637A1 (fr) 2014-03-21
EP2898211B1 (fr) 2019-04-10
CA2882166C (fr) 2020-08-25
CN104641096B (zh) 2017-09-22
WO2014044964A1 (fr) 2014-03-27
RU2650982C2 (ru) 2018-04-18
EP2898211A1 (fr) 2015-07-29

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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]