DE602009000808D1 - Anordnung aus einem Nebenstromtriebwerk, einem Pylon zum Befestigen an einer Flugzeugstruktur und einer Aufhängung des Nebenstromtriebwerks am Pylon - Google Patents

Anordnung aus einem Nebenstromtriebwerk, einem Pylon zum Befestigen an einer Flugzeugstruktur und einer Aufhängung des Nebenstromtriebwerks am Pylon

Info

Publication number
DE602009000808D1
DE602009000808D1 DE602009000808T DE602009000808T DE602009000808D1 DE 602009000808 D1 DE602009000808 D1 DE 602009000808D1 DE 602009000808 T DE602009000808 T DE 602009000808T DE 602009000808 T DE602009000808 T DE 602009000808T DE 602009000808 D1 DE602009000808 D1 DE 602009000808D1
Authority
DE
Germany
Prior art keywords
pylon
bypass engine
suspension
attachment
arrangement
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
DE602009000808T
Other languages
English (en)
Inventor
Wouter Balk
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602009000808D1 publication Critical patent/DE602009000808D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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)
DE602009000808T 2008-01-25 2009-01-23 Anordnung aus einem Nebenstromtriebwerk, einem Pylon zum Befestigen an einer Flugzeugstruktur und einer Aufhängung des Nebenstromtriebwerks am Pylon Active DE602009000808D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0800402A FR2926788B1 (fr) 2008-01-25 2008-01-25 Fixation d'un turboreacteur multiflux a un aeronef

Publications (1)

Publication Number Publication Date
DE602009000808D1 true DE602009000808D1 (de) 2011-04-21

Family

ID=39689146

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602009000808T Active DE602009000808D1 (de) 2008-01-25 2009-01-23 Anordnung aus einem Nebenstromtriebwerk, einem Pylon zum Befestigen an einer Flugzeugstruktur und einer Aufhängung des Nebenstromtriebwerks am Pylon

Country Status (7)

Country Link
US (1) US8215580B2 (de)
EP (1) EP2082961B1 (de)
JP (1) JP5522949B2 (de)
CA (1) CA2651013C (de)
DE (1) DE602009000808D1 (de)
FR (1) FR2926788B1 (de)
RU (1) RU2483004C2 (de)

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FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2952672B1 (fr) * 2009-11-17 2011-12-09 Snecma Montage d'un boitier d'accessoires sur un carter intermediaire pour compartiment de soufflante de turboreacteur
US8272595B2 (en) * 2009-11-27 2012-09-25 Rohr, Inc. Fan cowl support for a turbofan engine
FR2969578B1 (fr) * 2010-12-27 2013-02-08 Snecma Dispositif de suspension d'un turboreacteur
US8727269B2 (en) * 2011-06-06 2014-05-20 General Electric Company System and method for mounting an aircraft engine
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
US9091210B2 (en) * 2012-04-26 2015-07-28 United Technologies Corporation TEC mount redundant fastening
US8985509B2 (en) * 2012-08-31 2015-03-24 United Technologies Corporation Assembly for mounting a turbine engine to a pylon
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
FR3010700B1 (fr) 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
FR3015432B1 (fr) * 2013-12-19 2017-12-08 Airbus Operations Sas Ensemble pour aeronef comprenant un moteur a hauteur reglable et procede de commande de l'aeronef
RU2554046C1 (ru) * 2014-03-03 2015-06-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Курганский государственный университет" Крепление авиадвигателя к крылу
FR3040369B1 (fr) * 2015-09-02 2018-07-13 Airbus Operations Sas Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree
US10815804B2 (en) 2017-04-04 2020-10-27 General Electric Company Turbine engine containment assembly and method for manufacturing the same
US10723471B2 (en) * 2017-06-14 2020-07-28 General Electric Company Method and system for mounting an aircraft engine
US10814993B2 (en) 2017-08-21 2020-10-27 Raytheon Technologies Corporation Inlet cowl deflection limiting strut
CN107963225B (zh) * 2017-11-30 2021-06-04 中国商用飞机有限责任公司 飞机发动机吊挂及其吊挂盒段
US11939070B2 (en) 2020-02-21 2024-03-26 General Electric Company Engine-mounting links that have an adjustable inclination angle
US11970279B2 (en) 2020-02-21 2024-04-30 General Electric Company Control system and methods of controlling an engine-mounting link system

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FR2867157B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867156B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867158B1 (fr) * 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
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FR2891250B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
US8235325B2 (en) * 2005-10-04 2012-08-07 United Technologies Corporation Fan variable area nozzle positional measurement system
US8439299B2 (en) * 2005-12-21 2013-05-14 General Electric Company Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount
JP2007292194A (ja) * 2006-04-25 2007-11-08 Mitsubishi Heavy Ind Ltd 発電プラント
FR2903665B1 (fr) * 2006-07-11 2008-10-10 Airbus France Sas Ensemble moteur pour aeronef comprenant un berceau de support de capot de soufflante monte sur deux elements distincts
FR2915175B1 (fr) * 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
FR2920408B1 (fr) * 2007-08-30 2010-02-19 Snecma Pylone de suspension d'un moteur sous une aile d'avion

Also Published As

Publication number Publication date
CA2651013C (fr) 2016-01-12
FR2926788B1 (fr) 2010-04-02
RU2009102234A (ru) 2010-07-27
US8215580B2 (en) 2012-07-10
JP5522949B2 (ja) 2014-06-18
CA2651013A1 (fr) 2009-07-25
EP2082961A1 (de) 2009-07-29
RU2483004C2 (ru) 2013-05-27
EP2082961B1 (de) 2011-03-09
JP2009173277A (ja) 2009-08-06
US20090189014A1 (en) 2009-07-30
FR2926788A1 (fr) 2009-07-31

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