MX354164B - Sistemas de accionamiento de tren de aterrizaje. - Google Patents

Sistemas de accionamiento de tren de aterrizaje.

Info

Publication number
MX354164B
MX354164B MX2015001734A MX2015001734A MX354164B MX 354164 B MX354164 B MX 354164B MX 2015001734 A MX2015001734 A MX 2015001734A MX 2015001734 A MX2015001734 A MX 2015001734A MX 354164 B MX354164 B MX 354164B
Authority
MX
Mexico
Prior art keywords
drive
driven gear
drive pinion
pinion
path
Prior art date
Application number
MX2015001734A
Other languages
English (en)
Other versions
MX2015001734A (es
Inventor
Didey Arnaud
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Publication of MX2015001734A publication Critical patent/MX2015001734A/es
Publication of MX354164B publication Critical patent/MX354164B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • 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
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/04—Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members
    • F16H1/06—Toothed gearings for conveying rotary motion without gears having orbital motion involving only two intermeshing members with parallel axes
    • 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
    • F16H—GEARING
    • F16H55/00—Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
    • F16H55/02—Toothed members; Worms
    • F16H55/10—Constructively simple tooth shapes, e.g. shaped as pins, as balls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/40—Alighting gear characterised by elements which contact the ground or similar surface  the elements being rotated before touch-down
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • 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
    • Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/19—Gearing
    • Y10T74/19642—Directly cooperating gears
    • Y10T74/19679—Spur
    • Y10T74/19684—Motor and gearing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gear Transmission (AREA)
  • Transmission Devices (AREA)
  • Gears, Cams (AREA)

Abstract

La presente invención proporciona sistemas de accionamiento para girar una o más ruedas (16) de un tren de aterrizaje (10) de una aeronave con el propósito del desplazamiento en tierra y/o el giro antes del aterrizaje. Un primer aspecto proporciona un sistema de accionamiento para girar la rueda (16) de un tren de aterrizaje (10) de la aeronave, el sistema de accionamiento incluye un motor (52) que opera para accionar el primer piñón de accionamiento a través de la primera trayectoria de accionamiento, y un engrane (20) de accionamiento adaptado para quedar fijo con la rueda (16). El sistema de accionamiento tiene una primera configuración en donde el primer piñón de accionamiento tiene la capacidad de intercalarse con el engrane (20) de accionamiento para permitir que el motor (52) accione el engrane (20) de accionamiento a través de la primera trayectoria de accionamiento. Uno del primer piñón de accionamiento y el engrane (20) de accionamiento comprende una primera rueda dentada (60) y el otro del primer piñón de accionamiento y el engrane de accionamiento comprende una serie de rodillos (36) dispuestos para formar un anillo, cada rodillo (36) puede girar alrededor de un eje de rodillo a una distancia fija desde el eje de rotación del primer piñón de accionamiento o del engrane (20) de accionamiento, respectivamente. Algunas modalidades incluyen un segundo piñón de accionamiento y el motor (52) opera para girar al segundo piñón de accionamiento a través de la segunda trayectoria de accionamiento. Tal sistema de accionamiento puede cambiar entre la primera configuración y la segunda configuración, en donde el segundo piñón de accionamiento tiene la capacidad de intercalarse con el engrane (20) de accionamiento para permitir que el motor (52) accione el engrane de accionamiento a través de la segunda trayectoria de accionamiento. Uno del segundo piñón de accionamiento y el engrane (20) de accionamiento comprende una segunda rueda dentada (62) y el otro del segundo piñón de accionamiento y del engrane (20) de accionamiento comprende la serie de rodillos (36). La primera trayectoria de accionamiento tiene un índice de engranaje más alto que la segunda trayectoria de accionamiento.
MX2015001734A 2012-08-08 2013-08-01 Sistemas de accionamiento de tren de aterrizaje. MX354164B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1214198.2A GB201214198D0 (en) 2012-08-08 2012-08-08 Landing gear drive system
PCT/GB2013/052061 WO2014023939A1 (en) 2012-08-08 2013-08-01 Landing gear drive systems

Publications (2)

Publication Number Publication Date
MX2015001734A MX2015001734A (es) 2016-01-20
MX354164B true MX354164B (es) 2018-02-15

Family

ID=46935127

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015001734A MX354164B (es) 2012-08-08 2013-08-01 Sistemas de accionamiento de tren de aterrizaje.

