FR2894934B1 - Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente - Google Patents

Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente

Info

Publication number
FR2894934B1
FR2894934B1 FR0553896A FR0553896A FR2894934B1 FR 2894934 B1 FR2894934 B1 FR 2894934B1 FR 0553896 A FR0553896 A FR 0553896A FR 0553896 A FR0553896 A FR 0553896A FR 2894934 B1 FR2894934 B1 FR 2894934B1
Authority
FR
France
Prior art keywords
waiting
manility
spring
rear axle
aircraft engine
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
FR0553896A
Other languages
English (en)
Other versions
FR2894934A1 (fr
Inventor
Noel Virginie Audart
Stephane Levert
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 FR0553896A priority Critical patent/FR2894934B1/fr
Priority to US11/608,971 priority patent/US7942580B2/en
Publication of FR2894934A1 publication Critical patent/FR2894934A1/fr
Application granted granted Critical
Publication of FR2894934B1 publication Critical patent/FR2894934B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F16C11/0614—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints the female part of the joint being open on two sides
    • B64D27/40—
    • B64D27/404—
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/02—Sliding-contact bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Springs (AREA)
  • Vibration Prevention Devices (AREA)
  • Pivots And Pivotal Connections (AREA)
FR0553896A 2005-12-15 2005-12-15 Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente Active FR2894934B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0553896A FR2894934B1 (fr) 2005-12-15 2005-12-15 Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente
US11/608,971 US7942580B2 (en) 2005-12-15 2006-12-11 Rear suspension for an aircraft engine with shackle in waiting and spring for such a hinge pin in waiting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0553896A FR2894934B1 (fr) 2005-12-15 2005-12-15 Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente

Publications (2)

Publication Number Publication Date
FR2894934A1 FR2894934A1 (fr) 2007-06-22
FR2894934B1 true FR2894934B1 (fr) 2009-11-13

Family

ID=36917403

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0553896A Active FR2894934B1 (fr) 2005-12-15 2005-12-15 Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente

Country Status (2)

Country Link
US (1) US7942580B2 (fr)
FR (1) FR2894934B1 (fr)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
FR2891253B1 (fr) 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
WO2008150202A1 (fr) * 2007-06-08 2008-12-11 Volvo Aero Corporation Structure de transfert de charges au niveau d'une turbine à gaz, et turbine et aéronef comportant une telle structure
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
FR2926536B1 (fr) * 2008-01-23 2010-07-30 Snecma Accrochage d'un systeme propulsif a un element de structure d'un aeronef
GB2459483B (en) * 2008-04-24 2010-06-30 Rolls Royce Plc Engine mounting arrangement
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
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
US8075024B2 (en) * 2008-06-30 2011-12-13 Eaton Corporation Coupling assembly
US8991191B2 (en) * 2009-11-24 2015-03-31 General Electric Company Thermally actuated passive gas turbine engine compartment venting
US9227734B2 (en) * 2012-08-31 2016-01-05 United Technologies Corporation Secondary load path for gas turbine engine
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
FR3001713B1 (fr) * 2013-02-05 2016-07-15 Astrium Sas Dispositif de retenue d'un reservoir dans un aeronef
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
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
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
EP3024729B1 (fr) 2013-07-26 2022-04-27 MRA Systems, LLC Mât d'accrochage de moteur pour aéronef
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
US10371047B2 (en) 2013-10-16 2019-08-06 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
FR3021373B1 (fr) * 2014-05-21 2016-12-09 Snecma Dispositif d'articulation a rotule pour une turbomachine.
FR3026137B1 (fr) * 2014-09-22 2019-03-15 Safran Aircraft Engines Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion
EP3242834B1 (fr) * 2015-01-07 2018-11-28 LORD Corporation Bâti-moteur d'aéronef
US10029801B2 (en) * 2015-08-17 2018-07-24 The Boeing Company AFT engine mounting link rotational stop collar
US10351224B2 (en) * 2015-09-23 2019-07-16 The Boeing Company External structure mounting system for use with an aircraft
FR3044297B1 (fr) * 2015-11-27 2017-12-22 Airbus Operations Sas Ensemble moteur pour aeronef comprenant des attaches moteur arriere sous forme de manilles
US10066552B2 (en) * 2016-03-14 2018-09-04 Hamilton Sundstrand Corporation One degree-of-constraint semi-fusible gearbox mounting link
US10006373B2 (en) * 2016-03-14 2018-06-26 Hamilton Sundstrand Coporation Two degree-of-constraint semi-fusible gearbox mounting link
FR3061480B1 (fr) * 2016-12-30 2019-05-31 Airbus Operations Ensemble moteur pour aeronef comprenant une attache moteur avant facilitant son montage
FR3062439B1 (fr) 2017-02-02 2019-03-15 Safran Transmission Systems Chape de turbomachine a filtre integre et son procede de realisation
USD880279S1 (en) * 2017-12-11 2020-04-07 Marchesan Implementos E Maquinas Agricolas Tatu S.A. Support bracket
FR3093546B1 (fr) * 2019-03-05 2021-04-23 Airbus Operations Sas Liaison de sécurité d’une attache moteur d’un ensemble propulsif aéronef et ensemble propulsif d’aéronef équipé d’une telle liaison de sécurité
FR3093995A1 (fr) * 2019-03-18 2020-09-25 Airbus Operations (S.A.S.) Attache moteur arrière d’un aéronef présentant un encombrement réduit en largeur et aéronef comprenant au moins une telle attache moteur arrière
US11479104B2 (en) 2019-07-24 2022-10-25 Honeywell International Inc. System and method for gas turbine engine mount with seal
FR3103465A1 (fr) * 2019-11-27 2021-05-28 Airbus Operations Systeme d’attache moteur avant pour un moteur d’aeronef qui comporte une structure allegee

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE366582C (de) * 1923-01-08 Karl Schmitz Federndes Lager
US323709A (en) * 1885-08-04 Automatic swinging chair
US300433A (en) * 1884-06-17 Electric-arc lamp
GB366582A (en) 1930-11-07 1932-02-08 United Gas Industries Ltd Improvements relating to counters applicable to meters and other purposes
FR2169469A5 (fr) * 1972-01-26 1973-09-07 Peugeot & Renault
DE2630205A1 (de) * 1976-07-05 1978-01-19 Hurth Masch Zahnrad Carl Kippzapfen fuer gelenke, insbesondere kardangelenke o.dgl.
DE2758741A1 (de) * 1977-12-29 1979-07-12 Horst Ing Grad Taraschewsky Buchse mit federzungen
US4313331A (en) * 1978-06-02 1982-02-02 Nycoil Company Method of manufacturing a metallic retaining ring for a tube
US4682900A (en) * 1985-12-19 1987-07-28 The Garrett Corporation Thrust bearing underspring
GB2224707B (en) * 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity
DE4010466A1 (de) * 1990-03-31 1991-10-02 Bayerische Motoren Werke Ag Lagerung mindestens zweier relativ zueinander verschwenkbarer teile
JP2932041B2 (ja) * 1994-07-18 1999-08-09 大同メタル工業株式会社 ブッシュ
DE19508418C2 (de) * 1995-03-09 1997-12-18 Glyco Metall Werke Gerollte Lagerbuchse für Zapfen oder Wellen
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
USD517900S1 (en) * 2002-04-04 2006-03-28 420820 Ontario Limited Bushing
FR2887853B1 (fr) 2005-06-29 2007-08-17 Airbus France Sas Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage

Also Published As

Publication number Publication date
US7942580B2 (en) 2011-05-17
FR2894934A1 (fr) 2007-06-22
US20070138337A1 (en) 2007-06-21

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