BRPI0405729A - Arquitetura de sistema de frenagem para aeronave e processo de gestão de uma arquitetura de sistema de frenagem para aeronave - Google Patents

Arquitetura de sistema de frenagem para aeronave e processo de gestão de uma arquitetura de sistema de frenagem para aeronave

Info

Publication number
BRPI0405729A
BRPI0405729A BR0405729-5A BRPI0405729A BRPI0405729A BR PI0405729 A BRPI0405729 A BR PI0405729A BR PI0405729 A BRPI0405729 A BR PI0405729A BR PI0405729 A BRPI0405729 A BR PI0405729A
Authority
BR
Brazil
Prior art keywords
system architecture
braking system
aircraft braking
managing
modules
Prior art date
Application number
BR0405729-5A
Other languages
English (en)
Inventor
Stephane Mallevais
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 BRPI0405729A publication Critical patent/BRPI0405729A/pt
Publication of BRPI0405729B1 publication Critical patent/BRPI0405729B1/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
    • 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
    • B60T2270/404—Brake-by-wire or X-by-wire failsafe
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
  • Multi Processors (AREA)
  • Hardware Redundancy (AREA)
  • Braking Systems And Boosters (AREA)

Abstract

"ARQUITETURA DE SISTEMA DE FRENAGEM PARA AERONAVE E PROCESSO DE GESTãO DE UMA ARQUITETURA DE SISTEMA DE FRENAGEM PARA AERONAVE". A invenção se refere a uma arquitetura para um sistema de frenagem para uma aeronave equipada com uma pluralidade de trens de aterragem, cada uma suportando uma pluralidade de rodas, das quais pelo menos algumas são equipadas com freios (1, 2, ..., 8), a arquitetura compreendendo pelo menos dois computadores de frenagem (A, B), cada um tendo dois módulos (A1, B4), de forma que, em cada computador um dos módulos (A1, B1) controla uma primeira fração dos freios (1, 4, 5, 8) e o outro módulo (A2, B2) controla uma segunda fração dos freios (2, 3, 6, 7) complementar à primeira. De acordo com a invenção, a arquitetura é configurada para operar em qualquer dos seguintes modos de operação:. um primeiro modo normal no qual ambos módulos (A1, A2) de um dos computadores de frenagem estão ativos para controlar todos os freios; . um segundo modo normal no qual ambos módulos (B1, B2) do outro computador de frenagem estão ativos para controlar todos os freios; e um modo alternativo no qual um módulo (A2) de um dos computadores de frenagem e um módulo (B1) do outro computador de frenagem estão ativos para controlar todos os freios.
BRPI0405729-5A 2003-12-22 2004-12-21 Arquitetura de sistema de frenagem para aeronave e processo de gestão de uma arquitetura de sistema de frenagem para aeronave BRPI0405729B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0315134A FR2864024B1 (fr) 2003-12-22 2003-12-22 Procede de gestion d'une architecture de systeme de freinage d'aeronef, et architecture de systeme de freinage faisant application
FR0315134 2003-12-22

Publications (2)

Publication Number Publication Date
BRPI0405729A true BRPI0405729A (pt) 2005-08-30
BRPI0405729B1 BRPI0405729B1 (pt) 2018-03-06

Family

ID=34531315

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0405729-5A BRPI0405729B1 (pt) 2003-12-22 2004-12-21 Arquitetura de sistema de frenagem para aeronave e processo de gestão de uma arquitetura de sistema de frenagem para aeronave

Country Status (8)

Country Link
US (1) US7401869B2 (pt)
EP (1) EP1547918B1 (pt)
AT (1) ATE356021T1 (pt)
BR (1) BRPI0405729B1 (pt)
CA (1) CA2491272C (pt)
DE (1) DE602004005143T2 (pt)
ES (1) ES2282825T3 (pt)
FR (1) FR2864024B1 (pt)

Families Citing this family (24)

