ATE432874T1 - Flugzeugmotoranordnung - Google Patents

Flugzeugmotoranordnung

Info

Publication number
ATE432874T1
ATE432874T1 AT05797576T AT05797576T ATE432874T1 AT E432874 T1 ATE432874 T1 AT E432874T1 AT 05797576 T AT05797576 T AT 05797576T AT 05797576 T AT05797576 T AT 05797576T AT E432874 T1 ATE432874 T1 AT E432874T1
Authority
AT
Austria
Prior art keywords
engine
turboshaft engine
mounts
aircraft engine
engine arrangement
Prior art date
Application number
AT05797576T
Other languages
English (en)
Inventor
Lionel Diochon
Isabelle Petrissans
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
Application granted granted Critical
Publication of ATE432874T1 publication Critical patent/ATE432874T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements 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)
  • Vibration Prevention Devices (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Motor Power Transmission Devices (AREA)
  • Retarders (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Connection Of Plates (AREA)
AT05797576T 2004-08-04 2005-08-01 Flugzeugmotoranordnung ATE432874T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451785A FR2873986B1 (fr) 2004-08-04 2004-08-04 Ensemble moteur pour aeronef
PCT/FR2005/050638 WO2006021722A1 (fr) 2004-08-04 2005-08-01 Ensemble moteur pour aeronef

Publications (1)

Publication Number Publication Date
ATE432874T1 true ATE432874T1 (de) 2009-06-15

Family

ID=34948381

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05797576T ATE432874T1 (de) 2004-08-04 2005-08-01 Flugzeugmotoranordnung

Country Status (11)

Country Link
US (1) US7770840B2 (de)
EP (1) EP1773659B9 (de)
JP (1) JP4607963B2 (de)
CN (1) CN100471759C (de)
AT (1) ATE432874T1 (de)
BR (1) BRPI0513869A (de)
CA (1) CA2575982C (de)
DE (1) DE602005014777D1 (de)
FR (1) FR2873986B1 (de)
RU (1) RU2381148C2 (de)
WO (1) WO2006021722A1 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI118761B (fi) * 2006-02-09 2008-03-14 Patria Aerostructures Oy Ilma-aluksen siipi, kiinnitysjärjestely sekä välituki
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
FR2928180B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur.
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.
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2933073B1 (fr) * 2008-06-25 2010-06-04 Aircelle Sa Ensemble d'entree d'air de nacelle de moteur d'avion
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2948636B1 (fr) * 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
FR3027873B1 (fr) * 2014-11-03 2016-12-23 Airbus Operations Sas Attache moteur avant pour un moteur d'aeronef
FR3040369B1 (fr) * 2015-09-02 2018-07-13 Airbus Operations Sas Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree
US10093436B2 (en) * 2016-06-23 2018-10-09 General Electric Company Wireless aircraft engine communication system

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
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.
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5303880A (en) * 1992-10-28 1994-04-19 General Electric Company Aircraft engine pin mount
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
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
US5620154A (en) * 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
FR2770486B1 (fr) * 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
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
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
FR2820402B1 (fr) * 2001-02-08 2003-05-02 Eads Airbus Sa Dispositif d'accrochage d'un moteur sur un aeronef
FR2883256B1 (fr) * 2005-03-18 2008-10-24 Airbus France Sas Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
FR2894934B1 (fr) * 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente

Also Published As

Publication number Publication date
WO2006021722A1 (fr) 2006-03-02
US20070205323A1 (en) 2007-09-06
FR2873986A1 (fr) 2006-02-10
BRPI0513869A (pt) 2008-05-20
DE602005014777D1 (de) 2009-07-16
JP4607963B2 (ja) 2011-01-05
RU2381148C2 (ru) 2010-02-10
US7770840B2 (en) 2010-08-10
CA2575982C (fr) 2013-06-25
CN101014497A (zh) 2007-08-08
EP1773659A1 (de) 2007-04-18
EP1773659B1 (de) 2009-06-03
CN100471759C (zh) 2009-03-25
JP2008509319A (ja) 2008-03-27
EP1773659B9 (de) 2009-09-09
CA2575982A1 (fr) 2006-03-02
FR2873986B1 (fr) 2007-12-21
RU2007107927A (ru) 2008-09-10

Similar Documents

Publication Publication Date Title
ATE432874T1 (de) Flugzeugmotoranordnung
BRPI0513893A (pt) conjunto motor para aeronave, e, aeronave
ATE416975T1 (de) Flugzeugmotoreinheit
WO2010031958A3 (fr) Partie arriere d'aeronef comprenant deux demi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef
ATE521535T1 (de) Flugzeugmotorbefestigungsstruktur mit einem hinteren motorankerträger, der sich in einem abstand vom strukturkasten befindet
TW200731575A (en) Solid state lighting units and methods of forming solid state lighting units
GB2444692A (en) Gas turbine engine auxiliary component mount
DE602006015518D1 (de) Tragelement und herstellungsverfahren
ATE423729T1 (de) Triebwerkanordnung für flugzeug
RU2008114807A (ru) Устройство подвески газотурбинного двигателя и газотурбинный двигатель, содержащий такое устройство подвески
PE20080004A1 (es) Montaje de desgate
WO2009045669A3 (en) Headborne integration system
BRPI0811183A2 (pt) Veículo para todo tipo de terreno
WO2009112777A3 (fr) Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante
ATE540848T1 (de) Fahrzeugrahmenanordnung
WO2015074043A3 (en) Turboprop engine attachment systems and methods
WO2008091376A3 (en) Tiltrotor aircraft drivelink
BR112014007293A2 (pt) conjunto de cabeça de corte para aparelho de corte centrífugo e aparelho centrífugo equipado com o mesmo
EP2434101A3 (de) Dämpfungsanordnung
RU2014117397A (ru) Силовая установка летательного аппарата
ATE551258T1 (de) Hubschrauber
RU2007147944A (ru) Силовая установка летательного аппарата
BRPI0817758A2 (pt) Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave
ATE425918T1 (de) Aufsattelplattform
EA200802064A1 (ru) Обойма с выемками в основаниях кронштейнов

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties