BR112012027644A2 - unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave - Google Patents

unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave

Info

Publication number
BR112012027644A2
BR112012027644A2 BR112012027644A BR112012027644A BR112012027644A2 BR 112012027644 A2 BR112012027644 A2 BR 112012027644A2 BR 112012027644 A BR112012027644 A BR 112012027644A BR 112012027644 A BR112012027644 A BR 112012027644A BR 112012027644 A2 BR112012027644 A2 BR 112012027644A2
Authority
BR
Brazil
Prior art keywords
landing gear
aircraft landing
drive unit
wheel
aircraft
Prior art date
Application number
BR112012027644A
Other languages
English (en)
Inventor
Johann Oswald
Manfred Heeg
Original Assignee
L 3 Comm Magnet Motor Gmbh
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 L 3 Comm Magnet Motor Gmbh filed Critical L 3 Comm Magnet Motor Gmbh
Publication of BR112012027644A2 publication Critical patent/BR112012027644A2/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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H48/00Differential gearings
    • F16H48/06Differential gearings with gears having orbital motion
    • F16H48/08Differential gearings with gears having orbital motion comprising bevel gears
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H48/00Differential gearings
    • F16H48/20Arrangements for suppressing or influencing the differential action, e.g. locking devices
    • F16H48/30Arrangements for suppressing or influencing the differential action, e.g. locking devices using externally-actuatable means
    • F16H48/32Arrangements for suppressing or influencing the differential action, e.g. locking devices using externally-actuatable means using fluid pressure actuators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H48/00Differential gearings
    • F16H48/20Arrangements for suppressing or influencing the differential action, e.g. locking devices
    • F16H48/30Arrangements for suppressing or influencing the differential action, e.g. locking devices using externally-actuatable means
    • F16H48/34Arrangements for suppressing or influencing the differential action, e.g. locking devices using externally-actuatable means using electromagnetic or electric actuators
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Analytical Chemistry (AREA)
  • Chemical & Material Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetism (AREA)
  • Gear Transmission (AREA)
  • Retarders (AREA)
  • Toys (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave. a unidade de acionamento (16) para um trem de pouso de aeronave (2) tendo pelo menos uma primeira roda (4) e uma segunda roda (6) em um eixo de roda em comum (a) é caracterizado pelo fato de que a unidade de acionamento (16) pode ser acionadamente acoplada à primeira e segunda rodas (4,6) de forma que uma direção de extensão longitudinal (c) da unidade de acionamento (16) está em um plano ortogonal ao eixo de roda em comum (a).
BR112012027644A 2010-04-28 2010-04-28 unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave BR112012027644A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/EP2010/055688 WO2011134503A1 (en) 2010-04-28 2010-04-28 Drive unit for aircraft running gear

Publications (1)

Publication Number Publication Date
BR112012027644A2 true BR112012027644A2 (pt) 2016-08-16

Family

ID=43569481

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012027644A BR112012027644A2 (pt) 2010-04-28 2010-04-28 unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave

Country Status (10)

Country Link
US (2) US9169005B2 (pt)
EP (1) EP2563657B1 (pt)
JP (1) JP5519076B2 (pt)
CN (1) CN102892673B (pt)
AR (1) AR081340A1 (pt)
BR (1) BR112012027644A2 (pt)
CA (1) CA2796373C (pt)
DE (1) DE10718552T1 (pt)
RU (1) RU2529558C2 (pt)
WO (1) WO2011134503A1 (pt)

