ATE452823T1 - Strukturgondel - Google Patents

Strukturgondel

Info

Publication number
ATE452823T1
ATE452823T1 AT07788856T AT07788856T ATE452823T1 AT E452823 T1 ATE452823 T1 AT E452823T1 AT 07788856 T AT07788856 T AT 07788856T AT 07788856 T AT07788856 T AT 07788856T AT E452823 T1 ATE452823 T1 AT E452823T1
Authority
AT
Austria
Prior art keywords
nacelle
intended
turboreactor
internal structure
section
Prior art date
Application number
AT07788856T
Other languages
English (en)
Inventor
Guy Vauchel
Anne-Laure Gibouin
Regis Fassier
Jean-Philippe Joret
Jerome Collier
Guillaume Lefort
Pierre-Alain Chouard
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Application granted granted Critical
Publication of ATE452823T1 publication Critical patent/ATE452823T1/de

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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wrappers (AREA)
  • Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
  • Glass Compositions (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Wind Motors (AREA)
AT07788856T 2006-06-30 2007-06-11 Strukturgondel ATE452823T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0605912A FR2903076B1 (fr) 2006-06-30 2006-06-30 Nacelle structurante
PCT/FR2007/000951 WO2008000924A1 (fr) 2006-06-30 2007-06-11 Nacelle structurante

Publications (1)

Publication Number Publication Date
ATE452823T1 true ATE452823T1 (de) 2010-01-15

Family

ID=37762062

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07788856T ATE452823T1 (de) 2006-06-30 2007-06-11 Strukturgondel

Country Status (11)

Country Link
US (1) US8739552B2 (de)
EP (1) EP2035279B1 (de)
CN (1) CN101489870B (de)
AT (1) ATE452823T1 (de)
BR (1) BRPI0713993A2 (de)
CA (1) CA2654398C (de)
DE (1) DE602007003981D1 (de)
ES (1) ES2338385T3 (de)
FR (1) FR2903076B1 (de)
RU (1) RU2424160C2 (de)
WO (1) WO2008000924A1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2076438A2 (de) 2006-10-11 2009-07-08 Aircelle Bypassgasturbinengondel
FR2909974B1 (fr) 2006-12-13 2009-02-06 Aircelle Sa Nacelle pour turboreacteur double flux
FR2938236B1 (fr) * 2008-11-13 2011-04-15 Aircelle Sa Nacelle pour turboreacteur
US8262050B2 (en) * 2008-12-24 2012-09-11 General Electric Company Method and apparatus for mounting and dismounting an aircraft engine
US8469309B2 (en) * 2008-12-24 2013-06-25 General Electric Company Monolithic structure for mounting aircraft engine
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
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
FR2950860B1 (fr) 2009-10-01 2011-12-09 Airbus Operations Sas Dispositif d'accrochage d'un moteur a un mat d'aeronef
DE102009054568A1 (de) * 2009-12-11 2011-06-16 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung zur Aufhängung eines Strahltriebwerks an einer Stützstruktur
GB201007215D0 (en) * 2010-04-30 2010-06-16 Rolls Royce Plc Gas turbine engine
US9212607B2 (en) 2012-07-18 2015-12-15 Spirit Aerosystems, Inc. Intermediate structure for independently de-mountable propulsion components
US20140352797A1 (en) * 2013-06-04 2014-12-04 Rohr, Inc. Aircraft jet engine
FR3010048B1 (fr) * 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a cales de liaison
GB201322077D0 (en) * 2013-12-13 2014-01-29 Rolls Royce Plc Engine mount
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
FR3046201B1 (fr) * 2015-12-24 2018-01-19 Safran Aircraft Engines Turboreacteur avec un moyen de reprise de poussee sur le carter inter-compresseurs
FR3058704B1 (fr) * 2016-11-14 2018-11-16 Safran Aircraft Engines Berceau bipartite a coulissement pour turbopropulseur
FR3060532B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Ensemble moteur pour aeronef, comprenant des dispositifs elastiques souples de transmission d'efforts entre des capots de nacelle et une structure annulaire reliee au carter moteur par des bielles
US10899463B2 (en) 2017-05-16 2021-01-26 Rohr, Inc. Segmented pylon for an aircraft propulsion system
FR3068008B1 (fr) * 2017-06-21 2019-11-08 Airbus Operations Ensemble de motorisation pour un aeronef
FR3075174B1 (fr) 2017-12-18 2020-12-11 Safran Aircraft Engines Structure porteuse destinee au montage sur un generateur de gaz
US11448161B2 (en) 2018-09-10 2022-09-20 Rohr, Inc. Acoustic fairing
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure
CN113771564A (zh) * 2021-08-20 2021-12-10 王全文 一种水陆交通装置
EP4488181A1 (de) * 2023-07-06 2025-01-08 Airbus Operations (S.A.S.) Antriebssystem für ein flugzeug mit einem strahltriebwerk, einem pylon und einer motorbefestigung
FR3166884A1 (fr) * 2024-09-30 2026-04-03 Airbus Operations Ensemble de propulsion d’aéronef comprenant une structure porteuse reliant une motorisation et une structure primaire d’un mât et supportant au moins un accessoire

