ATE475592T1 - Befestigungssystem für ein bauteil einer triebwerksgondel - Google Patents

Befestigungssystem für ein bauteil einer triebwerksgondel

Info

Publication number
ATE475592T1
ATE475592T1 AT07718053T AT07718053T ATE475592T1 AT E475592 T1 ATE475592 T1 AT E475592T1 AT 07718053 T AT07718053 T AT 07718053T AT 07718053 T AT07718053 T AT 07718053T AT E475592 T1 ATE475592 T1 AT E475592T1
Authority
AT
Austria
Prior art keywords
component
fixing means
engine
nachel
pod
Prior art date
Application number
AT07718053T
Other languages
English (en)
Inventor
Guy Vauchel
Patrick Gonidec
Pascal Rouyer
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 ATE475592T1 publication Critical patent/ATE475592T1/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
    • B64D29/08—Inspection panels for power plants
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Coating With Molten Metal (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
  • Connection Of Plates (AREA)
  • Wind Motors (AREA)
AT07718053T 2006-01-23 2007-01-18 Befestigungssystem für ein bauteil einer triebwerksgondel ATE475592T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0600563A FR2896481B1 (fr) 2006-01-23 2006-01-23 Systeme de fixation pour element constitutif d'une nacelle de turboreacteur
PCT/FR2007/000088 WO2007083024A1 (fr) 2006-01-23 2007-01-18 Systeme de fixation pour element constitutif d'une nacelle de turboreacteur

Publications (1)

Publication Number Publication Date
ATE475592T1 true ATE475592T1 (de) 2010-08-15

Family

ID=37076221

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07718053T ATE475592T1 (de) 2006-01-23 2007-01-18 Befestigungssystem für ein bauteil einer triebwerksgondel

Country Status (10)

Country Link
US (1) US20090165463A1 (de)
EP (1) EP1976758B1 (de)
CN (1) CN101360649B (de)
AT (1) ATE475592T1 (de)
CA (1) CA2637892A1 (de)
DE (1) DE602007008057D1 (de)
ES (1) ES2348750T3 (de)
FR (1) FR2896481B1 (de)
RU (1) RU2433071C2 (de)
WO (1) WO2007083024A1 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920136B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Systeme de liaison entre une structure interne et un structure externe d'une nacelle
FR2933957B1 (fr) * 2008-07-18 2010-07-30 Airbus France Dispositif pour ceinturer une nacelle d'aeronef
FR2952403B1 (fr) * 2009-11-12 2012-01-13 Snecma Structure annulaire metallique de raccord pour turbomachine d'aeronef
FR2960855A1 (fr) * 2010-06-03 2011-12-09 Aircelle Sa Nacelle pour turboreacteur avec dispositif de reprise d'efforts circonferentiels
FR2967398B1 (fr) 2010-11-16 2012-11-02 Aircelle Sa Structure de renforcement d'une nacelle de turboreacteur
US9404507B2 (en) 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
US9915225B2 (en) 2015-02-06 2018-03-13 United Technologies Corporation Propulsion system arrangement for turbofan gas turbine engine
FR3032480B1 (fr) * 2015-02-09 2018-07-27 Safran Aircraft Engines Ensemble de redressement d'air a performances aerodynamiques ameliorees
US10150568B2 (en) * 2016-01-27 2018-12-11 Rohr, Inc. Thrust reverser compression rod with spring biased engagement
FR3053957B1 (fr) * 2016-07-12 2018-08-31 Safran Nacelles Ensemble arriere de nacelle de turboreacteur comportant un dispositif d'etancheite anti-feu
CN107985634A (zh) * 2017-11-29 2018-05-04 中山市小榄企业服务有限公司 一种航空航天推进器部件
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
FR3124493B1 (fr) * 2021-06-28 2023-10-20 Safran Nacelles Ensemble propulsif comprenant des panneaux de bifurcation pendulaires

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2379434A1 (fr) * 1977-02-08 1978-09-01 Snecma Systeme de verrouillage de capotage coulissant de nacelle de turboreacteur
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB8822798D0 (en) * 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine
FR2772342B1 (fr) * 1997-12-16 2000-02-18 Aerospatiale Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
US6517027B1 (en) * 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
FR2856379B1 (fr) * 2003-06-18 2006-11-24 Airbus France Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
FR2869290B1 (fr) * 2004-04-27 2006-07-21 Hurel Hispano Sa Groupe turbopropulseur pour aeronef a installation aerodynamique amelioree
US7083144B2 (en) * 2004-08-18 2006-08-01 The Boeing Company Apparatus and methods for support of propulsion systems interconnect members
US7275362B2 (en) * 2004-09-08 2007-10-02 The Boeing Company Thrust reversers including latching mechanisms and methods for manufacturing such thrust reversers

Also Published As

Publication number Publication date
RU2008133762A (ru) 2010-02-27
ES2348750T3 (es) 2010-12-13
EP1976758B1 (de) 2010-07-28
CA2637892A1 (fr) 2007-07-26
WO2007083024A1 (fr) 2007-07-26
RU2433071C2 (ru) 2011-11-10
CN101360649A (zh) 2009-02-04
CN101360649B (zh) 2013-03-27
FR2896481A1 (fr) 2007-07-27
US20090165463A1 (en) 2009-07-02
FR2896481B1 (fr) 2009-12-04
DE602007008057D1 (de) 2010-09-09
EP1976758A1 (de) 2008-10-08

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Legal Events

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