BR112014001123A2 - viga longitudinal para uma estrutura de suporte de nacela de motor turbojato, meia-estrutura de suporte para uma nacela e nacela para um motor de aeronave - Google Patents

viga longitudinal para uma estrutura de suporte de nacela de motor turbojato, meia-estrutura de suporte para uma nacela e nacela para um motor de aeronave

Info

Publication number
BR112014001123A2
BR112014001123A2 BR112014001123A BR112014001123A BR112014001123A2 BR 112014001123 A2 BR112014001123 A2 BR 112014001123A2 BR 112014001123 A BR112014001123 A BR 112014001123A BR 112014001123 A BR112014001123 A BR 112014001123A BR 112014001123 A2 BR112014001123 A2 BR 112014001123A2
Authority
BR
Brazil
Prior art keywords
nacelle
engine nacelle
frame
longitudinal beam
nacelle support
Prior art date
Application number
BR112014001123A
Other languages
English (en)
Inventor
Le Boulicaut Loïc
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 BR112014001123A2 publication Critical patent/BR112014001123A2/pt

Links

Classifications

    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Moulding By Coating Moulds (AREA)
  • Body Structure For Vehicles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BR112014001123A 2011-08-03 2012-07-05 viga longitudinal para uma estrutura de suporte de nacela de motor turbojato, meia-estrutura de suporte para uma nacela e nacela para um motor de aeronave BR112014001123A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1157108A FR2978729B1 (fr) 2011-08-03 2011-08-03 Poutre composite pour structure support de nacelle de turboreacteur
PCT/FR2012/051582 WO2013017759A2 (fr) 2011-08-03 2012-07-05 Poutre composite pour structure support de nacelle de turboréacteur

Publications (1)

Publication Number Publication Date
BR112014001123A2 true BR112014001123A2 (pt) 2017-02-14

Family

ID=46639576

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014001123A BR112014001123A2 (pt) 2011-08-03 2012-07-05 viga longitudinal para uma estrutura de suporte de nacela de motor turbojato, meia-estrutura de suporte para uma nacela e nacela para um motor de aeronave

Country Status (8)

Country Link
US (1) US9260193B2 (pt)
EP (1) EP2739533A2 (pt)
CN (1) CN103732494A (pt)
BR (1) BR112014001123A2 (pt)
CA (1) CA2842570A1 (pt)
FR (1) FR2978729B1 (pt)
RU (1) RU2014106964A (pt)
WO (1) WO2013017759A2 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2988407B1 (fr) * 2012-03-22 2014-10-31 Aircelle Sa Procede de fabrication d'une preforme monobloc pour structure composite
US9897007B2 (en) 2012-07-24 2018-02-20 Rohr, Inc. Thrust reverser-integrated track beam and inner fixed structure
EP2690018B1 (en) * 2012-07-24 2020-03-11 Rohr Inc. Hybrid hinge and latch beam
US10738738B2 (en) 2016-06-17 2020-08-11 Rohr, Inc. Nacelle with bifurcation extension and integral structural reinforcement

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1053338A (fr) 1952-04-03 1954-02-02 Procédé pour la fabrication de stylographes et crayons à bille
US5239822A (en) * 1992-01-14 1993-08-31 The Boeing Company Composite structure for thrust reverser torque box
US6584763B2 (en) * 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
US7083143B2 (en) * 2003-10-17 2006-08-01 The Boeing Company Apparatuses and methods for attaching engines and other structures to aircraft wings
FR2891803B1 (fr) * 2005-10-07 2007-11-30 Airbus France Sas Structure rigide pour mat d'accrochage de moteur d'aeronef, et mat comportant une telle structure
FR2908109B1 (fr) * 2006-11-03 2008-12-12 Aircelle Sa Element de nacelle de turboreacteur
GB0712553D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Composite panel stiffener
FR2920192B1 (fr) 2007-08-23 2014-06-06 Valeo Equip Electr Moteur Procede et dispositif de commande d'un systeme d'arret/relance moteur apte a equiper un vehicule automobile
FR2926605B1 (fr) * 2008-01-18 2012-08-31 Aircelle Sa Structure 12 heures pour inverseur de poussee notamment a grilles
US8262050B2 (en) * 2008-12-24 2012-09-11 General Electric Company Method and apparatus for mounting and dismounting an aircraft engine
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2958910B1 (fr) * 2010-04-20 2012-04-27 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
FR2959487B1 (fr) * 2010-04-29 2012-04-13 Aircelle Sa Nacelle pour moteur d'aeronef
FR2959486B1 (fr) * 2010-04-29 2012-04-13 Aircelle Sa Nacelle pour moteur d'aeronef
FR2963949A1 (fr) * 2010-08-18 2012-02-24 Aircelle Sa Poutre notamment pour inverseur de poussee a grilles
US20130119191A1 (en) * 2011-11-10 2013-05-16 General Electric Company Load-bearing structures for aircraft engines and processes therefor
US9109541B2 (en) * 2012-10-31 2015-08-18 Rohr, Inc. Lock for a translating sleeve of a nacelle

Also Published As

Publication number Publication date
CN103732494A (zh) 2014-04-16
FR2978729B1 (fr) 2013-07-19
WO2013017759A3 (fr) 2013-03-28
FR2978729A1 (fr) 2013-02-08
WO2013017759A2 (fr) 2013-02-07
RU2014106964A (ru) 2015-09-10
EP2739533A2 (fr) 2014-06-11
US20140145060A1 (en) 2014-05-29
US9260193B2 (en) 2016-02-16
CA2842570A1 (fr) 2013-02-07

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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]