Country Status (10)

Country Link
US (3) US9469397B2 (es)
EP (2) EP3260368A1 (es)
JP (3) JP2015530304A (es)
KR (2) KR20200028504A (es)
CN (1) CN104520185B (es)
CA (1) CA2879325A1 (es)
GB (1) GB201214198D0 (es)
MX (1) MX354164B (es)
RU (2) RU2643114C2 (es)
WO (1) WO2014023939A1 (es)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2882644B1 (en) * 2012-08-08 2017-10-04 Airbus Operations Limited Landing gear drive systems
GB201214198D0 (en) * 2012-08-08 2012-09-19 Airbus Uk Ltd Landing gear drive system
US9139291B2 (en) * 2013-05-28 2015-09-22 Hamilton Sundstrand Corporation Integrated hydrostatic transmission for electronic taxiing operations
FR3009276B1 (fr) * 2013-07-31 2017-03-10 Airbus Operations Sas Dispositif de couplage d'une roue motorisee de train d'atterrissage d'aeronef
GB2524244A (en) * 2014-03-17 2015-09-23 Airbus Operations Ltd Landing gear drive system flexible interface
EP3038899B1 (en) 2013-09-05 2018-05-02 Airbus Operations Limited Landing gear drive system flexible interface
CA2921136A1 (en) 2013-09-05 2015-03-12 Airbus Operations Limited Landing gear drive system flexible interface
GB2526869A (en) * 2014-06-05 2015-12-09 Airbus Operations Ltd Landing gear drive system flexible interface
GB2518604A (en) 2013-09-18 2015-04-01 Airbus Operations Ltd Drive system for aircraft 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
GB2523127B (en) * 2014-02-13 2020-01-08 Airbus Operations Ltd Drive system for aircraft landing gear
EP3105120B1 (en) 2014-02-13 2019-05-08 Airbus Operations Limited Drive system for aircraft landing gear
GB2523130A (en) * 2014-02-13 2015-08-19 Airbus Operations Ltd Drive system for aircraft landing gear
GB2524097A (en) 2014-03-14 2015-09-16 Airbus Operations Ltd Wheel and gear assembly
GB2524092B (en) * 2014-03-14 2020-05-20 Airbus Operations Ltd Landing gear drive system and method
GB2524091B (en) * 2014-03-14 2020-05-20 Airbus Operations Ltd Landing gear drive system and method
GB2524242A (en) 2014-03-17 2015-09-23 Airbus Operations Ltd Drive system for aircraft landing gear
GB2524246A (en) 2014-03-17 2015-09-23 Airbus Operations Ltd Roller gear for a drive system
GB2524763B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
GB2524764B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
GB2524762B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
GB2525019A (en) * 2014-04-10 2015-10-14 Airbus Operations Ltd Drive system for aircraft landing gear
GB2528966A (en) * 2014-08-07 2016-02-10 Airbus Operations Ltd Landing gear drive system
US9499260B2 (en) * 2014-10-14 2016-11-22 Honeywell International Inc. Aircraft landing gear wheel with integral gear drive
GB2534541B (en) * 2014-11-30 2020-11-04 Borealis Tech Ltd Method for increasing aircraft effective value
AU2016200053A1 (en) * 2015-01-06 2016-07-21 Hofmann Engineering Pty Ltd Mechanical Transmission
FR3031963B1 (fr) * 2015-01-23 2020-02-28 Safran Landing Systems Procede d'entrainement en rotation d'une roue d'aeronef.
DE102015104712B3 (de) * 2015-03-27 2016-04-07 Blickle Sondermaschinen Gmbh & Co. Kg Vorrichtung zum Durchführen einer phasenverriegelten Linearverschiebung zweier parallel angeordneter Wellen
US20170002896A1 (en) * 2015-07-02 2017-01-05 Honeywell International Inc. Roller-based drive systems
CN106838186B (zh) * 2015-12-07 2018-12-28 上海宇航系统工程研究所 一种可维修驱动锁定机构
CN106379541B (zh) * 2016-08-30 2018-07-17 金嵩 一种飞机起降轮上的驱动部件
CN108408030B (zh) * 2018-01-18 2021-11-23 西安建卓航空机械制造有限公司 一种用于航空航天的飞机起落架
GB2571348A (en) 2018-02-27 2019-08-28 Airbus Operations Ltd A drive system for rotating a wheel of a landing gear
FR3079813B1 (fr) * 2018-04-04 2022-02-04 Safran Landing Systems Atterrisseur d'aeronef a repliage "parapluie"
GB2585823B (en) * 2019-06-25 2023-01-18 Airbus Operations Ltd A landing gear drive system clutch assembly
CN110525904B (zh) * 2019-09-18 2020-12-29 优力智能科技(青岛)有限公司 一种可快速拆卸的圆弧同步带运送小车

