DE602008003807D1 - Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln - Google Patents

Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln

Info

Publication number
DE602008003807D1
DE602008003807D1 DE602008003807T DE602008003807T DE602008003807D1 DE 602008003807 D1 DE602008003807 D1 DE 602008003807D1 DE 602008003807 T DE602008003807 T DE 602008003807T DE 602008003807 T DE602008003807 T DE 602008003807T DE 602008003807 D1 DE602008003807 D1 DE 602008003807D1
Authority
DE
Germany
Prior art keywords
fastening device
fixing agents
turbo engine
rigid structure
hydraulic fixing
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
DE602008003807T
Other languages
English (en)
Inventor
Herve Marche
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602008003807D1 publication Critical patent/DE602008003807D1/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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • 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)
  • Supercharger (AREA)
  • Clamps And Clips (AREA)
  • Vibration Prevention Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Manipulator (AREA)
  • Connection Of Plates (AREA)
  • Actuator (AREA)
DE602008003807T 2007-06-04 2008-06-02 Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln Active DE602008003807D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0755449A FR2916736B1 (fr) 2007-06-04 2007-06-04 Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques.
PCT/EP2008/056742 WO2008148722A1 (fr) 2007-06-04 2008-06-02 Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques

Publications (1)

Publication Number Publication Date
DE602008003807D1 true DE602008003807D1 (de) 2011-01-13

Family

ID=38770953

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008003807T Active DE602008003807D1 (de) 2007-06-04 2008-06-02 Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln

Country Status (6)

Country Link
US (1) US8226028B2 (de)
EP (1) EP2162358B1 (de)
AT (1) ATE490178T1 (de)
DE (1) DE602008003807D1 (de)
FR (1) FR2916736B1 (de)
WO (1) WO2008148722A1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2939103B1 (fr) * 2008-12-01 2011-01-21 Airbus France Systeme hydraulique de transmission d'efforts entre un turbopropulseur d'aeronef et un dispositif d'accrochage
FR2955311B1 (fr) * 2010-01-15 2012-03-23 Airbus Operations Sas Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef
FR2959210B1 (fr) * 2010-04-21 2013-08-23 Snecma Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee
FR2993535B1 (fr) * 2012-07-20 2015-03-06 Airbus Operations Sas Ensemble propulsif comprenant un turboreacteur a double flux de tres grand diametre et son dispositif d'accrochage sous la voilure d'un aeronef
US9211955B1 (en) 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine
CN103303483B (zh) * 2013-04-16 2015-12-30 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机安装维护用旋转机构
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
CN106414241B (zh) * 2013-11-18 2019-03-01 洛德公司 涡轮螺旋桨发动机的附接系统和方法
GB201322077D0 (en) * 2013-12-13 2014-01-29 Rolls Royce Plc Engine mount
FR3016344B1 (fr) * 2014-01-10 2017-09-01 Snecma Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef a fixation rigide de la structure d'entree d'air
US9238511B2 (en) 2014-03-04 2016-01-19 Mra Systems, Inc. Engine pylon structure
FR3039132B1 (fr) * 2015-07-20 2017-08-11 Airbus Operations Sas Ensemble moteur a helice a axe horizontal pour aeronef
FR3050722B1 (fr) * 2016-04-28 2021-07-02 Snecma Ensemble propulsif pour aeronef a berceau filtre
FR3053661B1 (fr) * 2016-07-11 2018-07-13 Safran Aircraft Engines Dispositif de propulsion pour un aeronef, tel par exemple qu'un turbopropulseur
US10479515B2 (en) * 2016-08-10 2019-11-19 Sikorsky Aircraft Corporation Dual mode supplemental strut and damper
FR3061699B1 (fr) * 2017-01-12 2024-02-02 Safran Aircraft Engines Ensemble moteur pour aeronef
US11635024B2 (en) 2019-08-16 2023-04-25 Pratt & Whitney Canada Corp. Pusher turboprop powerplant installation
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
US11674414B2 (en) * 2021-03-19 2023-06-13 Pratt & Whitney Canada Corp. Gas turbine engine and mount assembly therefor
FR3124492A1 (fr) * 2021-06-29 2022-12-30 Airbus Operations (S.A.S.) Ensemble propulseur à hélice et moteur électrique comprenant une structure primaire adaptée et aéronef comportant au moins un tel ensemble propulseur
EP4299445A1 (de) * 2022-06-27 2024-01-03 Airbus Operations (S.A.S.) Elektrische antriebsanordnung mit mindestens zwei unabhängigen trägern, luftfahrzeug mit mindestens einer solchen elektrischen antriebsanordnung

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE21328E (en) * 1940-01-16 stitz
US2145280A (en) * 1936-01-07 1939-01-31 Wilbur E Stitz Engine mounting
US2261954A (en) * 1939-04-15 1941-11-11 Wright Aeronautical Corp Dynamic engine suspension
US2465790A (en) * 1944-05-19 1949-03-29 Lord Mfg Co Mounting for engines for aircraft
US2934332A (en) * 1955-06-14 1960-04-26 Mercier Jean Shock absorber
FR2584373B1 (fr) * 1985-07-03 1990-07-06 Aerospatiale Dispositif de suspension antiresonnante a six degres de liberte pour helicoptere
US5065959A (en) * 1989-11-21 1991-11-19 The Boeing Company Vibration damping aircraft engine attachment
US5197692A (en) * 1991-05-29 1993-03-30 Lord Corporation Adaptive fluid mount
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
PL170036B1 (pl) * 1993-04-28 1996-10-31 Urzadzen Mechanicznych Kamax S Amortyzator elastomerowy PL
GB2303884B (en) * 1995-04-13 1999-07-14 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5918833A (en) * 1997-01-16 1999-07-06 Applied Power Inc. Hydraulic torque restraint system
US6422545B1 (en) * 2001-02-09 2002-07-23 Delphi Technologies, Inc. Vacuum actuated active decoupler mount
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
FR2851226B1 (fr) * 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
GB2407134B (en) * 2003-10-16 2008-04-16 Rolls Royce Plc Aircraft engine mounting assembly
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2862945B1 (fr) * 2003-12-01 2006-04-28 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'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.
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.
JP4938248B2 (ja) * 2005-04-12 2012-05-23 株式会社ブリヂストン 防振装置
FR2939103B1 (fr) * 2008-12-01 2011-01-21 Airbus France Systeme hydraulique de transmission d'efforts entre un turbopropulseur d'aeronef et un dispositif d'accrochage

Also Published As

Publication number Publication date
US20100176239A1 (en) 2010-07-15
US8226028B2 (en) 2012-07-24
FR2916736A1 (fr) 2008-12-05
FR2916736B1 (fr) 2009-09-04
WO2008148722A1 (fr) 2008-12-11
EP2162358B1 (de) 2010-12-01
EP2162358A1 (de) 2010-03-17
ATE490178T1 (de) 2010-12-15

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