BR112012014323A2 - sistema de motorização de uma roda associada à uma suspensão - Google Patents

sistema de motorização de uma roda associada à uma suspensão

Info

Publication number
BR112012014323A2
BR112012014323A2 BR112012014323A BR112012014323A BR112012014323A2 BR 112012014323 A2 BR112012014323 A2 BR 112012014323A2 BR 112012014323 A BR112012014323 A BR 112012014323A BR 112012014323 A BR112012014323 A BR 112012014323A BR 112012014323 A2 BR112012014323 A2 BR 112012014323A2
Authority
BR
Brazil
Prior art keywords
suspension
drive system
wheel drive
system associated
wheel
Prior art date
Application number
BR112012014323A
Other languages
English (en)
Inventor
Cesare Stacchi
Olivier Essinger
Original Assignee
Michelin & Cie
Michelin Rech Tech
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 Michelin & Cie, Michelin Rech Tech filed Critical Michelin & Cie
Publication of BR112012014323A2 publication Critical patent/BR112012014323A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405Powered wheels, e.g. for taxing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/80Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Arrangement Of Transmissions (AREA)
  • Vehicle Body Suspensions (AREA)
  • Gear Transmission (AREA)
  • One-Way And Automatic Clutches, And Combinations Of Different Clutches (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

sistema de motorização de uma roda associada à uma suspensão. a invenção refere-se a um sistema de motorização de uma roda (5) associado à uma suspensão, o sistema compreendendo um bloco de motor (3) e um elemento de acionamento (4) integralizado com a roda (5). de acordo com a invenção, o bloco do motor é fixado à parte suspensa do suporte da suspenssão (2) e um dispositivo de embreagem (6) que liga o eixo de saida (7) do bloco do motor (3) ao elemento de acionamento (4).
BR112012014323A 2009-12-17 2010-12-17 sistema de motorização de uma roda associada à uma suspensão BR112012014323A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0959143A FR2954234B1 (fr) 2009-12-17 2009-12-17 Systeme de motorisation d'une roue associee a une suspension
PCT/FR2010/052780 WO2011073587A1 (fr) 2009-12-17 2010-12-17 Systeme de motorisation d'une roue associee a une suspension

Publications (1)

Publication Number Publication Date
BR112012014323A2 true BR112012014323A2 (pt) 2016-07-05

Family

ID=42320795

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012014323A BR112012014323A2 (pt) 2009-12-17 2010-12-17 sistema de motorização de uma roda associada à uma suspensão

Country Status (7)