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2954235B1 (fr) 2009-12-17 2012-03-16 Michelin Soc Tech Systeme de motorisation electrique d'une roue
FR2954234B1 (fr) 2009-12-17 2012-03-02 Michelin Soc Tech Systeme de motorisation d'une roue associee a une suspension
US9334047B2 (en) * 2011-02-08 2016-05-10 Borealis Technical Limited Method and system for the powered self push back of an aircraft
US9120565B2 (en) * 2011-07-15 2015-09-01 Borealis Technical Limited Method for enhancing pilot efficiency and aircraft safety during ground travel
US8807479B2 (en) * 2012-03-12 2014-08-19 Honeywell International Inc. Movable bushing interface and taxi drive system
GB201214198D0 (en) * 2012-08-08 2012-09-19 Airbus Uk Ltd Landing gear drive system
RU2643857C2 (ru) * 2012-08-08 2018-02-06 Эрбас Оперэйшнс Лимитед Приводная система шасси
GB2517396A (en) * 2013-05-13 2015-02-25 Airbus Operations Ltd Landing gear drive systems
FR2998870B1 (fr) * 2012-12-03 2015-01-09 Michelin & Cie Systeme de motorisation de roue, notamment d'un aeronef
IN2015DN04297A (pt) * 2012-12-14 2015-10-16 L 3 Comm Magnet Motor Gmbh
US9211948B2 (en) * 2013-03-24 2015-12-15 Honeywell International Inc. Between-wheel bogie mounted taxi system
US9139291B2 (en) * 2013-05-28 2015-09-22 Hamilton Sundstrand Corporation Integrated hydrostatic transmission for electronic taxiing operations
JP6585051B2 (ja) * 2013-09-05 2019-10-02 エアバス オペレーションズ リミテッドAirbus Operations Limited 着陸装置駆動システムのフレキシブルインターフェース
GB2518605B (en) * 2013-09-18 2020-02-12 Airbus Operations Ltd Drive system for landing gear
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
US20150210384A1 (en) * 2014-01-24 2015-07-30 Honeywell International Inc. Aircraft wheel driving system
FR3018502B1 (fr) * 2014-03-12 2018-03-23 Safran Landing Systems Atterrisseur d'aeronef
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
GB2524762B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
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
US20150283908A1 (en) * 2014-04-02 2015-10-08 Hamilton Sundstrand Corporation Systems utilizing a controllable voltage ac generator system
CN106464174A (zh) * 2014-04-04 2017-02-22 罗伯特·博世有限公司 方法、驱动系统和车辆
GB2525019A (en) * 2014-04-10 2015-10-14 Airbus Operations Ltd Drive system for aircraft landing gear
FR3024706B1 (fr) * 2014-08-05 2018-03-23 Messier Bugatti Dowty Transmission de couple a la roue par les boulons d'assemblage de la jante
GB2528966A (en) * 2014-08-07 2016-02-10 Airbus Operations Ltd Landing gear drive system
FR3026717B1 (fr) * 2014-10-03 2016-11-25 Messier Bugatti Dowty Atterrisseur d'aeronef.
US10940941B2 (en) * 2014-12-04 2021-03-09 Borealis Technical Limited Method for increasing aircraft effective value
US10308352B2 (en) * 2014-12-12 2019-06-04 Borealis Technical Limited Monitoring system for aircraft drive wheel system
DE202015000784U1 (de) 2015-01-31 2015-05-07 Michael Frimann Hydraulischer Antrieb und -Energiespeicherung für Flugzeug-Fahrwerke
RU2583518C1 (ru) * 2015-04-22 2016-05-10 Общество с ограниченной ответственностью "Научно-инженерная компания "Объектные системы автоматики" (ООО "НИК "ОСА") Многодвигательный электропривод поворота носовой опоры шасси самолета и способ его работы
FR3037561B1 (fr) * 2015-06-16 2017-06-09 Sagem Defense Securite Atterrisseur pour aeronef
FR3037562B1 (fr) * 2015-06-16 2018-11-02 Safran Electronics & Defense Atterrisseur pour aeronef
FR3038724B1 (fr) * 2015-07-10 2019-06-14 Safran Landing Systems Dispositif de mesure d'une vitesse relative de rotation et/ou d'une position angulaire relative entre deux elements tournants
US9771149B2 (en) * 2015-10-30 2017-09-26 Honeywell International Inc. Gate departure system for aircraft
US10272992B2 (en) * 2015-10-31 2019-04-30 Borealis Technical Limited Clutch assembly for aircraft drive wheel drive system
US10697528B2 (en) * 2016-03-23 2020-06-30 Shaun Chu Regenerative differential for differentially steered and front-wheel steered vehicles
US9709148B1 (en) 2016-04-20 2017-07-18 Shaun Chu Differential system with differential rate governed by variable speed motor and associated method of operation
RU167611U1 (ru) * 2016-03-25 2017-01-10 Акционерное общество "Технодинамика" Электромеханизм привода шасси
WO2019051314A1 (en) 2017-09-08 2019-03-14 Chu Shaun DIFFERENTIAL SYSTEM COMPRISING DIFFERENTIAL SPEED-SPEED PLANETARY GEARS GOVERNED BY A VARIABLE SPEED MOTOR AND METHOD OF OPERATION THEREOF
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
DE102018115112A1 (de) 2018-06-22 2019-12-24 Ebm-Papst St. Georgen Gmbh & Co. Kg Radantriebsmodul zum Antrieb und zur Lenkung eines Rades
CN113014161A (zh) * 2019-12-20 2021-06-22 美蓓亚三美株式会社 旋转装置的控制装置、旋转装置以及旋转装置的控制方法
CN112572781B (zh) * 2020-12-04 2023-04-14 中国航空工业集团公司成都飞机设计研究所 一种前轮转弯减速输出机构

