BR0105151A - Arquitetura para um sistema hidráulico de frenagem adequado para uma aeronave - Google Patents

Arquitetura para um sistema hidráulico de frenagem adequado para uma aeronave

Info

Publication number
BR0105151A
BR0105151A BR0105151-2A BR0105151A BR0105151A BR 0105151 A BR0105151 A BR 0105151A BR 0105151 A BR0105151 A BR 0105151A BR 0105151 A BR0105151 A BR 0105151A
Authority
BR
Brazil
Prior art keywords
brakes
circuit
architecture
aircraft
braking system
Prior art date
Application number
BR0105151-2A
Other languages
English (en)
Other versions
BR0105151B1 (pt
Inventor
Vincent Bourguet
Walid Hamzeh
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 BR0105151A publication Critical patent/BR0105151A/pt
Publication of BR0105151B1 publication Critical patent/BR0105151B1/pt

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 
    • B64C25/42—Arrangement or adaptation of brakes
    • 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
    • B60T13/00—Transmitting braking action from initiating means to ultimate brake actuator with power assistance or drive; Brake systems incorporating such transmitting means, e.g. air-pressure brake systems
    • B60T13/10—Transmitting braking action from initiating means to ultimate brake actuator with power assistance or drive; Brake systems incorporating such transmitting means, e.g. air-pressure brake systems with fluid assistance, drive, or release
    • B60T13/66—Electrical control in fluid-pressure brake systems
    • B60T13/68—Electrical control in fluid-pressure brake systems by electrically-controlled valves
    • B60T13/686—Electrical control in fluid-pressure brake systems by electrically-controlled valves in hydraulic systems or parts thereof
    • 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
    • B60T17/00—Component parts, details, or accessories of power brake systems not covered by groups B60T8/00, B60T13/00 or B60T15/00, or presenting other characteristic features
    • B60T17/18—Safety devices; Monitoring
    • 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
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/44—Actuating mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
  • Braking Systems And Boosters (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Braking Arrangements (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
  • Transmission Of Braking Force In Braking Systems (AREA)
  • Regulating Braking Force (AREA)

Abstract

"ARQUITETURA PARA UM SISTEMA HIDRáULICO DE FRENAGEM ADEQUADO PARA UMA AERONAVE". A invenção se refere a uma arquitetura para um sistema hidráulico de frenagem uma aeronave do tipo que tem ao menos um grupo (G) de unidades de trem de pouso principal (I, II), cada unidade de trem de pouso principal (I, II) compreendendo um número determinado de rodas, cada uma provida de um freio hidraulicamente atuado ( 9a... 9d, 109a... 109d, 209a... 209d), o grupo (G) de unidades de trem de pouso principal, ou cada um deles, sendo associado a um circuito hidráulico (C) provido de equipamentos hidráulicos e adaptado para conduzir fluido hidráulico sob pressão para todos os freios ( 9a... 9d, 109a... 109d,209a... 209d ) do grupo de trem de pouso, o fluido hidráulico sendo pressurizado por ao menos um sistema gerador de pressão (50) da aeronave associado a um sistema de suprimento de fluido hidráulico da aeronave. De acordo com a invenção os acumuladores (5, 105, 205) são conectados ao circuito (C), ou a cada um, em um número suficiente de acumuladores para alimentar dois pares de freio ( I. 1 e II 1, I.2 e II.2. I.3 e II.3 ), cada par de freio sendo montado em uma unidade de trem de pouso distinta (I e II), e uma bomba acionada eletricamente (30, 31) é disposta para manter um nível de pressão predeterminado em todos os acumuladores (5, 105, 205) do circuito (C) em questão.
BRPI0105151-2A 2000-11-10 2001-11-09 arquitetura para um sistema hidráulico de frenagem adequado para uma aeronave. BR0105151B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0014447A FR2816583B1 (fr) 2000-11-10 2000-11-10 Architecture de systeme hydraulique de freinage d'aeronef

Publications (2)

Publication Number Publication Date
BR0105151A true BR0105151A (pt) 2002-06-25
BR0105151B1 BR0105151B1 (pt) 2011-11-16

Family

ID=8856286

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0105151-2A BR0105151B1 (pt) 2000-11-10 2001-11-09 arquitetura para um sistema hidráulico de frenagem adequado para uma aeronave.

Country Status (9)

Country Link
US (1) US6663192B2 (pt)
EP (1) EP1205369B1 (pt)
JP (1) JP4327390B2 (pt)
AT (1) ATE382524T1 (pt)
BR (1) BR0105151B1 (pt)
CA (1) CA2361607C (pt)
DE (1) DE60132154T2 (pt)
ES (1) ES2298209T3 (pt)
FR (1) FR2816583B1 (pt)