Country Link
US (1) US9169004B2 (pt)
EP (5) EP2537751B1 (pt)
JP (4) JP5866525B2 (pt)
CN (1) CN102656086B (pt)
BR (1) BR112012014323A2 (pt)
FR (1) FR2954234B1 (pt)
WO (1) WO2011073587A1 (pt)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0915009D0 (en) 2009-08-28 2009-09-30 Airbus Operations Ltd Aircraft landing gear
WO2012134701A2 (en) * 2011-03-01 2012-10-04 Borealis Technical Limited Method of reducing fuel carried by an aircraft in flight
EP2720942B1 (en) * 2011-06-17 2015-05-20 L-3 Communications Magnet-Motor GmbH Drive unit for aircraft landing gear wheels
US20130112805A1 (en) * 2011-07-06 2013-05-09 Borealis Technical Limited Method for reducing requirements for aircraft brake size, complexity, and heat dissipation
GB201214198D0 (en) * 2012-08-08 2012-09-19 Airbus Uk Ltd Landing gear drive system
FR2998870B1 (fr) 2012-12-03 2015-01-09 Michelin & Cie Systeme de motorisation de roue, notamment d'un aeronef
FR2998859B1 (fr) * 2012-12-05 2014-11-21 Michelin & Cie Dispositif d'assistance electrique pour velo et velo a assistance electrique equipe dudit dispositif
FR2998858B1 (fr) 2012-12-05 2014-11-21 Michelin & Cie Dispositif d'assistance electrique pour velo et velo a assistance electrique equipe dudit dispositif
US20140187370A1 (en) * 2012-12-31 2014-07-03 Goodrich Corporation Landing gear wheel drive system
US9139291B2 (en) * 2013-05-28 2015-09-22 Hamilton Sundstrand Corporation Integrated hydrostatic transmission for electronic taxiing operations
FR3008956B1 (fr) * 2013-07-26 2018-05-04 Safran Landing Systems Dispositif d'entrainement en rotation d'une roue d'aeronef
FR3009277B1 (fr) * 2013-08-02 2017-11-03 Messier Bugatti Dowty Atterrisseur d'aeronef muni d'un organe d'entrainement des roues.
CN107719650A (zh) * 2013-09-05 2018-02-23 空中客车英国运营有限责任公司 用于飞行器的起落架的驱动系统
US10676178B2 (en) 2013-09-05 2020-06-09 Airbus Operations Limited Landing gear drive system flexible interface
GB2518604A (en) * 2013-09-18 2015-04-01 Airbus Operations Ltd Drive system for aircraft landing gear
GB2518605B (en) * 2013-09-18 2020-02-12 Airbus Operations Ltd Drive system for landing gear
FR3011531B1 (fr) * 2013-10-04 2017-04-21 Messier Bugatti Dowty Atterrisseur d'aeronef equipe de moyens d'entrainement en rotation des roues portees par l'atterrisseur
US9422053B2 (en) 2013-10-09 2016-08-23 Hamilton Sundstrand Corporation Passive fail safe coupling mechanism
FR3013327B1 (fr) * 2013-11-15 2015-12-25 Messier Bugatti Dowty Roue d'aeronef equipee de moyens de son entrainement en rotation par un actionneur d'entrainement.
US20150210384A1 (en) * 2014-01-24 2015-07-30 Honeywell International Inc. Aircraft wheel driving system
GB2524762B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
FR3022858B1 (fr) * 2014-06-30 2018-01-05 Compagnie Generale Des Etablissements Michelin Systeme de motorisation de roue, notamment d'un aeronef
FR3022859B1 (fr) * 2014-06-30 2018-01-05 Compagnie Generale Des Etablissements Michelin Systeme de motorisation de roue, notamment d'un aeronef
GB2528966A (en) 2014-08-07 2016-02-10 Airbus Operations Ltd Landing gear drive system
GB2558863B (en) * 2014-11-30 2021-03-03 Borealis Tech Ltd Monitoring system for aircraft drive wheel system
FR3031960B1 (fr) * 2015-01-23 2017-02-10 Messier Bugatti Dowty Procede d'entrainement en rotation d'une roue d'aeronef.
FR3031963B1 (fr) * 2015-01-23 2020-02-28 Safran Landing Systems Procede d'entrainement en rotation d'une roue d'aeronef.
GB2543606B (en) * 2015-07-26 2019-01-09 Borealis Tech Ltd Powered clutch assembly for aircraft wheel drive system
FR3048954B1 (fr) * 2016-03-21 2019-08-23 Safran Landing Systems Systeme de desengagement verrouillable d’actionneur de roue sur un atterisseur d’aeronef.
CN108128141B (zh) * 2017-08-28 2020-11-17 北京理工大学 一种电动轮的力传递方法及使用该方法的车辆
FR3082825B1 (fr) 2018-06-26 2020-09-04 Safran Landing Systems Mecanisme de verrouillage d’actionneur de roue
FR3087513B1 (fr) * 2018-10-17 2022-08-26 Safran Trans Systems Reducteur compact pour un dispositif de taxiage d'un aeronef
KR102674559B1 (ko) * 2022-03-29 2024-06-13 현대자동차주식회사 유니버설 휠 구동 시스템
KR102674555B1 (ko) * 2022-03-29 2024-06-13 현대자동차주식회사 유니버설 구동 장치
KR102674558B1 (ko) * 2022-03-29 2024-06-13 현대자동차주식회사 유니버설 휠 구동 시스템