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US860536A (en) * 1906-11-24 1907-07-16 Robert W Ellingham Roller-pinion.
GB1141884A (en) 1966-05-23 1969-02-05 Imp Metal Ind Kynoch Ltd Improvements in or relating to gear train assemblies
JPS4933276U (es) * 1972-06-30 1974-03-23
US3850389A (en) 1973-05-04 1974-11-26 D Dixon Landing gear wheel device for aircraft
JPS6091837U (ja) * 1983-11-29 1985-06-22 日立造船株式会社 ピンラツク
US4659039A (en) * 1985-07-29 1987-04-21 Valdes Guillermo A Landing gear drive system
SE446898B (sv) * 1985-12-11 1986-10-13 Neos Karlsson Neuman Tamm Flerstegad kuggvexel
CN2044665U (zh) * 1987-07-30 1989-09-20 陈椿年 内环行同步滚柱轮装置
DE8806683U1 (de) * 1988-05-20 1988-08-25 EURAS Elektro- Forschungs- und Produktionsgesellschaft mbH, 8060 Dachau Getriebe
KR940009803B1 (ko) 1991-08-08 1994-10-17 구인회 일정각 속도비의 로울러-캠 치차장치
JP2988843B2 (ja) * 1995-04-13 1999-12-13 リズム時計工業株式会社 時計の修正機構
JPH10311405A (ja) * 1997-05-08 1998-11-24 Nippon Taisanbin Kogyo Kk ローラ回動体および回転伝導機構並びに減速機構
CN2378576Y (zh) * 1999-01-29 2000-05-17 中国人民解放军55254部队 外啮合滚子链轮传动装置
RO117639B1 (ro) * 1999-12-20 2002-05-30 St. Constantin Ion Angrenaj dinţat şi procedeu de realizare a danturii angrenajului
GB2422643B (en) 2003-10-09 2007-04-25 Borealis Tech Ltd A compound planetary gear system in a geared wheel motor
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
JP2010203608A (ja) * 2009-02-05 2010-09-16 Kazuyoshi Kano 駆動伝達装置
RU2395428C1 (ru) * 2009-03-10 2010-07-27 Российская Федерация, от имени которой выступает Министерство обороны РФ Устройство управления передней опорой шасси самолета
GB0915009D0 (en) 2009-08-28 2009-09-30 Airbus Operations Ltd Aircraft landing gear
FR2954234B1 (fr) * 2009-12-17 2012-03-02 Michelin Soc Tech Systeme de motorisation d'une roue associee a une suspension
FR2954236B1 (fr) 2009-12-17 2012-03-02 Michelin Soc Tech Systeme de motorisation electrique d'une roue
WO2011134503A1 (en) * 2010-04-28 2011-11-03 L-3 Communications Magnet-Motor Gmbh Drive unit for aircraft running gear
FR2975667B1 (fr) 2011-05-27 2013-07-12 Airbus Operations Sas Dispositif d'interface debrayable entre un systeme de motorisation de roue de train d'atterrissage d'avion et une roue
RU2559191C1 (ru) 2011-06-17 2015-08-10 Л-3 Коммьюникейшнз Магнет-Мотор Гмбх Узел привода для колес шасси летательного аппарата
US8979019B2 (en) 2011-07-27 2015-03-17 Honeywell International Inc. Aircraft taxi system including drive chain
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
US9499260B2 (en) * 2014-10-14 2016-11-22 Honeywell International Inc. Aircraft landing gear wheel with integral gear drive

