BRPI0513892A - mastro de fixação de um turborreator para aeronave, e, aeronave - Google Patents

mastro de fixação de um turborreator para aeronave, e, aeronave

Info

Publication number
BRPI0513892A
BRPI0513892A BRPI0513892-2A BRPI0513892A BRPI0513892A BR PI0513892 A BRPI0513892 A BR PI0513892A BR PI0513892 A BRPI0513892 A BR PI0513892A BR PI0513892 A BRPI0513892 A BR PI0513892A
Authority
BR
Brazil
Prior art keywords
aircraft
arches
mast
turborreator
mast fixing
Prior art date
Application number
BRPI0513892-2A
Other languages
English (en)
Inventor
Lionel Diochon
Jerome Durand
Original Assignee
Airbus France
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 filed Critical Airbus France
Publication of BRPI0513892A publication Critical patent/BRPI0513892A/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
    • B64D27/40—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Vibration Dampers (AREA)
  • Tires In General (AREA)

Abstract

MASTRO DE FIXAçãO DE UM TURBORREATOR PARA AERONAVE, E, AERONAVE A invenção se refere a um mastro de fixação de turborreator para aeronave, o mastro dispondo de uma estrutura rígida (10) munida de uma pluralidade de arcos (30) dispostos de modo a delimitar conjuntamente uma parte de uma superfície fictícia (32) sensivelmente cilíndrica de seção circular. A pluralidade de arcos compreende notadamente dois arcos laterais de compensação dos esforços de impulsão (28) dispostos respectivamente de um lado e de outro de um caixão central (20), cada um dos dois arcos laterais (28) sendo solidarizado por um lado a cada arco em forma de porção anular (26) centrado no eixo longitudinal da superfície fictícia, e por outro lado ao caixão central.
BRPI0513892-2A 2004-08-05 2005-08-03 mastro de fixação de um turborreator para aeronave, e, aeronave BRPI0513892A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451791A FR2873988B1 (fr) 2004-08-05 2004-08-05 Mat d'accrochage de turboreacteur pour aeronef
PCT/FR2005/050645 WO2006090032A1 (fr) 2004-08-05 2005-08-03 Mat d'accrochage de turboreacteur pour aeronef

Publications (1)

Publication Number Publication Date
BRPI0513892A true BRPI0513892A (pt) 2008-05-20

Family

ID=34948383

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0513892-2A BRPI0513892A (pt) 2004-08-05 2005-08-03 mastro de fixação de um turborreator para aeronave, e, aeronave

Country Status (11)

Country Link
US (1) US7784733B2 (pt)
EP (1) EP1789320B1 (pt)
JP (1) JP4729573B2 (pt)
CN (1) CN100422046C (pt)
AT (1) ATE398074T1 (pt)
BR (1) BRPI0513892A (pt)
CA (1) CA2576100C (pt)
DE (1) DE602005007507D1 (pt)
FR (1) FR2873988B1 (pt)
RU (1) RU2381150C2 (pt)
WO (1) WO2006090032A1 (pt)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2905990A1 (fr) 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
US8523516B2 (en) 2006-10-11 2013-09-03 Aircelle Bypass turbojet engine nacelle
FR2913664B1 (fr) * 2007-03-16 2009-07-24 Aircelle Sa Nacelle pour turboreacteur double flux
FR2907098B1 (fr) * 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
FR2917710A1 (fr) * 2007-06-22 2008-12-26 Aircelle Sa Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
FR2931134B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur d'aeronef comprenant un caisson de section en forme de cercle ou d'ellipse
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2939101B1 (fr) * 2008-12-01 2010-12-31 Airbus France Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation
FR2950322B1 (fr) 2009-09-22 2012-05-25 Airbus Operations Sas Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
FR2950323B1 (fr) 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2993535B1 (fr) * 2012-07-20 2015-03-06 Airbus Operations Sas Ensemble propulsif comprenant un turboreacteur a double flux de tres grand diametre et son dispositif d'accrochage sous la voilure d'un aeronef
US9211955B1 (en) 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon
FR3015433B1 (fr) * 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
FR3021029B1 (fr) * 2014-05-16 2016-05-06 Airbus Operations Sas Carenage aerodynamique
FR3021843B1 (fr) * 2014-06-06 2016-07-08 Lesaffre & Cie Methode et composition pour ameliorer la productivite de plantes non legumineuses
US20160167798A1 (en) * 2014-12-12 2016-06-16 General Electric Company Variable pitch mounting for aircraft gas turbine engine
FR3040043B1 (fr) * 2015-08-12 2019-04-12 Sogeclair Sa Mat de moteur d'aeronef a ossature multifonctionnelle integree
US9868539B2 (en) * 2015-09-24 2018-01-16 Embraer S.A. Aircraft engine pylon to wing mounting assembly
US10144525B2 (en) * 2015-09-24 2018-12-04 Embraer S.A. Aircraft engine pylon to wing mounting assembly
FR3045570B1 (fr) * 2015-12-16 2017-12-22 Airbus Operations Sas Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
FR3075174B1 (fr) 2017-12-18 2020-12-11 Safran Aircraft Engines Structure porteuse destinee au montage sur un generateur de gaz
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
FR3115766B1 (fr) * 2020-11-02 2023-03-31 Safran Nacelles Nacelle pour ensemble propulsif d’aéronef, comprenant une bielle de sécurité formant renfort structural
CN114030626B (zh) * 2021-11-30 2024-04-05 北京航星机器制造有限公司 一种不易断裂的挂架、无人机及物品挂载于无人机的方法
US20230182910A1 (en) * 2021-12-13 2023-06-15 Spirit Aerosystems, Inc. Aircraft engine attachment assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon

Also Published As

Publication number Publication date
EP1789320A1 (fr) 2007-05-30
US20070205324A1 (en) 2007-09-06
RU2381150C2 (ru) 2010-02-10
CA2576100A1 (fr) 2006-08-31
JP4729573B2 (ja) 2011-07-20
WO2006090032A1 (fr) 2006-08-31
CN100422046C (zh) 2008-10-01
ATE398074T1 (de) 2008-07-15
FR2873988A1 (fr) 2006-02-10
EP1789320B1 (fr) 2008-06-11
JP2008509041A (ja) 2008-03-27
CN1993266A (zh) 2007-07-04
DE602005007507D1 (de) 2008-07-24
RU2007107930A (ru) 2008-09-10
US7784733B2 (en) 2010-08-31
FR2873988B1 (fr) 2007-12-21
CA2576100C (fr) 2013-07-02

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 10A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2317 DE 02-06-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.