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DE102005059423A1 (de) * 2005-12-13 2007-06-21 Airbus Deutschland Gmbh Verfahren und Einrichtung zur redundanten Versorgung von mehreren elektrischen Stell-oder Antriebsmotoren durch eine gemeinsame Leistungselektronikeinheit
US9656641B2 (en) * 2006-08-04 2017-05-23 The Boeing Company Aircraft electrical brake control system architecture
GB0623804D0 (en) * 2006-11-29 2007-01-10 Dunlop Aerospace Ltd A Braking system for an aircraft and a method of monitoring braking for an air
US7618100B2 (en) * 2006-12-13 2009-11-17 The Boeing Company Braking interlock for an electric brake system of an aircraft
US20080154470A1 (en) * 2006-12-21 2008-06-26 Goranson Pete T System and methods for an electric brake actuation overdrive feature in an aircraft electric brake system
US8204661B2 (en) * 2006-12-21 2012-06-19 The Boeing Company Reduced power mode for an aircraft electric brake system
EP1964741B1 (de) * 2007-02-28 2013-04-03 Robert Bosch Gmbh Elektrische Parkbremse
GB0705789D0 (en) * 2007-03-26 2007-05-02 Haldex Brake Products Ltd Vehicle braking system
US20080258548A1 (en) * 2007-04-18 2008-10-23 Bill May Aircraft brake control architecture having improved antiskid redundancy
EP2167357B1 (en) 2007-05-19 2016-03-30 Goodrich Corporation Independent brake control of a common aircraft landing gear
EP2090952A3 (de) * 2008-02-14 2012-03-28 Robert Bosch Gmbh Hydraulikkomponenten-Steuergerät und Verfahren zum Ansteuern von hydraulischen Komponenten
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
FR2952010B1 (fr) 2009-10-30 2011-11-25 Messier Bugatti Architecture d'alimentation de freins d'aeronef equipes d'actionneurs electromecaniques
FR2952009B1 (fr) 2009-10-30 2011-12-09 Messier Bugatti Architecture de systeme de freinage electromecanique
US20110226569A1 (en) * 2010-03-19 2011-09-22 Hydro-Aire, Inc. Electronic motor actuators brake inhibit for aircraft braking system
FR2996509B1 (fr) * 2012-10-09 2014-12-19 Messier Bugatti Dowty Architecture de systeme de freinage electromecanique.
US9527487B2 (en) * 2014-07-11 2016-12-27 Ford Global Technologies, Llc Failure tolerant vehicle speed
US10300896B2 (en) * 2016-10-10 2019-05-28 Textron Innovations, Inc. Brake system for aircraft
US10259569B2 (en) * 2016-10-17 2019-04-16 Goodrich Corporation Systems and methods for emergency aircraft brake operation
US9975627B2 (en) * 2016-10-18 2018-05-22 Goodrich Corporation Systems and methods for aircraft parking brakes with multiple control locations
US10829210B2 (en) * 2018-06-27 2020-11-10 The Boeing Company Braking system for a dual landing gear aircraft
FR3099461B1 (fr) * 2019-07-30 2021-08-13 Safran Landing Systems Dispositif de freinage d’une roue
CN112198903A (zh) * 2019-12-31 2021-01-08 北京理工大学 一种模块化的多功能机载计算机体系
FR3110126B1 (fr) * 2020-05-14 2022-06-17 Safran Landing Systems Equipement électrique de distribution de puissance pour système de freinage et de taxiage d’un aéronef et système de freinage et de taxiage d’un aéronef

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4807516A (en) * 1987-04-23 1989-02-28 The Boeing Company Flight control system employing three controllers operating a dual actuator
US5274554A (en) * 1991-02-01 1993-12-28 The Boeing Company Multiple-voting fault detection system for flight critical actuation control systems
DE19634567B4 (de) * 1996-08-27 2007-11-29 Robert Bosch Gmbh Elektrisches Bremssystem
US6513885B1 (en) * 1999-05-14 2003-02-04 Hydro-Aire, Inc. Dual redundant active/active brake-by-wire architecture
US6390571B1 (en) * 2000-06-29 2002-05-21 Goodrich Corporation Redundant aircraft braking system architecture

Also Published As

Publication number Publication date
CA2491272A1 (fr) 2005-06-22
EP1547918B1 (fr) 2007-03-07
CA2491272C (fr) 2010-01-26
FR2864024A1 (fr) 2005-06-24
FR2864024B1 (fr) 2006-04-07
DE602004005143T2 (de) 2007-11-15
ES2282825T3 (es) 2007-10-16
EP1547918A1 (fr) 2005-06-29
ATE356021T1 (de) 2007-03-15
US7401869B2 (en) 2008-07-22
DE602004005143D1 (de) 2007-04-19
US20050189814A1 (en) 2005-09-01
BRPI0405729B1 (pt) 2018-03-06

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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 020120020116/RJ DE 09/03/2012.

B07A Application suspended after technical examination (opinion) [chapter 7.1 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]
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 19A 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 2754 DE 17-10-2023 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.