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1095605A (fr) 1953-08-06 1955-06-03 Perfectionnements apportés aux dispositifs de fixation de panneaux, capots, couvercles, etc.
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
AU555526B2 (en) * 1982-10-29 1986-09-25 General Electric Company Aircraft engine nacelle
DE3374546D1 (en) 1983-12-19 1987-12-23 Boeing Co Apparatus and method for minimizing engine backbone bending
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB2312251B (en) * 1996-04-18 1999-10-27 Rolls Royce Plc Ducted fan gas turbine engine mounting
CN1269308A (zh) * 2000-03-21 2000-10-11 贾龙 一种飞行器的升空和飞行方法及其装置
US6330985B1 (en) * 2000-06-30 2001-12-18 General Electric Company Link component for aircraft engine mounting systems
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
GB0418454D0 (en) * 2004-08-19 2004-09-22 Rolls Royce Plc An engine mounting assembly
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef

Also Published As

Publication number Publication date
CA2654398A1 (fr) 2008-01-03
BRPI0713993A2 (pt) 2012-11-20
EP2035279A1 (de) 2009-03-18
RU2424160C2 (ru) 2011-07-20
WO2008000924A1 (fr) 2008-01-03
FR2903076A1 (fr) 2008-01-04
US8739552B2 (en) 2014-06-03
RU2009102323A (ru) 2010-08-10
CN101489870B (zh) 2013-12-25
CA2654398C (fr) 2015-04-07
ES2338385T3 (es) 2010-05-06
DE602007003981D1 (de) 2010-02-04
US20090255271A1 (en) 2009-10-15
EP2035279B1 (de) 2009-12-23
CN101489870A (zh) 2009-07-22
FR2903076B1 (fr) 2009-05-29

Similar Documents

Publication Publication Date Title
ATE452823T1 (de) Strukturgondel
WO2008093003A8 (fr) Nacelle pour turboréacteur double flux
DE602007009232D1 (de) Motoranordnung für ein luftfahrzeug mit an zwei getrennten elementen angebrachter aerodynamischer kupplungsverteilung
WO2008043903A3 (fr) Nacelle pour turboréacteur double flux
ATE444896T1 (de) Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel
BRPI0818497A2 (pt) Estrutura de entrada de ar para ser montada a montante de uma estrutura intermediária de nacela para motor de avião, e nacela equipada com tal estrutura de entrada de ar.
BRPI0811239A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0815705A2 (pt) Conjunto motor para aeronave, e, aeronave.
BRPI0907478A2 (pt) flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave
BR112012031008A2 (pt) pá em cascata automontada para um reversor de empuxo em cascata para uma nacela de motor turbojato de avião, cascata e montagem da mesma..
WO2009112777A3 (fr) Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante
FR2892705B1 (fr) Aeronef a impact environnemental reduit.
BR112012024647A2 (pt) disposição de haste de ligação de flap de reversor de empuxo sobre a estrutura fixa interna de uma nacela de motor turbojato e nacela de motor turbojato de avião
EP2537755A3 (de) Montageanordnung
WO2009060138A3 (fr) Ensemble propulsif pour aeronef
EP2080700A3 (de) Pylon- und Motorträgerkonfiguration
BR112012022437A2 (pt) sistema de propulsão
WO2009098402A3 (fr) Système de verrouillage pour structure d'entrée d'air d'une nacelle de turboréacteur
EP2330036A3 (de) Träger einer Verdichterhaubenteil für ein Mantelstromtriebwerk
EP2181921A3 (de) Geräuschunterdrückendes Strebenstützsystem für ein unbemanntes Luftfahrzeug
FR2903665B1 (fr) Ensemble moteur pour aeronef comprenant un berceau de support de capot de soufflante monte sur deux elements distincts
BRPI0921378A2 (pt) entrada de ar de um motor de avião do tipo com hélices propulsoras não carenadas, motor de avião e avião
WO2009024662A3 (fr) Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur
WO2010061071A3 (fr) Nacelle integree sur aile volante
BRPI0813609A2 (pt) "nacela de turbojato projetada para ser ajustada em uma aeronave e aeronave"

Legal Events

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