ES2174507T3 - Dispositivo de enganche de un motor sobre un aeronave. - Google Patents

Dispositivo de enganche de un motor sobre un aeronave.

Info

Publication number
ES2174507T3
ES2174507T3 ES98954527T ES98954527T ES2174507T3 ES 2174507 T3 ES2174507 T3 ES 2174507T3 ES 98954527 T ES98954527 T ES 98954527T ES 98954527 T ES98954527 T ES 98954527T ES 2174507 T3 ES2174507 T3 ES 2174507T3
Authority
ES
Spain
Prior art keywords
mastil
hitch structure
engine
aircraft
hardware
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.)
Expired - Lifetime
Application number
ES98954527T
Other languages
English (en)
Inventor
Blaye Sebastien Le
Marc Canadas
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2174507T3 publication Critical patent/ES2174507T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Lock And Its Accessories (AREA)
  • Connection Of Plates (AREA)
  • Toys (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

UN DISPOSITIVO DE ACOPLAMIENTO DE UN MOTOR EN UN MASTIL (10) DE UNA AERONAVE COMPRENDE UNA ESTRUCTURA DE ENGANCHE PRINCIPAL Y UNA ESTRUCTURA DE ENGANCHE AUXILIAR (52). LA ESTRUCTURA DE ENGANCHE PRINCIPAL INCLUYE UN HERRAJE (1) FIJADO AL MASTIL (10) ASI COMO AL MENOS DOS BIELAS CON ROTULA (18, 20) QUE CONECTAN EL HERRAJE (16) AL MOTOR. LA ESTRUCTURA DE ENGANCHE AUXILIAR (52), POR LA QUE NO PASA NINGUN ESFUERZO CUANDO LA ESTRUCTURA DE ENGANCHE PRINCIPAL ESTA EN ESTADO OPERATIVO, CONECTA DIRECTAMENTE, CON JUEGO, EL MASTIL (10) AL MOTOR. ESTA COMPRENDE, POR EJEMPLO, UNA BRIDA (54) SOLIDARIA AL MASTIL (10) Y QUE ATRAVIESA UNA VENTANA FORMADA EN EL HERRAJE (16) O UNA BIELA ARTICULADA EN EL MOTOR Y EN EL MASTIL.
ES98954527T 1997-11-06 1998-11-05 Dispositivo de enganche de un motor sobre un aeronave. Expired - Lifetime ES2174507T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9713966A FR2770486B1 (fr) 1997-11-06 1997-11-06 Dispositif d'accrochage d'un moteur sur un aeronef

Publications (1)

Publication Number Publication Date
ES2174507T3 true ES2174507T3 (es) 2002-11-01

Family

ID=9513107

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98954527T Expired - Lifetime ES2174507T3 (es) 1997-11-06 1998-11-05 Dispositivo de enganche de un motor sobre un aeronave.

Country Status (7)

Country Link
US (1) US6059227A (es)
EP (1) EP0948443B1 (es)
CA (1) CA2277016C (es)
DE (1) DE69804758T2 (es)
ES (1) ES2174507T3 (es)
FR (1) FR2770486B1 (es)
WO (1) WO1999024320A1 (es)

