[go: up one dir, main page]

MX2016012923A - Sistema de accionamiento de engranaje de aterrizaje de aviones. - Google Patents

Sistema de accionamiento de engranaje de aterrizaje de aviones.

Info

Publication number
MX2016012923A
MX2016012923A MX2016012923A MX2016012923A MX2016012923A MX 2016012923 A MX2016012923 A MX 2016012923A MX 2016012923 A MX2016012923 A MX 2016012923A MX 2016012923 A MX2016012923 A MX 2016012923A MX 2016012923 A MX2016012923 A MX 2016012923A
Authority
MX
Mexico
Prior art keywords
pinion
actuator
driven gear
torque
initial contact
Prior art date
Application number
MX2016012923A
Other languages
English (en)
Inventor
Morris James
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 MX2016012923A publication Critical patent/MX2016012923A/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 
    • B64C25/40—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 
    • B64C25/405—Powered wheels, e.g. for taxing
    • 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 
    • B64C25/42—Arrangement or adaptation of brakes
    • 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
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/02—Toothed gearings for conveying rotary motion without gears having orbital motion
    • F16H1/24—Toothed gearings for conveying rotary motion without gears having orbital motion involving gears essentially having intermeshing elements other than involute or cycloidal teeth
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P31/00—Arrangements for regulating or controlling electric motors not provided for in groups H02P1/00 - H02P5/00, H02P7/00 or H02P21/00 - H02P29/00
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Gear Transmission (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Transmission Device (AREA)

Abstract

Un método para acoplar un sistema de accionamiento con una rueda rotatoria de un engranaje de aterrizaje de avión. Un motor es operado para aplicar torque a un piñón de manera que el piñón gira. Se emite un comando de acoplamiento a un accionador a un tiempo de acoplamiento y el accionador opera el accionador en respuesta al comando de acoplamiento para mover el piñón desde una posición neutral a una posición de contacto en la cual contacta un engranaje impulsado rotatorio en un tiempo de contacto inicial, montándose el engranaje impulsado rotatorio en una rueda rotatoria de un engranaje de aterrizaje de avión; entonces después del tiempo de contacto inicial que opera el accionador para mover el piñón de manera adicional a una posición de engrane donde el piñón se engrana con el engranaje impulsado. Una distancia centro-a-centro entre el piñón y el engranaje impulsado se reduce conforme el piñón se mueve a la posición de contacto y a la posición de engrane. El motor es operado para reducir el torque por debajo de un nivel predeterminado a o después del tiempo de acoplamiento, mantener el torque por abajo del nivel predeterminado durante una fase de desactivación hasta el tiempo de contacto inicial, entonces después del tiempo de contacto inicial aumentar el torque por arriba del nivel predeterminado.
MX2016012923A 2014-04-01 2015-03-31 Sistema de accionamiento de engranaje de aterrizaje de aviones. MX2016012923A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1405849.9A GB2524762B (en) 2014-04-01 2014-04-01 Drive system for aircraft landing gear
PCT/GB2015/050979 WO2015150776A1 (en) 2014-04-01 2015-03-31 Drive system for aircraft landing gear

Publications (1)

Publication Number Publication Date
MX2016012923A true MX2016012923A (es) 2016-12-07

Family

ID=50737811

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016012923A MX2016012923A (es) 2014-04-01 2015-03-31 Sistema de accionamiento de engranaje de aterrizaje de aviones.

Country Status (10)

