BRPI0616578A8 - estribo de afixação de turborreator para aeronave, e, aeronave - Google Patents

estribo de afixação de turborreator para aeronave, e, aeronave Download PDF

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Publication number
BRPI0616578A8
BRPI0616578A8 BRPI0616578A BRPI0616578A BRPI0616578A8 BR PI0616578 A8 BRPI0616578 A8 BR PI0616578A8 BR PI0616578 A BRPI0616578 A BR PI0616578A BR PI0616578 A BRPI0616578 A BR PI0616578A BR PI0616578 A8 BRPI0616578 A8 BR PI0616578A8
Authority
BR
Brazil
Prior art keywords
aircraft
turborreator
coffin
mounting bracket
coffins
Prior art date
Application number
BRPI0616578A
Other languages
English (en)
Inventor
Chartier David
Cetout Jean-Michel
Lafont Laurent
Diochon Lionel
Original Assignee
Airbus France
Airbus Operations Sas
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 Airbus France, Airbus Operations Sas filed Critical Airbus France
Publication of BRPI0616578A2 publication Critical patent/BRPI0616578A2/pt
Publication of BRPI0616578A8 publication Critical patent/BRPI0616578A8/pt
Publication of BRPI0616578B1 publication Critical patent/BRPI0616578B1/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
    • 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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Assembled Shelves (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
  • Connection Of Plates (AREA)

Abstract

estribo de afixação de turborreator para aeronave, e, aeronave. a invenção se refere a um estribo de afixação de turborreator para aeronave que compreende um caixão central (22) formado pela união de dois painéis laterais ligados por intermédio de nervuras transversais (23), o estribo compreendendo também dois caixões laterais (24a) solidários de uma parte dianteira do caixão (22) e dispostos de um lado e de outro desse último, cada caixão lateral dispondo de um quadro de fechamento traseiro (46a). de acordo com a invenção, uma das nervuras (23) que formam o caixão (22) é equipada de duas extensões laterais (52a) realizadas de um só peça com essa nervura (23) e que formam respectivamente saliência dos dois painéis laterais para o exterior do caixão (22), as duas extensões (52a) sendo montadas fixamente no quadro (46a) de um e de outro dos dois caixões laterais, respectivamente.
BRPI0616578A 2005-10-03 2006-09-29 estribo de afixação de turborreator para aeronave BRPI0616578B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0552989A FR2891526B1 (fr) 2005-10-03 2005-10-03 Mat d'accrochage de turboreacteur pour aeronef
FR0552989 2005-10-03
PCT/EP2006/066873 WO2007039556A1 (fr) 2005-10-03 2006-09-29 Mat d'accrochage de turboreacteur pour aeronef

Publications (3)

Publication Number Publication Date
BRPI0616578A2 BRPI0616578A2 (pt) 2012-12-25
BRPI0616578A8 true BRPI0616578A8 (pt) 2018-05-08
BRPI0616578B1 BRPI0616578B1 (pt) 2018-10-23

Family

ID=36577371

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0616578A BRPI0616578B1 (pt) 2005-10-03 2006-09-29 estribo de afixação de turborreator para aeronave

Country Status (10)

Country Link
US (1) US8070093B2 (pt)
EP (1) EP1931567B8 (pt)
JP (1) JP4864975B2 (pt)
CN (1) CN100548803C8 (pt)
AT (1) ATE552173T1 (pt)
BR (1) BRPI0616578B1 (pt)
CA (1) CA2624457C (pt)
FR (1) FR2891526B1 (pt)
RU (1) RU2399558C9 (pt)
WO (1) WO2007039556A1 (pt)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1912567B1 (en) 2005-08-04 2012-12-26 Bayer HealthCare, LLC Small lancing device
FR2920198B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Structure pour inverseur de poussee
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2928347B1 (fr) * 2008-03-07 2010-06-25 Aircelle Sa Structure d'accrochage pour turboreacteur
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2936493A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat.
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2965548B1 (fr) * 2010-10-01 2012-10-19 Airbus Operations Sas Mat d'accrochage d'un moteur d'aeronef comprenant deux attaches voilure avant a pions de cisaillement orthogonaux
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
CN102849218A (zh) * 2012-09-04 2013-01-02 西安飞机工业（集团）有限责任公司 一种飞机辅助动力装置安装梁
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
FR3012793B1 (fr) * 2013-11-05 2017-05-05 Airbus Operations Sas Ensemble pour aeronef comprenant une ferrure fixee sur la partie extrados d'un caisson de voilure, pour le montage d'un mat d'accrochage sur ce caisson de voilure
CN103569367B (zh) * 2013-11-13 2015-08-26 中国航空工业集团公司西安飞机设计研究所 机翼吊装涡扇发动机飞机的发动机挂架
EP3071481B1 (en) 2013-11-18 2020-01-08 LORD Corporation Turboprop engine attachment systems and methods
FR3015434B1 (fr) * 2013-12-23 2017-12-08 Snecma Suspension de turbomachine
FR3040076B1 (fr) * 2015-08-13 2017-08-11 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
FR3065442B1 (fr) * 2017-04-25 2021-03-19 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une attache moteur avant integree au caisson du mat d'accrochage
JP2019131071A (ja) * 2018-01-31 2019-08-08 三菱重工業株式会社 航空機
US10806087B2 (en) * 2018-05-21 2020-10-20 Deere & Company Fan support arm
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
FR3129376A1 (fr) * 2021-11-19 2023-05-26 Airbus Operations Mat réacteur pour coupler un turboréacteur à une aile d’un aéronef

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4206893A (en) * 1978-09-27 1980-06-10 The Boeing Company Seal closure for slot in engine mounting strut
SU849694A1 (ru) * 1980-03-12 1996-09-20 А.А. Бобух Устройство для крепления двухконтурного турбореактивного двигателя
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method

Also Published As

Publication number Publication date
US20080315033A1 (en) 2008-12-25
RU2399558C9 (ru) 2019-12-30
WO2007039556A8 (fr) 2009-06-11
BRPI0616578A2 (pt) 2012-12-25
EP1931567B8 (fr) 2018-08-08
CN100548803C (zh) 2009-10-14
RU2008117402A (ru) 2009-11-10
CN100548803C8 (zh) 2018-06-29
FR2891526B1 (fr) 2007-11-02
EP1931567B1 (fr) 2012-04-04
RU2399558C2 (ru) 2010-09-20
BRPI0616578B1 (pt) 2018-10-23
US8070093B2 (en) 2011-12-06
CN101272952A (zh) 2008-09-24
WO2007039556A1 (fr) 2007-04-12
FR2891526A1 (fr) 2007-04-06
JP4864975B2 (ja) 2012-02-01
CA2624457C (en) 2013-09-24
CA2624457A1 (en) 2007-04-12
ATE552173T1 (de) 2012-04-15
EP1931567A1 (fr) 2008-06-18
JP2009509847A (ja) 2009-03-12

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Legal Events

Date Code Title Description
B06G Technical and formal requirements: other requirements [chapter 6.7 patent gazette]

Free format text: SOLICITA-SE A REGULARIZACAO DA PROCURACAO, UMA VEZ QUE BASEADO NO ARTIGO 216 1O DA LPI, O DOCUMENTO DE PROCURACAO DEVE SER APRESENTADO NO ORIGINAL, TRASLADO OU FOTOCOPIA AUTENTICADA.

B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 23/10/2018, OBSERVADAS AS CONDICOES LEGAIS.