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2774358B1 (fr) * 1998-02-04 2000-04-21 Aerospatiale Dispositif d'accrochage d'un moteur d'aeronef
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
GB9927425D0 (en) * 1999-11-20 2000-01-19 Rolls Royce Plc A gas turbine engine mounting arrangement
FR2820402B1 (fr) * 2001-02-08 2003-05-02 Eads Airbus Sa Dispositif d'accrochage d'un moteur sur un aeronef
FR2825976B1 (fr) 2001-06-13 2003-09-05 Eads Airbus Sa Dispositif de reprise d'efforts generes par un moteur d'aeronef
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
FR2830515B1 (fr) * 2001-10-04 2004-01-30 Snecma Moteurs Suspension de turboreacteur
US7179269B2 (en) 2002-05-20 2007-02-20 Scimed Life Systems, Inc. Apparatus and system for removing an obstruction from a lumen
WO2004026689A1 (en) * 2002-09-17 2004-04-01 Bell Helicopter Textron Inc. Torsionally de-coupled engine mount system
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2856656B1 (fr) * 2003-06-30 2006-12-01 Snecma Moteurs Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang
US20050084221A1 (en) * 2003-10-16 2005-04-21 3M Innovative Properties Company Apparatus and method for transitioning fiber optic cables
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
US7526921B2 (en) * 2005-03-29 2009-05-05 Honeywell International Inc. Auxiliary power unit with integral firebox
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
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2887852B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
US20070057128A1 (en) * 2005-09-14 2007-03-15 Honeywell International, Inc. Auxiliary power unit case flange to plate adapter
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
GB0607991D0 (en) 2006-04-22 2006-05-31 Rolls Royce Plc Aeroengine mounting
FR2900906B1 (fr) * 2006-05-09 2009-01-09 Airbus France Sas Systeme de fixation tolerant aux dommages pour moteur d'aeronef
FR2901243B1 (fr) 2006-05-16 2008-06-27 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef
FR2914908B1 (fr) 2007-04-13 2009-10-30 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.
FR2915176B1 (fr) * 2007-04-20 2009-07-10 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet
GB2459483B (en) * 2008-04-24 2010-06-30 Rolls Royce Plc Engine mounting arrangement
DE102008021431A1 (de) * 2008-04-29 2009-11-12 Airbus Deutschland Gmbh Flugzeug mit einer Energie-Versorgungsvorrichtung
FR2931800B1 (fr) * 2008-05-29 2010-07-30 Airbus France Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810585D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
RU2388659C1 (ru) * 2008-11-24 2010-05-10 Государственное предприятие "Запорожское машиностроительное конструкторское бюро "Прогресс" имени академика А.Г. Ивченко Устройство крепления газотурбинного двигателя к летательному аппарату
KR101767071B1 (ko) 2010-06-14 2017-08-10 로오드 코포레이션 헬리콥터 엔진 장착 시스템 및 방법
US8348191B2 (en) 2010-07-14 2013-01-08 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
US8919134B2 (en) * 2011-01-26 2014-12-30 United Technologies Corporation Intershaft seal with support linkage
FR2974065B1 (fr) * 2011-04-14 2013-05-10 Snecma Procede de montage d'un moteur d'aeronef sur un pylone et attache moteur pour la mise en oeuvre d'un tel procede.
US8882029B2 (en) 2011-07-14 2014-11-11 United Technologies Corporation Fire resistant structural mount yoke and system
CN103101628B (zh) * 2013-02-06 2015-05-27 中国商用飞机有限责任公司 一种与飞机吊挂一体化的前安装节
WO2014189588A2 (en) 2013-03-15 2014-11-27 United Technologies Corporation Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
GB201315968D0 (en) 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
EP3242834B1 (en) * 2015-01-07 2018-11-28 LORD Corporation Aircraft engine mount
FR3039204B1 (fr) * 2015-07-24 2017-07-21 Snecma Ensemble de montage d'une turbomachine
FR3089264B1 (fr) * 2018-11-30 2020-11-06 Safran Aircraft Engines Dispositif d’aide a l’alignement de deux organes, de preference pour ensemble moteur d’aeronef, et procede de montage mettant en œuvre un tel dispositif
US11273923B2 (en) * 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
DE69012071T2 (de) * 1989-12-05 1995-04-13 Rolls Royce Plc Ausfallsichere Haltevorrichtung für Treibwerke.
US5275357A (en) 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5620154A (en) 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
FR2755944B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount

Also Published As

Publication number Publication date
EP0948443A1 (fr) 1999-10-13
EP0948443B1 (fr) 2002-04-10
US6059227A (en) 2000-05-09
CA2277016C (en) 2007-01-02
WO1999024320A1 (fr) 1999-05-20
FR2770486A1 (fr) 1999-05-07
FR2770486B1 (fr) 2000-01-28
DE69804758T2 (de) 2002-11-21
DE69804758D1 (de) 2002-05-16
CA2277016A1 (en) 1999-05-20

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