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1883740A (en) * 1930-05-31 1932-10-18 Irwin Herbert Ellwood Airplane
FR697180A (fr) * 1930-11-08 1931-01-13 Cie J G Brill Perfectionnements à la commande des essieux moteurs de voitures sur voies ferrées
US3096052A (en) * 1961-01-25 1963-07-02 Sperry Rand Corp Pre-spinning of aircraft landing wheels
US3279722A (en) * 1964-08-07 1966-10-18 Nat Can Retinning Co Aircraft moving device
DE1625099A1 (de) * 1967-03-06 1970-05-21 Linde Ag Hydrostatisches Getriebe mit zwei Motoren
SU301039A1 (ru) * 1969-11-03 1988-12-07 Brill D E Устройство гидравлического привода дл передвижени летательного аппарата по земле
US3762670A (en) * 1971-12-16 1973-10-02 Curtiss Wright Corp Landing gear wheel drive system for aircraft
US4858490A (en) * 1987-10-13 1989-08-22 Hughes Aircraft Company Two motor redundant drive mechanism
GB8724123D0 (en) * 1987-10-14 1987-11-18 Balloch J Variable speed aircraft landing wheels
JPH03295796A (ja) 1990-04-16 1991-12-26 Mitsubishi Heavy Ind Ltd 飛行機用着陸装置
GB9408075D0 (en) * 1994-04-22 1994-06-15 Greenlite Limited Improvements in or relating to aircraft
JP3295796B2 (ja) * 1995-10-30 2002-06-24 株式会社岡村製作所 椅子の肘掛け装置及びそれを備える椅子
US6843750B1 (en) * 2003-07-30 2005-01-18 Arvinmeritor Technology, Llc Two-speed gearbox with integrated differential
US20080142284A1 (en) * 2006-12-15 2008-06-19 General Electric Company Double-sided dual-shaft electrical machine
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
GB0616730D0 (en) * 2006-08-23 2006-10-04 Airbus Uk Ltd Jam-tolerant actuator
GB0618902D0 (en) * 2006-09-25 2006-11-01 Airbus Uk Ltd Actuator
RU2384467C2 (ru) * 2008-04-01 2010-03-20 Вячеслав Иванович Беляев Устройство для раскрутки колеса шасси самолета при полете перед приземлением
GB0915009D0 (en) * 2009-08-28 2009-09-30 Airbus Operations Ltd Aircraft landing gear
FR2954752B1 (fr) * 2009-12-24 2012-03-09 Messier Bugatti Ensemble de roue et frein pour aeronef equipe d'un dispositif d'entrainement en rotation.
GB2489503A (en) * 2011-03-31 2012-10-03 Ge Aviat Systems Ltd Rotary actuator and method of operation with failsafe mechanism
RU2559191C1 (ru) * 2011-06-17 2015-08-10 Л-3 Коммьюникейшнз Магнет-Мотор Гмбх Узел привода для колес шасси летательного аппарата
US8899516B2 (en) * 2012-04-05 2014-12-02 JHamilton Sundstrand Corporation Coaxial contra-rotating motors for differential landing gear steering
US9211948B2 (en) * 2013-03-24 2015-12-15 Honeywell International Inc. Between-wheel bogie mounted taxi system