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2320547A (en) * 1942-01-30 1943-06-01 Roy L Tiger Landing wheel rotating device for airplanes
GB1370090A (en) * 1970-12-23 1974-10-09 Rotax Ltd Aircraft having a ground propulsion system
US3762670A (en) * 1971-12-16 1973-10-02 Curtiss Wright Corp Landing gear wheel drive system for aircraft
US3850389A (en) * 1973-05-04 1974-11-26 D Dixon Landing gear wheel device for aircraft
US3874619A (en) 1974-05-03 1975-04-01 Boeing Co Reciprocating powered wheel drive
US3977631A (en) * 1975-06-04 1976-08-31 The Boeing Company Aircraft wheel drive apparatus and method
GB8724123D0 (en) * 1987-10-14 1987-11-18 Balloch J Variable speed aircraft landing wheels
GB2323345A (en) 1998-07-08 1998-09-23 Kate Elizabeth May Rotating aircraft wheels prior to landing
US20030233900A1 (en) 2002-04-26 2003-12-25 Olympus Optical Co., Ltd. Rotary transmission device
JP2004068964A (ja) 2002-08-08 2004-03-04 Olympus Corp 歯車機構
JP4245438B2 (ja) * 2003-08-08 2009-03-25 シャープ株式会社 炭素薄膜ならびにそれを用いた電界放出電子源および作用電極
US20070158497A1 (en) * 2003-10-09 2007-07-12 Edelson Jonathan S Geared wheel motor design
JP4442315B2 (ja) * 2004-05-18 2010-03-31 トヨタ自動車株式会社 電動輪
US7445178B2 (en) * 2004-09-28 2008-11-04 The Boeing Company Powered nose aircraft wheel system
FR2903072B1 (fr) 2006-06-28 2009-11-20 Airbus France Dispositif pour le deplacement autonome d'un aeronef au sol
US8220740B2 (en) 2007-11-06 2012-07-17 Borealis Technical Limited Motor for driving aircraft, located adjacent to undercarriage wheel
DE102008006295B4 (de) * 2008-01-28 2018-05-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Angetriebenes flugzeugfahrwerk
DE102008011791B4 (de) * 2008-02-29 2013-09-19 Airbus Operations Gmbh Integriertes multifunktionales Radantriebssystem für Luftfahrzeuge
FR2939099B1 (fr) * 2008-12-02 2012-06-22 Messier Dowty Sa Dispositif electromecanique multifonctions pour atterrisseur
GB0915009D0 (en) * 2009-08-28 2009-09-30 Airbus Operations Ltd Aircraft landing gear
EP2563657B1 (en) 2010-04-28 2016-09-21 L-3 Communications Magnet-Motor GmbH Drive unit for aircraft running gear

Also Published As

Publication number Publication date
JP5866525B2 (ja) 2016-02-17
EP2512917A1 (fr) 2012-10-24
CN102656086B (zh) 2015-07-15
EP2537751A1 (fr) 2012-12-26
EP3034397B1 (fr) 2020-04-29
JP2016047720A (ja) 2016-04-07
FR2954234B1 (fr) 2012-03-02
EP2537751B1 (fr) 2014-05-14
US20120217340A1 (en) 2012-08-30
EP2537749A1 (fr) 2012-12-26
FR2954234A1 (fr) 2011-06-24
EP2512917B1 (fr) 2016-03-16
WO2011073587A1 (fr) 2011-06-23
US9169004B2 (en) 2015-10-27
EP2537750B1 (fr) 2014-05-14
CN102656086A (zh) 2012-09-05
JP6169144B2 (ja) 2017-07-26
JP2019073286A (ja) 2019-05-16
JP2013514228A (ja) 2013-04-25
JP6470798B2 (ja) 2019-02-13
EP2537749B1 (fr) 2014-05-14
EP2537750A1 (fr) 2012-12-26
JP2017159906A (ja) 2017-09-14
EP3034397A1 (fr) 2016-06-22

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN (FR

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B15K Others concerning applications: alteration of classification

Free format text: A CLASSIFICACAO ANTERIOR ERA: B64C 25/40

Ipc: B64C 25/36 (2006.01), B60K 7/00 (2006.01), B60K 17

B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B25L Entry of change of name and/or headquarter and transfer of application, patent and certificate of addition of invention: publication cancelled

Owner name: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN (FR) ; MICHELIN RECHERCHE ET TECHNIQUE S.A. (CH)

Free format text: ANULADA A PUBLICACAO CODIGO 25.1 NA RPI NO 2452 DE 02/01/2018 POR TER SIDO INDEVIDA.

B25A Requested transfer of rights approved

Owner name: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN (FR) ; MICHELIN RECHERCHE ET TECHNIQUE S.A. (CH) ; AIRBUS OPERATIONS LIMITED (GB)

B25A Requested transfer of rights approved

Owner name: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN (FR) ; AIRBUS OPERATIONS LIMITED (GB)

B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements
B350 Update of information on the portal [chapter 15.35 patent gazette]