ATE538032T1 - Sicherungsplatte und längliches griffelement für eine einteilige flugzeugantriebseinheit - Google Patents

Sicherungsplatte und längliches griffelement für eine einteilige flugzeugantriebseinheit

Info

Publication number
ATE538032T1
ATE538032T1 AT08805630T AT08805630T ATE538032T1 AT E538032 T1 ATE538032 T1 AT E538032T1 AT 08805630 T AT08805630 T AT 08805630T AT 08805630 T AT08805630 T AT 08805630T AT E538032 T1 ATE538032 T1 AT E538032T1
Authority
AT
Austria
Prior art keywords
power unit
plate
locking plate
securing
handle element
Prior art date
Application number
AT08805630T
Other languages
English (en)
Inventor
Guy Vauchel
Nicolas Hillereau
Jerome Collier
Jean-Francois Cribelier
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 ATE538032T1 publication Critical patent/ATE538032T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Connection Of Plates (AREA)
  • Wind Motors (AREA)
  • Toys (AREA)
  • Manipulator (AREA)
AT08805630T 2007-06-22 2008-06-02 Sicherungsplatte und längliches griffelement für eine einteilige flugzeugantriebseinheit ATE538032T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0704495A FR2917710A1 (fr) 2007-06-22 2007-06-22 Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef
PCT/FR2008/000740 WO2009007520A2 (fr) 2007-06-22 2008-06-02 Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef

Publications (1)

Publication Number Publication Date
ATE538032T1 true ATE538032T1 (de) 2012-01-15

Family

ID=38983328

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08805630T ATE538032T1 (de) 2007-06-22 2008-06-02 Sicherungsplatte und längliches griffelement für eine einteilige flugzeugantriebseinheit

Country Status (10)

Country Link
US (1) US9156566B2 (de)
EP (1) EP2160328B1 (de)
CN (1) CN101801787B (de)
AT (1) ATE538032T1 (de)
BR (1) BRPI0812806A2 (de)
CA (1) CA2688301A1 (de)
ES (1) ES2378860T3 (de)
FR (1) FR2917710A1 (de)
RU (1) RU2469918C2 (de)
WO (1) WO2009007520A2 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2920408B1 (fr) * 2007-08-30 2010-02-19 Snecma Pylone de suspension d'un moteur sous une aile d'avion
FR2955311B1 (fr) * 2010-01-15 2012-03-23 Airbus Operations Sas Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef
US9211955B1 (en) * 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
US10295970B2 (en) 2013-07-29 2019-05-21 C Series Aircraft Limited Partnership Method for attachment of a pre-assembled powerplant and pylon assembly to an aircraft
US9738391B2 (en) * 2014-03-10 2017-08-22 United Technologies Corporation Engine installation system
FR3020343B1 (fr) 2014-04-23 2017-10-27 Airbus Operations Sas Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage constituee par trois elements independants
US9783313B2 (en) 2015-06-23 2017-10-10 Rohr, Inc. Installing or removing aircraft engines
RU2630565C2 (ru) * 2015-12-28 2017-09-11 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Устройство соединения разделяемых элементов летательного аппарата
FR3075886B1 (fr) 2017-12-22 2019-12-27 Safran Nacelles Nacelle de turboreacteur comportant des ouvertures de capots avant d'acces a des points de fixation de la nacelle
FR3078058B1 (fr) * 2018-02-20 2022-03-25 Safran Nacelles Ensemble de motorisation pour aeronef comportant des points de levage, et chariots pour supporter un tel ensemble
GB201808514D0 (en) * 2018-05-24 2018-07-11 Rolls Royce Plc Mounting System and Mounting Method for Gas Turbine Aero Engine
GB201808515D0 (en) * 2018-05-24 2018-07-11 Rolls Royce Plc Mounting System and Mounting Method for Gas Turbine Aero Engine
FR3085710B1 (fr) * 2018-09-12 2020-09-11 Safran Aircraft Engines Interface de support amovible pour carter annulaire de turbomachine
CN109455304B (zh) * 2018-11-30 2024-02-23 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞机静不定吊挂结构

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
RU2009083C1 (ru) * 1991-05-23 1994-03-15 Авиационный комплекс им.С.В.Ильюшина Силовая установка летательного аппарата
GB9116986D0 (en) * 1991-08-07 1991-10-09 Rolls Royce Plc Gas turbine engine nacelle assembly
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
FR2755944B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2755942B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2755943B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2873988B1 (fr) * 2004-08-05 2007-12-21 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2878229B1 (fr) * 2004-11-23 2008-04-18 Airbus France Sas Systeme de fixation d'un mat de moteur a l'aile d'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
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
GB0507721D0 (en) * 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
FR2891251B1 (fr) * 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2905990A1 (fr) * 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
US9302785B2 (en) * 2007-11-29 2016-04-05 The Boeing Company Engine installation using machine vision for alignment
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
GB0810791D0 (en) * 2008-06-13 2008-07-23 Rolls Royce Plc Thrust mounting arrangement
FR2934565B1 (fr) * 2008-08-04 2010-09-17 Airbus France Systeme d'attache d'un moteur sur une structure d'un aeronef tel qu'une aile volante.
FR2934563B1 (fr) * 2008-08-04 2010-09-10 Airbus France Aile volante comportant un moteur monte sur un mat.
FR2983836B1 (fr) * 2011-12-08 2014-12-19 Airbus Operations Sas Outillage d'aide a la construction et a la maintenance des aeronefs

Also Published As

Publication number Publication date
US9156566B2 (en) 2015-10-13
EP2160328A2 (de) 2010-03-10
FR2917710A1 (fr) 2008-12-26
ES2378860T3 (es) 2012-04-18
CN101801787A (zh) 2010-08-11
BRPI0812806A2 (pt) 2014-12-09
RU2469918C2 (ru) 2012-12-20
WO2009007520A3 (fr) 2010-05-20
WO2009007520A2 (fr) 2009-01-15
US20100181418A1 (en) 2010-07-22
CN101801787B (zh) 2014-10-29
RU2009147806A (ru) 2011-07-27
EP2160328B1 (de) 2011-12-21
CA2688301A1 (fr) 2009-01-15

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