Also Published As

Publication number Publication date
EP2563657B1 (en) 2016-09-21
WO2011134503A1 (en) 2011-11-03
DE10718552T1 (de) 2013-07-18
JP2013525188A (ja) 2013-06-20
CN102892673B (zh) 2015-10-14
JP5519076B2 (ja) 2014-06-11
AR081340A1 (es) 2012-08-08
US9169005B2 (en) 2015-10-27
RU2529558C2 (ru) 2014-09-27
CA2796373A1 (en) 2011-11-03
CA2796373C (en) 2017-08-22
RU2012150817A (ru) 2014-06-20
US20130200210A1 (en) 2013-08-08
EP2563657A1 (en) 2013-03-06
US20160009383A1 (en) 2016-01-14
CN102892673A (zh) 2013-01-23

Similar Documents

Publication Publication Date Title
BR112012027644A2 (pt) unidade de acionamento para um trem de pouso de aeronave, e, trem de pouso de aeronave
BR112013028024A2 (pt) unidade de acionamento, e, trem de rolamento de aeronave
BR102014012127A8 (pt) reboque de veículo, para uma unidade de tração, em particular um semirreboque ou reboque de lança e combinação de veículos
BR112013006283A2 (pt) conexão de feixe-eixo para veículo pesado
BR112015013037A2 (pt) trem de pouso para reboque de múltiplas velocidades
WO2013070296A3 (en) Aircraft system for reduced observer visibility
BR112016025058A2 (pt) caixa de câmbio para veículos e veículos compreendendo tal caixa de câmbio
BRPI0818602A2 (pt) Detecção de carga em um trem de pouso de aeronave
BR112015019820A2 (pt) dispositivo de exercício
BR112015023754A2 (pt) artigo de liga de titânio nanoestruturada, e, método para fabricar uma liga de titânio nanoestruturada
BR112012029819A2 (pt) trem de pouso
BR112013006278A2 (pt) montagem de eixo componente de sistema de freio
BRPI0812806A2 (pt) Placa de fixação para fixar de modo removível uma unidade de propulsão de peça única a uma asa de uma aeronave, membro de manipulação longitudinal e instalação
BR112015025134A2 (pt) sistema para dirigir um eixo auxiliar de um veículo
BR112012019688A2 (pt) sistema de impressão
BR102013022221A8 (pt) unidade de anexação para acionamento pelo menos auxiliar, preferencialmente para acionamento pelo menos temporário único de um veículo e veículo
BR112015018741A2 (pt) retentor de tanque em uma aeronave
WO2012136804A3 (en) High lift system for an aircraft
BR112013006035A2 (pt) diferencial para veículos automotores.
BR112015029987A8 (pt) Beta-caseína a2 e a prevenção de inflamação do intestino
BR112015004598A8 (pt) porta de veículo automotor, com uma fechadura de porta de veículo automotor
BR112017009477A2 (pt) ?sistema de irrigação por pivô e componentes?.
BRPI0801697A2 (pt) trem de pouso para aeronaves
BR112012020137A2 (pt) trem de pouso com eixo de roda direcionável
BR112016024229A2 (pt) banda de rodagem de pneumático para veículo de uso agrícola

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application fees: application dismissed [chapter 8.6 patent gazette]

Free format text: REFERENTE A 9A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2512 DE 26-02-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]