[go: up one dir, main page]

ATE446903T1 - Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur - Google Patents

Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur

Info

Publication number
ATE446903T1
ATE446903T1 AT06763903T AT06763903T ATE446903T1 AT E446903 T1 ATE446903 T1 AT E446903T1 AT 06763903 T AT06763903 T AT 06763903T AT 06763903 T AT06763903 T AT 06763903T AT E446903 T1 ATE446903 T1 AT E446903T1
Authority
AT
Austria
Prior art keywords
engine
pin
engine mount
aircraft
placement
Prior art date
Application number
AT06763903T
Other languages
English (en)
Inventor
Virginie Audart-Noel
Pascal Gardes
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE446903T1 publication Critical patent/ATE446903T1/de

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
    • 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
    • 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
    • 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
    • F16C11/0695—Mounting of ball-joints, e.g. fixing them to a connecting rod
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Vibration Prevention Devices (AREA)
  • Motor Or Generator Frames (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Clamps And Clips (AREA)
  • Combined Devices Of Dampers And Springs (AREA)
AT06763903T 2005-06-29 2006-06-27 Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur ATE446903T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0551821A FR2887853B1 (fr) 2005-06-29 2005-06-29 Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
PCT/EP2006/063602 WO2007000458A1 (fr) 2005-06-29 2006-06-27 Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage

Publications (1)

Publication Number Publication Date
ATE446903T1 true ATE446903T1 (de) 2009-11-15

Family

ID=35708566

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06763903T ATE446903T1 (de) 2005-06-29 2006-06-27 Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur

Country Status (11)

Country Link
US (1) US8740136B2 (de)
EP (1) EP1896326B1 (de)
JP (1) JP5166257B2 (de)
CN (1) CN100500514C (de)
AT (1) ATE446903T1 (de)
BR (1) BRPI0608596A2 (de)
CA (1) CA2613194C (de)
DE (1) DE602006010069D1 (de)
FR (1) FR2887853B1 (de)
RU (1) RU2391259C2 (de)
WO (1) WO2007000458A1 (de)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2894934B1 (fr) 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente
WO2008150202A1 (en) * 2007-06-08 2008-12-11 Volvo Aero Corporation A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure
FR2921341B1 (fr) * 2007-09-25 2010-05-21 Snecma Accrochage d'un turboreacteur sous l'aile d'un aeronef
FR2958267B1 (fr) * 2010-04-02 2012-03-23 Airbus Operations Sas Systeme d'axe pour ensemble de liaison d'un mat-reacteur sous une voilure d'aeronef
FR2975132B1 (fr) * 2011-05-09 2015-06-26 Snecma Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques
US8727269B2 (en) * 2011-06-06 2014-05-20 General Electric Company System and method for mounting an aircraft engine
FR2978730B1 (fr) * 2011-08-03 2013-09-27 Airbus Operations Sas Berceau d'articulation de capots de soufflante supportes par ces capots en position fermee
US8851417B2 (en) 2012-08-07 2014-10-07 United Technologies Corporation Self-retaining shear pin for blind mount location
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
FR3014971B1 (fr) 2013-12-12 2016-01-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
FR3014970B1 (fr) 2013-12-12 2016-01-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
FR3014972B1 (fr) * 2013-12-12 2016-04-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
FR3021373B1 (fr) * 2014-05-21 2016-12-09 Snecma Dispositif d'articulation a rotule pour une turbomachine.
FR3027875A1 (fr) * 2014-10-30 2016-05-06 Airbus Operations Sas Dispositif de fixation d'un moteur d'aeronef, et aeronef correspondant
FR3029504B1 (fr) * 2014-12-09 2018-03-30 Airbus Operations (S.A.S.) Attache moteur avant d'aeronef
EP3242834B1 (de) 2015-01-07 2018-11-28 LORD Corporation Flugzeugtriebwerksaufhängung
FR3041935B1 (fr) * 2015-10-05 2017-12-15 Airbus Operations Sas Ensemble moteur pour aeronef comprenant au moins deux attaches moteur arriere decalees axialement l'une de l'autre
US10570950B2 (en) 2016-05-23 2020-02-25 United Technologies Corporation Spherical joint assembly with a spherical bearing between integral collars
US10598211B2 (en) * 2016-05-23 2020-03-24 United Technologies Corporation Spherical bearing sleeve configured with one or more discrete collars
FR3058127B1 (fr) * 2016-10-28 2022-02-25 Safran Aircraft Engines Assemblage entre un pylone d'aeronef et une turbomachine
FR3058388B1 (fr) * 2016-11-04 2019-05-10 Airbus Operations Attache arriere d'un moteur d'aeronef
US10197213B2 (en) * 2017-01-26 2019-02-05 General Electric Company Systems and methods for mounting a rotatable machine
FR3068008B1 (fr) * 2017-06-21 2019-11-08 Airbus Operations Ensemble de motorisation pour un aeronef
FR3072078B1 (fr) * 2017-10-05 2021-06-11 Airbus Operations Sas Attache moteur arriere pour un moteur d'aeronef
FR3077560B1 (fr) * 2018-02-06 2020-01-10 Airbus Operations Assemblage pour une attache-moteur d'aeronef comprenant un axe d'articulation supporte par une chape et immobile en translation
FR3089954B1 (fr) * 2018-12-12 2021-01-08 Airbus Operations Sas Ensemble de motorisation pour un aeronef comprenant un support de charge
FR3091911A1 (fr) * 2019-01-21 2020-07-24 Airbus Operations (S.A.S.) Dispositif de liaison pivotante entre au moins deux pièces, aéronef comprenant un capot équipé dudit dispositif de liaison pivotante
FR3097836A1 (fr) * 2019-06-25 2021-01-01 Airbus Operations (S.A.S.) Ensemble propulseur d’aéronef comportant une structure primaire de mât et une attache moteur avant améliorées
US11066860B1 (en) * 2020-01-06 2021-07-20 Rohr, Inc. Hinged assembly with fail-safe hinge pin
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
FR3123323B1 (fr) * 2021-05-27 2024-05-03 Safran Aircraft Engines Structure de liaison et de support d’une turbomachine a un pylone d’aeronef
FR3124164A1 (fr) 2021-06-30 2022-12-23 Airbus Operations Manille de fixation d’un moteur d’aeronef comprenant un couple de revetements antifriction encapsules, et aeronef comprenant une telle manille.
EP4477552A1 (de) * 2023-06-14 2024-12-18 Airbus Operations (S.A.S.) Flugzeugantriebsanordnung mit einem strahltriebwerk, einem pylon und mitteln zur befestigung des strahltriebwerks an dem pylon