Also Published As

Publication number Publication date
JP2015530304A (ja) 2015-10-15
EP2882643A1 (en) 2015-06-17
MX2015001734A (es) 2016-01-20
JP2018070156A (ja) 2018-05-10
WO2014023939A1 (en) 2014-02-13
US20140246539A1 (en) 2014-09-04
JP2019135156A (ja) 2019-08-15
GB201214198D0 (en) 2012-09-19
CN104520185A (zh) 2015-04-15
JP6533277B2 (ja) 2019-06-19
CA2879325A1 (en) 2014-02-13
RU2018101462A (ru) 2019-02-21
US9469397B2 (en) 2016-10-18
US9738376B2 (en) 2017-08-22
RU2015108039A (ru) 2016-09-27
KR20200028504A (ko) 2020-03-16
CN104520185B (zh) 2017-03-08
KR20150040965A (ko) 2015-04-15
EP2882643B1 (en) 2017-10-04
US20140245853A1 (en) 2014-09-04
RU2643114C2 (ru) 2018-01-30
EP3260368A1 (en) 2017-12-27
US20170305536A1 (en) 2017-10-26

Similar Documents

Publication Publication Date Title
MX354164B (es) Sistemas de accionamiento de tren de aterrizaje.
MX2015001731A (es) Sistemas de accionamiento de tren de aterrizaje.
GB2533982A (en) Drive system for aircraft landing gear
MX2015010045A (es) Sistema de accionamiento de tren de aterrizaje.
GB201309563D0 (en) Reduction gear with epicyclic gear train having roller-bearing-mounted planet spindles
WO2016061209A3 (en) Integrated electronic drive unit
IN2014DE02516A (es)
BR112017009718A2 (pt) conjunto de direção, método de operar poço, e, sistema de poço.
WO2012098198A3 (fr) Dispositif de freinage et d'entraînement en rotation d'une roue d'aéronef
BR112014030446A2 (pt) propulsion system for a vehicle or a toy vehicle
JP2013052874A5 (es)
IN2014DE02519A (es)
WO2014184608A3 (en) Control of ground travel and steering in an aircraft with powered main gear drive wheels
MX2017005737A (es) Sistema de riego por pivote y componentes.
FI20115256L (fi) Telin tasapainotusmekanismi
WO2013058666A3 (en) A lifting apparatus with two independent drive wheels
CN203924831U (zh) 一种用于立体车库的防晃动回转装置
GB201206437D0 (en) Maritime reducer gearbox
WO2013053988A3 (en) Power transmission arrangement, method for power transmission in a gear system and use of power transmission arrangement
CN203755763U (zh) 一种立体车库载车板旋转装置
WO2014121776A3 (de) Differentialgetriebe
RU2512055C2 (ru) Универсальное транспортное средство суперманевренности и суперпроходимости
UA89545U (ru) Устройство для обработки отверстий
UA97787U (xx) Планетарна передача
UA91277U (uk) Планетарна передача

Legal Events

Date Code Title Description
FG Grant or registration