Country Link
US (2) US10266255B2 (es)
EP (2) EP3296197A1 (es)
JP (1) JP6581594B2 (es)
KR (1) KR20160141761A (es)
CN (2) CN106163923B (es)
CA (1) CA2943433A1 (es)
GB (1) GB2524762B (es)
MX (1) MX2016012923A (es)
RU (1) RU2675769C2 (es)
WO (1) WO2015150776A1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019113433A1 (en) * 2017-12-08 2019-06-13 Aero Controlex Group Inc. Blow down actuator assembly having a drag brake
GB2571348A (en) * 2018-02-27 2019-08-28 Airbus Operations Ltd A drive system for rotating a wheel of a landing gear
FR3079570B1 (fr) * 2018-03-28 2020-04-17 Safran Landing Systems Procede d'engagement de deux elements engrenage et dispositif d'entrainement mettant en œuvre un tel procede
FR3082825B1 (fr) * 2018-06-26 2020-09-04 Safran Landing Systems Mecanisme de verrouillage d’actionneur de roue
FR3085457B1 (fr) * 2018-09-05 2021-01-22 Safran Landing Systems Procede d'engagement de deux elements engrenage et dispositif d'entrainement mettant en œuvre un tel procede
EP4556044A3 (en) 2019-11-07 2025-07-02 ResMed Pty Ltd Vent for a respiratory system
US11912399B2 (en) 2022-02-18 2024-02-27 Goodrich Corporation Compact aircraft actuator system
US11851167B2 (en) 2022-02-24 2023-12-26 Goodrich Corporation Integral steering motor and collar for landing gear
GB202306561D0 (en) * 2023-05-03 2023-06-14 Precision Tech Group Ptg Limited Gear assembly

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4142698A (en) * 1976-12-03 1979-03-06 United Technologies Corporation Improved aircraft suspension system with mechanism operable to establish system vertical stiffness and damping and mechanism operationally independent thereof to establish system roll stiffness and damping
JPH02100876U (es) * 1989-01-30 1990-08-10
KR940009803B1 (ko) * 1991-08-08 1994-10-17 구인회 일정각 속도비의 로울러-캠 치차장치
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
JP4404254B2 (ja) * 2004-02-17 2010-01-27 コスモ工機株式会社 フランジ接合装置
JP4556035B2 (ja) * 2005-06-21 2010-10-06 独立行政法人 日本原子力研究開発機構 陽子加速器用配管着脱装置
EP2077367A1 (en) * 2008-01-07 2009-07-08 Meritor Technology, Inc. Holding/releasing/resetting mechanism
RU2384467C2 (ru) * 2008-04-01 2010-03-20 Вячеслав Иванович Беляев Устройство для раскрутки колеса шасси самолета при полете перед приземлением
DE102008054979A1 (de) * 2008-12-19 2010-06-24 Robert Bosch Gmbh Verfahren und Vorrichtung für Start-Stopp-Anlagen von Brennkraftmaschinen in Kraftfahrzeugen
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
JP4835774B2 (ja) * 2009-09-04 2011-12-14 株式会社デンソー エンジン停止始動制御装置
FR2954234B1 (fr) * 2009-12-17 2012-03-02 Michelin Soc Tech Systeme de motorisation d'une roue associee a une suspension
CN102892673B (zh) * 2010-04-28 2015-10-14 L-3通信磁铁电动机有限公司 用于飞机行走机构的驱动单元
CN101870358B (zh) * 2010-06-23 2012-12-26 南京航空航天大学 扭力臂式前轮转弯机构及工作方法
JP4926272B1 (ja) * 2010-10-29 2012-05-09 三菱電機株式会社 エンジン自動停止再始動装置
JP5409587B2 (ja) 2010-12-17 2014-02-05 日立オートモティブシステムズ株式会社 車両エンジンの再始動装置及びその制御方法
JP5470241B2 (ja) * 2010-12-28 2014-04-16 日立オートモティブシステムズ株式会社 車両の制御装置
JP5495390B2 (ja) 2011-02-17 2014-05-21 日立オートモティブシステムズ株式会社 アイドルストップシステムの制御装置および制御方法
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
BR112013028024A2 (pt) * 2011-06-17 2017-01-10 L 3 Comm Magnet Motor Gmbh unidade de acionamento, e, trem de rolamento de aeronave
US8979019B2 (en) * 2011-07-27 2015-03-17 Honeywell International Inc. Aircraft taxi system including drive chain
US9193449B2 (en) * 2011-08-22 2015-11-24 Borealis Technical Limited Method for optimizing operation of aircraft ground travel drive system
FR2981331B1 (fr) 2011-10-14 2013-11-15 Messier Bugatti Dowty Dispositif de connexion d'un motoreducteur a une roue d'aeronef, pour permettre son entrainement selectif par le motoreducteur.
US8829845B2 (en) * 2012-02-28 2014-09-09 Remy Technologies, Llc Starter machine system and method
GB201214198D0 (en) * 2012-08-08 2012-09-19 Airbus Uk Ltd Landing gear drive system
MX359695B (es) * 2012-08-08 2018-10-08 Airbus Operations Ltd Sistemas de accionamiento de tren de aterrizaje.

