BRPI0602357A - arquitetura de sistema para comandar trem de pouso de aeronave - Google Patents

arquitetura de sistema para comandar trem de pouso de aeronave

Info

Publication number
BRPI0602357A
BRPI0602357A BRPI0602357-6A BRPI0602357A BRPI0602357A BR PI0602357 A BRPI0602357 A BR PI0602357A BR PI0602357 A BRPI0602357 A BR PI0602357A BR PI0602357 A BRPI0602357 A BR PI0602357A
Authority
BR
Brazil
Prior art keywords
landing gear
system architecture
actuators
control
aircraft landing
Prior art date
Application number
BRPI0602357-6A
Other languages
English (en)
Inventor
Jean-Pierre Garcia
Original Assignee
Messier Bugatti
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 filed Critical Messier Bugatti
Publication of BRPI0602357A publication Critical patent/BRPI0602357A/pt
Publication of BRPI0602357B1 publication Critical patent/BRPI0602357B1/pt

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)

Abstract

"ARQUITETURA DE SISTEMA PARA COMANDAR TREM DE POUSO DE AERONAVE". A invenção relaciona-se a uma arquitetura de sistema para comandar trem de pouso de aeronave e adequada para extensão/retração de trens de pouso retráteis, esterçamento de rodas esterçáveis, e frenagem de rodas com freio. De acordo com a invenção, a arquitetura compreende uma rede de comunicações (A; B) tendo conectada a ela atuadores de extensão/retração, atuadores de direcionamento, e atuadores de frenagem, juntamente com uma ou mais unidades de controle adaptadas para controlar todos os atuadores conectados a elas, a rede de comunicações tendo características de transmissão que são adaptadas para habilitar a(s) unidade(s) de controle a implementar servo controle anti-travamento para controlar os atuadores de frenagem.
BRPI0602357-6A 2005-06-27 2006-06-26 Arquitetura de sistema para comandar trem de pouso de aeronave BRPI0602357B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0506498 2005-06-27
FR0506498A FR2887516B1 (fr) 2005-06-27 2005-06-27 Architecture distribuee de systeme de gestion d'atterisseurs d'aeronef

Publications (2)

Publication Number Publication Date
BRPI0602357A true BRPI0602357A (pt) 2007-02-21
BRPI0602357B1 BRPI0602357B1 (pt) 2018-07-10

Family

ID=35645798

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0602357-6A BRPI0602357B1 (pt) 2005-06-27 2006-06-26 Arquitetura de sistema para comandar trem de pouso de aeronave

Country Status (8)

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

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US9656641B2 (en) † 2006-08-04 2017-05-23 The Boeing Company Aircraft electrical brake control system architecture
ATE485981T1 (de) * 2007-05-19 2010-11-15 Goodrich Corp Flugzeugbremsen-steuerungsarchitektur mit verbesserter antirutsch-redundanz
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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.
US8817622B1 (en) * 2012-06-26 2014-08-26 Rockwell Collins, Inc. Data network with aggregate flow monitoring
US8964555B1 (en) 2012-06-26 2015-02-24 Rockwell Collins, Inc. Data network with constrained switch transmission rates
EP2727783B1 (en) * 2012-11-06 2016-05-18 Airbus Defence and Space SA Braking control system and method
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
CN119262330B (zh) * 2024-11-15 2025-08-05 南京航空航天大学 一种基于虚实交互的飞行器地面滑跑刹车试验系统

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Also Published As

Publication number Publication date
DE602006001378D1 (de) 2008-07-17
FR2887516A1 (fr) 2006-12-29
EP1739010B1 (fr) 2008-06-04
US7369922B2 (en) 2008-05-06
BRPI0602357B1 (pt) 2018-07-10
EP1739010A1 (fr) 2007-01-03
US20060293805A1 (en) 2006-12-28
CN1891544A (zh) 2007-01-10
CA2550797A1 (fr) 2006-12-27
ES2308694T3 (es) 2008-12-01
FR2887516B1 (fr) 2008-10-03
CN100497054C (zh) 2009-06-10
CA2550797C (fr) 2009-01-27

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: MESSIER-BUGATTI-DOWTY (FR)

Free format text: NOME ALTERADO DE: MESSIER-BUGATTI

B25G Requested change of headquarter approved

Owner name: MESSIER-BUGATTI-DOWTY (FR)

Free format text: ENDERECO ALTERADO CONFORME SOLICITADO NA PETICAO NO 020120020098/RJ DE 09/03/2012.

B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]