JP2008513283A5 - - Google Patents

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Publication number
JP2008513283A5
JP2008513283A5 JP2007531809A JP2007531809A JP2008513283A5 JP 2008513283 A5 JP2008513283 A5 JP 2008513283A5 JP 2007531809 A JP2007531809 A JP 2007531809A JP 2007531809 A JP2007531809 A JP 2007531809A JP 2008513283 A5 JP2008513283 A5 JP 2008513283A5
Authority
JP
Japan
Prior art keywords
control command
landing leg
gate
leg
landing
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
JP2007531809A
Other languages
English (en)
Japanese (ja)
Other versions
JP2008513283A (ja
JP4528831B2 (ja
Filing date
Publication date
Priority claimed from FR0452105A external-priority patent/FR2875475B1/fr
Application filed filed Critical
Publication of JP2008513283A publication Critical patent/JP2008513283A/ja
Publication of JP2008513283A5 publication Critical patent/JP2008513283A5/ja
Application granted granted Critical
Publication of JP4528831B2 publication Critical patent/JP4528831B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2007531809A 2004-09-21 2005-09-15 航空機用着陸脚の操作システム及びそのようなシステムを備える航空機 Expired - Fee Related JP4528831B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452105A FR2875475B1 (fr) 2004-09-21 2004-09-21 Systeme de manoeuvre d'un train d'atterrissage pour aeronef et aeronef comportant un tel systeme
PCT/FR2005/050746 WO2006032811A1 (fr) 2004-09-21 2005-09-15 Systeme de manoeuvre d'un train d'atterrissage pour aeronef et aeronef comportant un tel systeme

Publications (3)

Publication Number Publication Date
JP2008513283A JP2008513283A (ja) 2008-05-01
JP2008513283A5 true JP2008513283A5 (enExample) 2010-05-06
JP4528831B2 JP4528831B2 (ja) 2010-08-25

Family

ID=34949528

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007531809A Expired - Fee Related JP4528831B2 (ja) 2004-09-21 2005-09-15 航空機用着陸脚の操作システム及びそのようなシステムを備える航空機

Country Status (8)

Country Link
US (1) US8191827B2 (enExample)
EP (1) EP1802526B1 (enExample)
JP (1) JP4528831B2 (enExample)
CN (1) CN100515862C (enExample)
CA (1) CA2580829C (enExample)
FR (1) FR2875475B1 (enExample)
RU (1) RU2363617C2 (enExample)
WO (1) WO2006032811A1 (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2898866B1 (fr) * 2006-03-22 2008-11-21 Airbus France Sas Distributeur hydraulique pour train d'atterrissage d'avion
FR2931798B1 (fr) * 2008-05-29 2010-08-20 Airbus France Atterrisseur avant d'aeronef integre a commande electrique
US8070094B2 (en) * 2008-07-16 2011-12-06 Hamilton Sundstrand Corporation Aircraft landing gear actuator
FR2957585B1 (fr) * 2010-03-17 2012-03-02 Airbus Operations Sas Procede et dispositif d'entrainement d'au moins une roue de train d'atterrissage d'un aeronef par un moteur de roue
FR2980461B1 (fr) * 2011-09-26 2013-10-04 Messier Bugatti Dowty Dispositif de manoeuvre au sol d'une trappe d'un atterrisseur d'aeronef.
FR2984276B1 (fr) * 2011-12-15 2014-03-07 Messier Bugatti Dowty Procede de gestion de systemes lies au train d'atterrissage d'un aeronef.
FR2986502B1 (fr) * 2012-02-08 2014-03-07 Messier Bugatti Dowty Boitier de commande
FR3013681B1 (fr) * 2013-11-22 2017-06-09 Messier Bugatti Dowty Procede pour diminuer le temps de manoeuvre apparent d'atterrisseurs d'un aeronef.
FR3030442B1 (fr) * 2014-12-18 2017-01-27 Airbus Operations Sas Pointe avant d'aeronef equipee d'un cadre de jonction entre la case de train d'atterrissage et la peau exterieure du fuselage
GB2562027A (en) * 2017-03-02 2018-11-07 Airbus Operations Ltd Control system and method for landing gear extension/retraction
GB2562485A (en) * 2017-05-15 2018-11-21 Airbus Operations Ltd Aircraft door control
GB2563437A (en) * 2017-06-16 2018-12-19 Airbus Operations Ltd Landing gear controller
GB2563675A (en) * 2017-06-23 2018-12-26 Airbus Operations Ltd Aircraft hydraulics
CN109343335A (zh) * 2018-11-05 2019-02-15 中国航空工业集团公司西安飞机设计研究所 一种舱门多余度控制系统
GB2581824A (en) * 2019-02-28 2020-09-02 Airbus Operations Ltd Landing gear control
GB2583464A (en) * 2019-04-18 2020-11-04 Airbus Operations Ltd System and method for landing gear retraction
CN113753223A (zh) * 2020-06-02 2021-12-07 北京航天易联科技发展有限公司 一种起落架的控制方法及装置、电子设备、存储介质
CN111731491B (zh) * 2020-06-12 2024-09-13 陕西飞机工业（集团）有限公司 一种飞机脚操纵机构装配方法
CN112937841B (zh) * 2021-03-04 2022-07-05 中国商用飞机有限责任公司 起落架及舱门控制系统以及控制方法
US12280866B2 (en) 2022-07-01 2025-04-22 Textron Innovations Inc. Pneumo-mechanical landing gear deployment system and method

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2452787A (en) * 1948-01-02 1948-11-02 North American Aviation Inc Landing gear system
US2701695A (en) * 1949-08-18 1955-02-08 Mcdonnell Aircraft Corp Hydraulic interlock for retractable landing gear and closure operators for the chambers therefor
US4312619A (en) * 1979-07-19 1982-01-26 Fmc Corporation Aircraft cargo loading method and apparatus
US4573649A (en) * 1983-08-01 1986-03-04 The Boeing Company Integrated alternate gear extension and ground-crew door opening/closing system for an aircraft
JPS6456889A (en) 1987-08-28 1989-03-03 Sumitomo Chemical Co Method for removing scale in jacket of glass lined apparatus
FR2677950B1 (fr) * 1991-06-21 1996-07-05 Messier Bugatti Dispositif de manóoeuvre electrique d'un atterrisseur.
JP3095598B2 (ja) * 1993-12-08 2000-10-03 本田技研工業株式会社 航空機の脚の昇降装置
US5484120A (en) * 1994-03-11 1996-01-16 Sundstrand Corporation Support strut for ram air driven turbine
US6499005B2 (en) * 1997-11-10 2002-12-24 The Boeing Company System and method for simulating air mode and ground mode of an airplane
RU2122964C1 (ru) * 1998-06-15 1998-12-10 Акционерное общество открытого типа "ОКБ Сухого" Механизм управления выпуском шасси летательного аппарата
CN2402596Y (zh) * 1999-09-01 2000-10-25 张新民 飞机起落架机械式控制装置
US6625504B2 (en) * 2001-03-22 2003-09-23 Honeywell International Inc. Auxiliary power unit engine monitoring system
FR2836668B1 (fr) * 2002-03-04 2004-12-03 Messier Bugatti Dispositif d'accrochage, notamment pour l'accrochage d'un train d'atterrissage d'aeronef ou d'une trappe de train d'atterrissage d'aeronef, et procede de fonctionnement dudit dispositif
DE10330805B4 (de) * 2003-07-08 2015-07-30 Liebherr-Aerospace Lindenberg Gmbh Luftfahrzeug-Fahrwerksbetätigung

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