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EP1339582A1 (de) * 2000-11-27 2003-09-03 Continental Teves AG & Co. oHG Verfahren zur steuerung einer elektrohydraulischen bremsanlage
FR2827346B1 (fr) * 2001-07-12 2003-12-26 Messier Bugatti Architecture de circuit hydraulique
US6704634B1 (en) * 2002-11-06 2004-03-09 The Boeing Company Gear retract braking system and method
FR2869015B1 (fr) * 2004-04-16 2006-06-30 Airbus France Sas Procede et dispositif pour la conduite et le freinage d'un aeronef roulant sur le sol.
US7281684B2 (en) * 2005-02-23 2007-10-16 The Boeing Company Systems and methods for braking aircraft, including braking intermediate main gears and differential braking
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
US8038094B2 (en) * 2008-03-31 2011-10-18 Honda Motor Co., Ltd. Hydraulic system for aircraft
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
FR2946320B1 (fr) * 2009-06-09 2011-07-29 Messier Bugatti Architecture de systeme de freinage pour aeronef equipe de freins electromecaniques.
US8544964B2 (en) * 2010-06-29 2013-10-01 Deere & Company Brake control system for dual mode vehicle
US9481452B2 (en) * 2010-11-22 2016-11-01 The Boeing Company Hydraulic actuator for semi levered landing gear
US8939400B2 (en) 2011-02-21 2015-01-27 The Boeing Company Air-ground detection system for semi-levered landing gear
FR2972176B1 (fr) * 2011-03-04 2014-03-07 Messier Bugatti Architectures de freinage hydraulique pour aeronef permettant de freiner au moins une roue de l'aeronef.
FR2982240B1 (fr) * 2011-11-09 2013-12-13 Messier Bugatti Dowty Procede de deploiement d'atterrisseurs d'aeronef en mode secours.
CN104340362B (zh) * 2013-08-05 2016-09-14 哈尔滨飞机工业集团有限责任公司 飞机液压教练刹车系统
CN103786877B (zh) * 2014-01-26 2016-01-13 北京航空航天大学 基于自馈能式刹车装置的多轮飞机刹车系统及其控制方法
US9650130B2 (en) * 2014-03-24 2017-05-16 Mohammed Bouzmane Electric hydraulic motor system for aircraft
CN104787310B (zh) * 2015-04-01 2016-10-26 西安航空制动科技有限公司 一种具有起飞线刹车能力的飞机正常刹车系统
KR101806896B1 (ko) 2016-04-11 2017-12-08 국방과학연구소 공극 조정 기능을 가지는 유압식 제동장치
CN108284947B (zh) * 2017-12-13 2021-11-02 中航(成都)无人机系统股份有限公司 一种基于蓄压储能的飞机刹车系统
ES2903159T3 (es) * 2017-12-28 2022-03-31 Safran Landing Systems Uk Ltd Montaje de aeronave
GB2571100A (en) * 2018-02-15 2019-08-21 Airbus Operations Ltd Controller for an aircraft braking system
FR3080880B1 (fr) * 2018-05-04 2020-09-04 Safran Landing Systems Dispositif de verrouillage a verrou rotatif a commande impulsionnelle
US10829210B2 (en) * 2018-06-27 2020-11-10 The Boeing Company Braking system for a dual landing gear aircraft
US10703464B2 (en) 2018-07-12 2020-07-07 Goodrich Corporation Architecture for locked wheel and antiskid performance
US11867206B2 (en) 2019-10-15 2024-01-09 Airbus Operations Limited Method of removing hydraulic fluid from an aircraft hydraulic system, an aircraft hydraulic system, and an aircraft
CN112224391A (zh) * 2020-10-12 2021-01-15 四川航天烽火伺服控制技术有限公司 一种刹车装置及系统
GB2602157A (en) * 2020-12-21 2022-06-22 Airbus Operations Ltd Braking system
EP4086169A1 (en) * 2021-05-06 2022-11-09 Safran Landing Systems Canada Inc. Aircraft braking system
GB2611518A (en) * 2021-09-30 2023-04-12 Airbus Operations Ltd Aircraft hydraulic braking system and method of controlling same

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FR2480217A1 (fr) * 1980-04-11 1981-10-16 Labavia Perfectionnements aux dispositifs de commande des ralentisseurs
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FR2702447B1 (fr) * 1993-03-08 1995-04-28 Messier Bugatti Dispositif de freinage électro-hydraulique d'un train de roues d'aéronef.
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FR2773530B1 (fr) * 1998-01-12 2000-02-11 Messier Bugatti Dispositif de freinage d'un train de roues d'aeronef
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Also Published As

Publication number Publication date
BR0105151B1 (pt) 2011-11-16
JP4327390B2 (ja) 2009-09-09
ATE382524T1 (de) 2008-01-15
US20020057012A1 (en) 2002-05-16
EP1205369A1 (fr) 2002-05-15
FR2816583B1 (fr) 2003-02-21
ES2298209T3 (es) 2008-05-16
DE60132154D1 (de) 2008-02-14
FR2816583A1 (fr) 2002-05-17
JP2002200976A (ja) 2002-07-16
EP1205369B1 (fr) 2008-01-02
CA2361607C (fr) 2005-10-04
CA2361607A1 (fr) 2002-05-10
DE60132154T2 (de) 2008-12-18
US6663192B2 (en) 2003-12-16

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Legal Events

Date Code Title Description
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]

Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 16/11/2011, OBSERVADAS AS CONDICOES LEGAIS.

B25D Requested change of name of applicant approved

Free format text: NOME ALTERADO DE: MESSIER-BUGATTI

B25G Requested change of headquarter approved

Free format text: ENDERECO ALTERADO CONFORME SOLICITADO NA PETICAO NO 020120020138/RJ DE 09/03/2012.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 14A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2342 DE 24-11-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.