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2818225A (en) * 1954-03-15 1957-12-31 Rolls Royce Power plant installations for aircraft
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
GB8722021D0 (en) * 1987-09-18 1987-10-28 British Aerospace Lock nut assemblies
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
DE4221250C2 (de) * 1992-07-01 1995-10-05 Daimler Benz Aerospace Airbus Vorrichtung zur Sicherung
US5649417A (en) * 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine 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
US6695557B2 (en) * 2001-09-05 2004-02-24 John Hove Wheel lug nut security seal
US6669393B2 (en) * 2001-10-10 2003-12-30 General Electric Co. Connector assembly for gas turbine engines
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system

Also Published As

Publication number Publication date
JP2008544907A (ja) 2008-12-11
CN101203425A (zh) 2008-06-18
US8740136B2 (en) 2014-06-03
CN100500514C (zh) 2009-06-17
CA2613194A1 (fr) 2007-01-04
WO2007000458A1 (fr) 2007-01-04
DE602006010069D1 (de) 2009-12-10
FR2887853B1 (fr) 2007-08-17
RU2391259C2 (ru) 2010-06-10
JP5166257B2 (ja) 2013-03-21
CA2613194C (fr) 2013-09-24
BRPI0608596A2 (pt) 2010-12-21
US20080156930A1 (en) 2008-07-03
RU2008103266A (ru) 2009-08-10
FR2887853A1 (fr) 2007-01-05
EP1896326A1 (de) 2008-03-12
EP1896326B1 (de) 2009-10-28

Similar Documents

Publication Publication Date Title
ATE446903T1 (de) Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur
ATE535442T1 (de) Flugzeugmotorbefestigungspylon mit einer mit einer tonnenmutter versehenen hinteren motorbefestigung
DE602006004872D1 (de) Triebwerkmontagestruktur für ein flugzeug
BRPI0401809A (pt) Dispositivo de fixação dianteiro de motor de avião
ATE451302T1 (de) Verfahren zur montage eines fugzeugmotors auf einer starren strebenstruktur zur sicherung des motors
ATE510769T1 (de) Vorrichtung zur kupplung eines luftfahrzeugtriebwerks und verfahren zur befestigung eines luftfahrzeugtriebwerks mittels solch einer vorrichtung
DE602008005290D1 (de) Befestigungsvorrichtung für flugzeugtriebwerk und mindestens eine solche vorrichtung enthaltendes flugzeug
ATE457927T1 (de) Halterung fuer flugzeugtriebwerk
ATE520884T1 (de) Befestigungsanordnung für eine abdeckung zur verbesserung der aerodynamischen leistung
DE502006002932D1 (de) Fahrzeugsitzanordnung mit einer elektrischen Verstellung
DE602006017170D1 (de) Leitungsverbindungsanordnung für anlagen in einer flugzeugpassagierkabine
EP1798776A3 (de) Rahmengestell eines Solarzellenmoduls
DE602006004477D1 (de) Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug
RU2010144797A (ru) Потолочная панель для облицовки внутреннего помещения транспортных средств
DE602008003807D1 (de) Befestigungsvorrichtung für flugzeugturbomotor mit hydraulischen fixiermitteln
DE602007010948D1 (de) Rahmenelement, montagesystem für flugzeugkomponenten und verfahren für den einbau einer komponente in ein flugzeug
GB2493948B (en) Tower section alignment apparatus and system
ATE503146T1 (de) Luftfederanordnung mit einer verbindung ohne gewinde
GB2507218A (en) Connection fixture
ATE423729T1 (de) Triebwerkanordnung für flugzeug
GB2559018B (en) Assembly for an aircraft comprising an engine of the "open rotor puller" type and means for attaching the latter to the rigid structure of an attachment pylon
ATE416975T1 (de) Flugzeugmotoreinheit
TR200807900T2 (tr) Taşıt sileceği için adaptör
BR112014020258A8 (pt) Método para conectar uma primeira peça do fixador e uma segunda peça do fixador de um conjunto de primeira e segunda peças do fixador em um furo de fixação através de uma parede de uma estrutura, e aparelho para posicionar uma primeira peça do fixador de um conjunto fixador de primeira e segunda peças dentro de uma estrutura e um furo de fixador através de uma parede da estrutura
ATE541783T1 (de) Durch mindestens ein sperrelement unter druckbelastung mit dem rumpf verbundenes heckteil eines flugzeugs mit einer struktur zur abstützung von triebwerken

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties