DE602006001378D1 - Verteilte Architektur eines Kontrollsystems eines Flugzeug-Fahrgestells - Google Patents

Verteilte Architektur eines Kontrollsystems eines Flugzeug-Fahrgestells

Info

Publication number
DE602006001378D1
DE602006001378D1 DE602006001378T DE602006001378T DE602006001378D1 DE 602006001378 D1 DE602006001378 D1 DE 602006001378D1 DE 602006001378 T DE602006001378 T DE 602006001378T DE 602006001378 T DE602006001378 T DE 602006001378T DE 602006001378 D1 DE602006001378 D1 DE 602006001378D1
Authority
DE
Germany
Prior art keywords
control system
distributed architecture
aircraft chassis
aircraft
chassis
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.)
Active
Application number
DE602006001378T
Other languages
English (en)
Inventor
Jean-Pierre Garcia
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Landing Systems SAS
Original Assignee
Messier Bugatti SA
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 Messier Bugatti SA filed Critical Messier Bugatti SA
Publication of DE602006001378D1 publication Critical patent/DE602006001378D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/32—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration
    • B60T8/88—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration with failure responsive means, i.e. means for detecting and indicating faulty operation of the speed responsive control means
    • B60T8/885—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration with failure responsive means, i.e. means for detecting and indicating faulty operation of the speed responsive control means using electrical circuitry
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T8/00—Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
    • B60T8/17—Using electrical or electronic regulation means to control braking
    • B60T8/1701—Braking or traction control means specially adapted for particular types of vehicles
    • B60T8/1703—Braking or traction control means specially adapted for particular types of vehicles for aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/26—Control or locking systems therefor
    • 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
    • B64C25/44—Actuating mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T2270/00—Further aspects of brake control systems not otherwise provided for
    • B60T2270/40—Failsafe aspects of brake control systems
    • B60T2270/413—Plausibility monitoring, cross check, redundancy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
    • B60T2270/00—Further aspects of brake control systems not otherwise provided for
    • B60T2270/82—Brake-by-Wire, EHB
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L2012/40208—Bus networks characterized by the use of a particular bus standard
    • H04L2012/40241—Flexray
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L12/00—Data switching networks
    • H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
    • H04L12/40—Bus networks
    • H04L2012/40267—Bus for use in transportation systems
    • H04L2012/4028—Bus for use in transportation systems the transportation system being an aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Regulating Braking Force (AREA)
DE602006001378T 2005-06-27 2006-06-15 Verteilte Architektur eines Kontrollsystems eines Flugzeug-Fahrgestells Active DE602006001378D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0506498A FR2887516B1 (fr) 2005-06-27 2005-06-27 Architecture distribuee de systeme de gestion d'atterisseurs d'aeronef

Publications (1)

Publication Number Publication Date
DE602006001378D1 true DE602006001378D1 (de) 2008-07-17

Family

ID=35645798

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006001378T Active DE602006001378D1 (de) 2005-06-27 2006-06-15 Verteilte Architektur eines Kontrollsystems eines Flugzeug-Fahrgestells

Country Status (8)

Country Link
US (1) US7369922B2 (de)
EP (1) EP1739010B1 (de)
CN (1) CN100497054C (de)
BR (1) BRPI0602357B1 (de)
CA (1) CA2550797C (de)
DE (1) DE602006001378D1 (de)
ES (1) ES2308694T3 (de)
FR (1) FR2887516B1 (de)

