FR2900906B1 - Systeme de fixation tolerant aux dommages pour moteur d'aeronef - Google Patents

Systeme de fixation tolerant aux dommages pour moteur d'aeronef

Info

Publication number
FR2900906B1
FR2900906B1 FR0604080A FR0604080A FR2900906B1 FR 2900906 B1 FR2900906 B1 FR 2900906B1 FR 0604080 A FR0604080 A FR 0604080A FR 0604080 A FR0604080 A FR 0604080A FR 2900906 B1 FR2900906 B1 FR 2900906B1
Authority
FR
France
Prior art keywords
tolerant
aircraft engine
fixing system
damage fixing
damage
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 - Fee Related
Application number
FR0604080A
Other languages
English (en)
Other versions
FR2900906A1 (fr
Inventor
Herve Marche
Gilles Weyland
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
Priority to FR0604080A priority Critical patent/FR2900906B1/fr
Priority to US11/745,032 priority patent/US8328132B2/en
Publication of FR2900906A1 publication Critical patent/FR2900906A1/fr
Application granted granted Critical
Publication of FR2900906B1 publication Critical patent/FR2900906B1/fr
Expired - Fee Related 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
    • B64D27/02—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
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0604080A 2006-05-09 2006-05-09 Systeme de fixation tolerant aux dommages pour moteur d'aeronef Expired - Fee Related FR2900906B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0604080A FR2900906B1 (fr) 2006-05-09 2006-05-09 Systeme de fixation tolerant aux dommages pour moteur d'aeronef
US11/745,032 US8328132B2 (en) 2006-05-09 2007-05-07 Damage-tolerant attachment system for an aircraft engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0604080A FR2900906B1 (fr) 2006-05-09 2006-05-09 Systeme de fixation tolerant aux dommages pour moteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2900906A1 FR2900906A1 (fr) 2007-11-16
FR2900906B1 true FR2900906B1 (fr) 2009-01-09

Family

ID=37605787

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0604080A Expired - Fee Related FR2900906B1 (fr) 2006-05-09 2006-05-09 Systeme de fixation tolerant aux dommages pour moteur d'aeronef

Country Status (2)

Country Link
US (1) US8328132B2 (fr)
FR (1) FR2900906B1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2939100B1 (fr) * 2008-12-01 2010-12-31 Airbus France Ensemble moteur pour aeronef comprenant une structure rigide modulaire de mat d'accrochage
WO2010085360A2 (fr) 2009-01-26 2010-07-29 Lord Corporation Système et procédé de montage de moteurs d'aéronef
FR2989952B1 (fr) * 2012-04-27 2014-04-18 Aircelle Sa Nacelle de turboreacteur a section aval
EP3049657B1 (fr) * 2013-09-27 2018-10-03 United Technologies Corporation Systèmes de montage pour moteurs à turbine à gaz
FR3016608B1 (fr) * 2014-01-21 2016-02-26 Airbus Operations Sas Attache moteur pour aeronef.
FR3039132B1 (fr) * 2015-07-20 2017-08-11 Airbus Operations Sas Ensemble moteur a helice a axe horizontal pour aeronef
FR3058704B1 (fr) * 2016-11-14 2018-11-16 Safran Aircraft Engines Berceau bipartite a coulissement pour turbopropulseur
FR3062439B1 (fr) * 2017-02-02 2019-03-15 Safran Transmission Systems Chape de turbomachine a filtre integre et son procede de realisation
US10414509B2 (en) * 2017-02-23 2019-09-17 United Technologies Corporation Propulsor mounting for advanced body aircraft
US10814995B2 (en) * 2017-08-29 2020-10-27 Spirit Aerosystems, Inc. High-mounted aircraft nacelle
US11306681B2 (en) * 2019-01-15 2022-04-19 The Boeing Company Sheared exhaust nozzle
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3208217A (en) * 1964-08-28 1965-09-28 Gen Electric Turbine engine and gearbox mounting arrangement
GB1397068A (en) * 1971-06-24 1975-06-11 Hawker Siddeley Aviation Ltd Aircraft
GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust 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
US6170780B1 (en) * 1997-07-21 2001-01-09 Sam Barlow Williams Twin engine aircraft
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount
FR2770486B1 (fr) * 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
FR2806699B1 (fr) * 2000-03-22 2002-05-10 Aerospatiale Matra Airbus Dispositif de reprise de poussee apte a relier un turbomoteur et un mat d'aeronef
US6296203B1 (en) * 2000-05-24 2001-10-02 General Electric Company Snubber thrust mount
FR2820402B1 (fr) * 2001-02-08 2003-05-02 Eads Airbus Sa Dispositif d'accrochage d'un moteur sur un aeronef
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
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
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion

Also Published As

Publication number Publication date
FR2900906A1 (fr) 2007-11-16
US8328132B2 (en) 2012-12-11
US20080121754A1 (en) 2008-05-29

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

ST Notification of lapse

Effective date: 20210105