BRPI0513867A - conjunto motor para aeronave, e, aeronave - Google Patents

conjunto motor para aeronave, e, aeronave

Info

Publication number
BRPI0513867A
BRPI0513867A BRPI0513867-1A BRPI0513867A BRPI0513867A BR PI0513867 A BRPI0513867 A BR PI0513867A BR PI0513867 A BRPI0513867 A BR PI0513867A BR PI0513867 A BRPI0513867 A BR PI0513867A
Authority
BR
Brazil
Prior art keywords
aircraft
turbomotor
engine assembly
mast
solidary
Prior art date
Application number
BRPI0513867-1A
Other languages
English (en)
Inventor
Lionel Diochon
Guillaume Seguin
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 BRPI0513867A publication Critical patent/BRPI0513867A/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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Gas-Insulated Switchgears (AREA)
  • Air Bags (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

CONJUNTO MOTOR PARA AERONAVE, E, AERONAVE A invenção se refere a um conjunto motor para aeronave que compreende um turbomotor, um mastro de fixação assim como uma pluralidade de liames de motor interpostos entre o mastro de fixação e o turbomotor. De acordo com a invenção, a pluralidade de liames de motor compreende um liame (6a) projetado de maneira a assegurar unicamente a compensação dos esforços que são exercidos de acordo com uma direção transversal (Y) do turbomotor, esse liame (6a) compreendendo uma ferragem intermediária (46) unida em uma primeira ferragem (40) solidária do mastro por intermédio de dois eixos rótulas (48) orientados paralelamente de acordo com uma direção vertical (Z), assim como um pião (56) orientado de acordo com uma direção longitudinal (X) e solidário da ferragem intermediária, o pião sendo montado com folga na direção longitudinal (X) em uma segunda ferragem (58) solidária do turbomotor.
BRPI0513867-1A 2004-08-04 2005-08-01 conjunto motor para aeronave, e, aeronave BRPI0513867A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451784A FR2873985B1 (fr) 2004-08-04 2004-08-04 Ensemble moteur pour aeronef
PCT/FR2005/050637 WO2006021721A1 (fr) 2004-08-04 2005-08-01 Ensemble moteur pour aeronef

Publications (1)

Publication Number Publication Date
BRPI0513867A true BRPI0513867A (pt) 2008-05-20

Family

ID=34947592

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0513867-1A BRPI0513867A (pt) 2004-08-04 2005-08-01 conjunto motor para aeronave, e, aeronave

Country Status (11)

Country Link
US (1) US7624945B2 (pt)
EP (1) EP1773660B1 (pt)
JP (1) JP4676982B2 (pt)
CN (1) CN1993268B (pt)
AT (1) ATE416975T1 (pt)
BR (1) BRPI0513867A (pt)
CA (1) CA2576518C (pt)
DE (1) DE602005011633D1 (pt)
FR (1) FR2873985B1 (pt)
RU (1) RU2381149C2 (pt)
WO (1) WO2006021721A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2891243B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891252B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Mat a ossature monolithique
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
GB2434836B (en) * 2006-02-04 2008-12-10 Rolls Royce Plc Mounting system for use in mounting a gas turbine engine
FI118761B (fi) * 2006-02-09 2008-03-14 Patria Aerostructures Oy Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki
FR2901243B1 (fr) * 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
US7770841B2 (en) * 2006-12-22 2010-08-10 Calvin Burgess Inverted airfoil pylon for an aircraft
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.
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
FR2931133B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur comprenant des moyens de fixation des longerons et des panneaux agences en dehors de l'espace interieur de caisson
FR3029504B1 (fr) * 2014-12-09 2018-03-30 Airbus Operations (S.A.S.) Attache moteur avant d'aeronef
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
FR3040369B1 (fr) * 2015-09-02 2018-07-13 Airbus Operations Sas Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree
FR3061480B1 (fr) 2016-12-30 2019-05-31 Airbus Operations Ensemble moteur pour aeronef comprenant une attache moteur avant facilitant son montage
FR3075174B1 (fr) * 2017-12-18 2020-12-11 Safran Aircraft Engines Structure porteuse destinee au montage sur un generateur de gaz
FR3076282B1 (fr) 2017-12-29 2020-02-07 Airbus Operations Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure par des attaches presentant un encombrement reduit dans la zone de bord d'attaque
CN112709613B (zh) * 2020-12-30 2023-01-17 中国航发沈阳发动机研究所 一种航空发动机侧向辅助安装节结构

Family Cites Families (14)

* 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
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
DE69012071T2 (de) * 1989-12-05 1995-04-13 Rolls Royce Plc Ausfallsichere Haltevorrichtung für Treibwerke.
FR2676707B1 (fr) * 1991-05-23 1993-08-13 Snecma Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
FR2680353B1 (fr) * 1991-08-14 1993-10-15 Snecma Structure d'accrochage arriere d'un turboreacteur.
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
EP0784564B1 (en) * 1994-10-18 1998-12-30 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
FR2770486B1 (fr) * 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
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
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat

Also Published As

Publication number Publication date
JP4676982B2 (ja) 2011-04-27
CN1993268A (zh) 2007-07-04
CA2576518A1 (en) 2006-03-02
FR2873985A1 (fr) 2006-02-10
CN1993268B (zh) 2011-06-15
EP1773660B1 (fr) 2008-12-10
RU2007107929A (ru) 2008-09-10
FR2873985B1 (fr) 2006-11-24
WO2006021721A1 (fr) 2006-03-02
US20070228213A1 (en) 2007-10-04
ATE416975T1 (de) 2008-12-15
EP1773660A1 (fr) 2007-04-18
RU2381149C2 (ru) 2010-02-10
DE602005011633D1 (de) 2009-01-22
CA2576518C (en) 2014-02-25
US7624945B2 (en) 2009-12-01
JP2008509318A (ja) 2008-03-27

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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 13A 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 2473 DE 29-05-2018 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.