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US8064347B2 (en) * 2006-03-29 2011-11-22 Honeywell International Inc. System and method for redundant switched communications
US9656641B2 (en) † 2006-08-04 2017-05-23 The Boeing Company Aircraft electrical brake control system architecture
EP2162325B1 (de) * 2007-05-19 2010-10-27 Goodrich Corporation Flugzeugbremsen-steuerungsarchitektur mit verbesserter antirutsch-redundanz
GB0711922D0 (en) * 2007-06-20 2007-08-01 Goodrich Control Sys Ltd Control arrangement
GB0717903D0 (en) * 2007-09-14 2007-10-31 Airbus Uk Ltd Method and apparatus for providing power in an aircraft to one or more aircraft systems
FR2925017B1 (fr) * 2007-12-13 2010-01-15 Messier Bugatti Procede d'alimentation en energie d'actionneurs associes a un train d'atterrissage d'aeronef
US8175762B2 (en) * 2008-01-23 2012-05-08 The Boeing Company Electrically activated aircraft landing gear control system and method
DE102008011791B4 (de) * 2008-02-29 2013-09-19 Airbus Operations Gmbh Integriertes multifunktionales Radantriebssystem für Luftfahrzeuge
FR2932158B1 (fr) * 2008-06-04 2011-04-01 Messier Bugatti Circuit de freinage electrique muni de moyens pour commander les organes de blocage des poussoirs d'actionneurs electromecanique equipant un frein d'aeronef
FR2941311B1 (fr) * 2009-01-16 2012-10-26 Messier Bugatti Procede de gestion de la commande d'orientation d'un atterrisseur d'aeronef
FR2943037B1 (fr) * 2009-03-11 2012-09-21 Airbus France Systeme de commande d'aeronef a architecture modulaire integre.
FR2945647A1 (fr) * 2009-05-18 2010-11-19 Airbus France Methode d'optimisation d'une plateforme avionique
FR2945646B1 (fr) * 2009-05-18 2012-03-09 Airbus France Methode d'aide a la realisation et de validation d'une plateforme avionique
US8797842B2 (en) 2011-03-10 2014-08-05 The Boeing Company Aircraft communication bus fault isolator apparatus and method
FR2975376B1 (fr) * 2011-05-20 2018-03-30 Safran Landing Systems Procede pour alimenter des moteurs de deplacement autonome d'un aeronef.
FR2977864B1 (fr) * 2011-07-12 2013-08-09 Messier Bugatti Dowty Procede de gestion de l'orientation de roues d'aeronef, notamment en cas d'eclatement ou degonflement de pneumatiques
FR2981910B1 (fr) 2011-10-26 2013-12-27 Eurocopter France Atterrisseur, aeronef et procede
FR2984276B1 (fr) * 2011-12-15 2014-03-07 Messier Bugatti Dowty Procede de gestion de systemes lies au train d'atterrissage d'un aeronef.
US8964555B1 (en) 2012-06-26 2015-02-24 Rockwell Collins, Inc. Data network with constrained switch transmission rates
US8817622B1 (en) * 2012-06-26 2014-08-26 Rockwell Collins, Inc. Data network with aggregate flow monitoring
EP2727783B1 (de) 2012-11-06 2016-05-18 Airbus Defence and Space SA Bremssteuerungssystem und -verfahren
US9838436B2 (en) * 2015-03-30 2017-12-05 Gulfstream Aerospace Corporation Aircraft data networks
GB2540180A (en) 2015-07-08 2017-01-11 Airbus Operations Ltd Data processing unit for aircraft undercarriage performance monitoring
FR3044296B1 (fr) * 2015-12-01 2017-12-29 Messier Bugatti Dowty Architecture de systeme de freinage pour aeronoef.
US10155583B2 (en) 2016-10-14 2018-12-18 Goodrich Corporation Aircraft control system architecture
CN106742048B (zh) * 2016-11-18 2019-02-15 中航飞机起落架有限责任公司 一种飞机起落架系统rs422总线数据验证方法及装置
CN106672217A (zh) * 2016-12-15 2017-05-17 中国航空工业集团公司西安飞机设计研究所 一种飞机起落架控制系统架构
DE102017111527A1 (de) * 2017-05-26 2018-11-29 Liebherr-Aerospace Lindenberg Gmbh Flugsteuersystem
GB2563437A (en) 2017-06-16 2018-12-19 Airbus Operations Ltd Landing gear controller
GB2563851B (en) * 2017-06-27 2020-04-01 Airbus Operations Ltd Aircraft steering
CN107651173B (zh) * 2017-09-13 2020-05-19 西安航空制动科技有限公司 多余度电刹车机电驱动架构及刹车力控制方法
US11358710B2 (en) 2018-02-23 2022-06-14 The Boeing Company Methods and apparatus for controlling landing gear retract braking
US10933982B2 (en) * 2018-02-26 2021-03-02 The Boeing Company Methods and apparatus for controlling landing gear retract braking
FR3080880B1 (fr) * 2018-05-04 2020-09-04 Safran Landing Systems Dispositif de verrouillage a verrou rotatif a commande impulsionnelle
CN109850134B (zh) * 2019-02-25 2022-02-22 中国航空工业集团公司西安飞机设计研究所 一种飞机起落装置系统
CN110550191B (zh) * 2019-08-16 2022-11-22 西安飞机工业（集团）有限责任公司 一种飞机起落架位置指示机构及指示方法
US11440416B2 (en) 2020-02-28 2022-09-13 Safran Landing Systems Maglev supervisory control architecture
US11649041B2 (en) 2020-07-21 2023-05-16 Safran Landing Systems Methods for stable extension of landing gear systems
CN113525670B (zh) * 2021-07-29 2023-01-24 张丹 一种自适应起降-移动一体化起落架机器人
CN116176832B (zh) * 2023-05-04 2023-10-24 成都凯天电子股份有限公司 一种基于复杂起落架构型的收上和放下控制方法

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US2612331A (en) * 1947-03-19 1952-09-30 Robert L Frazier Automatic flight controller
US3904153A (en) * 1974-02-25 1975-09-09 Boeing Co Steerable and retractable aircraft nose landing gear assembly
US4228975A (en) * 1979-05-29 1980-10-21 The Boeing Company Kneeling nose landing gear assembly
FR2639319A1 (fr) * 1988-11-18 1990-05-25 Messier Hispano Sa Dispositif d'orientation d'un atterrisseur
JP3147539B2 (ja) * 1992-10-05 2001-03-19 本田技研工業株式会社 航空機の降着装置
US6003640A (en) * 1997-05-09 1999-12-21 The B.F. Goodrich Company Electronic braking system with brake wear measurement and running clearance adjustment
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US6390571B1 (en) * 2000-06-29 2002-05-21 Goodrich Corporation Redundant aircraft braking system architecture
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
US6755375B2 (en) * 2002-10-22 2004-06-29 The Boeing Company Method and apparatus for controlling aircraft devices with multiple actuators
US7128376B2 (en) * 2003-05-30 2006-10-31 Goodrich Corporation Redundant architecture for brake-by-wire system
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US7621481B2 (en) * 2004-09-03 2009-11-24 Lockheed-Martin Corporation Decoupled steering/planing air vehicle nose landing gear

Also Published As

Publication number Publication date
CA2550797C (fr) 2009-01-27
EP1739010B1 (de) 2008-06-04
US7369922B2 (en) 2008-05-06
CN100497054C (zh) 2009-06-10
ES2308694T3 (es) 2008-12-01
FR2887516B1 (fr) 2008-10-03
US20060293805A1 (en) 2006-12-28
BRPI0602357A (pt) 2007-02-21
FR2887516A1 (fr) 2006-12-29
CN1891544A (zh) 2007-01-10
BRPI0602357B1 (pt) 2018-07-10
CA2550797A1 (fr) 2006-12-27
EP1739010A1 (de) 2007-01-03

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