[go: up one dir, main page]

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
    • 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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Gas-Insulated Switchgears (AREA)
  • Air Bags (AREA)
  • Vibration Prevention Devices (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (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 (20)

* 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
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.
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.
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
EP4506258A1 (en) * 2023-08-09 2025-02-12 Airbus Operations (S.A.S.) Propulsion system for an aircraft comprising a turbojet, a pylon and engine attachment
FR3156756A1 (fr) * 2023-12-14 2025-06-20 Airbus Operations Ensemble propulsif pour aéronef comportant un moteur, un mât et des moyens d’accrochage du moteur au mât

Family Cites Families (16)

* 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
SU849694A1 (ru) * 1980-03-12 1996-09-20 А.А. Бобух Устройство для крепления двухконтурного турбореактивного двигателя
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
EP0431800B1 (en) * 1989-12-05 1994-08-31 ROLLS-ROYCE plc Failure tolerant engine mounting
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.
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
JP3599342B2 (ja) * 1994-10-18 2004-12-08 ユナイテッド テクノロジーズ コーポレイション 航空機エンジンのためのナセル及びその取り付け配置
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
US7624945B2 (en) 2009-12-01
ATE416975T1 (de) 2008-12-15
US20070228213A1 (en) 2007-10-04
RU2007107929A (ru) 2008-09-10
WO2006021721A1 (fr) 2006-03-02
DE602005011633D1 (de) 2009-01-22
FR2873985A1 (fr) 2006-02-10
CA2576518C (en) 2014-02-25
CN1993268B (zh) 2011-06-15
JP4676982B2 (ja) 2011-04-27
CN1993268A (zh) 2007-07-04
RU2381149C2 (ru) 2010-02-10
JP2008509318A (ja) 2008-03-27
CA2576518A1 (en) 2006-03-02
EP1773660A1 (fr) 2007-04-18
EP1773660B1 (fr) 2008-12-10
FR2873985B1 (fr) 2006-11-24

Similar Documents

Publication Publication Date Title
BRPI0513867A (pt) conjunto motor para aeronave, e, aeronave
ES2613412T3 (es) Muelle laminar para vehículos automóviles
WO2009038088A1 (ja) 車体の側部構造
BRPI0703307A (pt) instalação de elevador com uma correia, correia para essa instalação de elevador, processo para produção dessa correia, conjunto dessas correias, bem como processo para montagem desse conjunto em uma instalação de elevador
ATE483630T1 (de) Leichter flugzeugpassagiersitz mit verbundkonstruktion
DE602007003361D1 (de) Vorrichtung zur triebwerksbefestigung mit zwei schräg zusammenpassenden schubreaktionsverbindungsstangen
BRPI0513869A (pt) conjunto motor para aeronave, e, aeronave
ES2570582T3 (es) Acoplamiento de herramienta
DE602008003807D1 (de) Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln
WO2011057827A8 (de) Belastungseinrichtung zur erzeugung von flächenlasten auf plattenförmige prüfkörper
CL2008001769A1 (es) Metodo para conectar un primer componente y un segundo componente, donde cada uno de los componentes comprende a lo menos una disposicion de clavijeros, el metodo comprende los pasos de alinear las disposiciones de clavijeros y extender longitudinalmente un conector entre las clavijas; y un conjunto de componentes.
WO2008091376A3 (en) Tiltrotor aircraft drivelink
MX2009001256A (es) Mecanismo impulsor de cuña con dispositivo de retorno de acción positiva.
BR112012029960A2 (pt) torno subterrâneo com conjunto de rodas
ATE551258T1 (de) Hubschrauber
WO2010100471A3 (en) Seat assembly
ATE375502T1 (de) Vorrichtung zum wiegen gleichgearteter wägegüter
WO2011023396A3 (en) Aircraft having at least two electrical propulsion groups mounted at a rear portion thereof
BR112013004252A2 (pt) conjunto de suporte para um veículo de manipulação de materiais, veículo de manipulação de materiais, e, método de instalação de um conjunto de roda de carga
MA38311A1 (fr) Structure à base de carton
ATE423729T1 (de) Triebwerkanordnung für flugzeug
BR112014017002A8 (pt) dispositivo de comutação elétrico com uma parte de guia
SE0403194D0 (sv) An annular torsional rigid static component for an aircraft engine
ATE505109T1 (de) Stützstruktur zur lagerung und handhabung von fässern
ATE510072T1 (de) Fahrzeug mit einer bugseitig angeordeten stütz- und räumanlage

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.