Also Published As

Publication number Publication date
RU2016142575A3 (es) 2018-10-30
GB2524762A (en) 2015-10-07
EP3296197A1 (en) 2018-03-21
RU2016142575A (ru) 2018-05-10
RU2675769C2 (ru) 2018-12-24
KR20160141761A (ko) 2016-12-09
US20170197707A1 (en) 2017-07-13
GB2524762B (en) 2020-06-17
CA2943433A1 (en) 2015-10-08
CN106163923B (zh) 2019-01-22
US20190202551A1 (en) 2019-07-04
JP2017512700A (ja) 2017-05-25
WO2015150776A1 (en) 2015-10-08
US10266255B2 (en) 2019-04-23
CN110015409A (zh) 2019-07-16
JP6581594B2 (ja) 2019-09-25
US11066154B2 (en) 2021-07-20
CN106163923A (zh) 2016-11-23
EP3126228A1 (en) 2017-02-08
GB201405849D0 (en) 2014-05-14
EP3126228B1 (en) 2018-01-24

Similar Documents

Publication Publication Date Title
MX2016012923A (es) Sistema de accionamiento de engranaje de aterrizaje de aviones.
MX362864B (es) Sistema de accionamiento de tren de aterrizaje.
GB201522634D0 (en) Method for operating a motor vehicle by remote control
WO2015147948A3 (en) Geared gas turbine engine with reduced oil tank size
RU2016102613A (ru) Устройство управления рулением
PL3160823T3 (pl) Wspomaganie mieszane układu kierowniczego posiadające układ sterowania z wartością zadaną sterowany przez sterownik pozycji przeznaczony do sterowania torem jazdy
MX365231B (es) Dispositivo de diagnóstico de fallas y método de diagnóstico de fallas.
GB201404699D0 (en) Drive system for landing gear and drive system control method
WO2015006153A3 (en) Fan drive gear system mechanical controller
MX364768B (es) Procedimiento para controlar un accionamiento y sistema de accionamiento que trabaja de acuerdo con el procedimiento.
EP3119652A4 (en) Method for controlling a hybrid driveline in order to achieve gear change without interruption of torque
PH12016502289B1 (en) Method for controlling a pump arrangement
FR3015707B1 (fr) Procede de commande d'un moteur electrique d'entrainement en rotation d'une roue d'aeronef.
CL2014000741A1 (es) Metodo y sistema para operar una maquina relacionada con la mineria y/o la construccion, donde dicha maquina esta dispuesta para ser controlada por un operador mediante medios de maniobra, donde el operador al conducir dicha maquina, provee comandos de direccion mediante los medios de maniobra
GB2533982A (en) Drive system for aircraft landing gear
EP3303086A4 (en) METHOD FOR CONTROLLING THE CURRENT SPEED OF A MOTOR VEHICLE
WO2013149780A3 (de) Verfahren und vorrichtung zum elektrodynamischen bremsen eines universalmotors
EP3186501A4 (en) Method for controlling the operation a submersible power plant
MY191546A (en) Electric brake device
WO2013160351A3 (en) Apparatus comprising electromechanical device and motion detector and method for operating apparatus
WO2014115016A3 (en) Drive assist system, drive assist method, and drive assist device
GB201803147D0 (en) A drive system for rotating a wheel of a landing gear
EP3615829B8 (fr) Procede de controle d'un groupe motopropulseur de vehicule automobile pour empecher le calage d'un moteur
WO2013098102A3 (de) Verfahren zum betreiben einer elektrischen maschine, elektrische maschine
IL251227B (en) An automatic transmission system in which the combination of gears is determined by the angular velocity of the driven wheel