CA2659444C - Power interrupt management for an aircraft electric brake system - Google Patents

Power interrupt management for an aircraft electric brake system Download PDF

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Publication number
CA2659444C
CA2659444C CA2659444A CA2659444A CA2659444C CA 2659444 C CA2659444 C CA 2659444C CA 2659444 A CA2659444 A CA 2659444A CA 2659444 A CA2659444 A CA 2659444A CA 2659444 C CA2659444 C CA 2659444C
Authority
CA
Canada
Prior art keywords
electric brake
brake system
power
autobrake
interrupt condition
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
CA2659444A
Other languages
English (en)
French (fr)
Other versions
CA2659444A1 (en
Inventor
Todd T. Griffith
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to CA2745738A priority Critical patent/CA2745738C/en
Publication of CA2659444A1 publication Critical patent/CA2659444A1/en
Application granted granted Critical
Publication of CA2659444C publication Critical patent/CA2659444C/en
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
    • B60T8/17—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
    • 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
    • B60T2270/00—Further aspects of brake control systems not otherwise provided for
    • B60T2270/40—Failsafe aspects of brake control systems
    • B60T2270/414—Power supply failure

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Regulating Braking Force (AREA)
  • Braking Systems And Boosters (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
CA2659444A 2006-09-26 2007-08-24 Power interrupt management for an aircraft electric brake system Active CA2659444C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA2745738A CA2745738C (en) 2006-09-26 2007-08-24 Operating an aircraft electric brake system exposed to power interrupt conditions

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US11/535,449 2006-09-26
US11/535,449 US7784882B2 (en) 2006-09-26 2006-09-26 Power interrupt management for an aircraft electric brake system
PCT/US2007/018829 WO2008105821A2 (en) 2006-09-26 2007-08-24 Power interrupt management for an aircraft electric brake system

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CA2745738A Division CA2745738C (en) 2006-09-26 2007-08-24 Operating an aircraft electric brake system exposed to power interrupt conditions

Publications (2)

Publication Number Publication Date
CA2659444A1 CA2659444A1 (en) 2008-09-04
CA2659444C true CA2659444C (en) 2011-11-08

Family

ID=39224168

Family Applications (2)

Application Number Title Priority Date Filing Date
CA2659444A Active CA2659444C (en) 2006-09-26 2007-08-24 Power interrupt management for an aircraft electric brake system
CA2745738A Active CA2745738C (en) 2006-09-26 2007-08-24 Operating an aircraft electric brake system exposed to power interrupt conditions

Family Applications After (1)

Application Number Title Priority Date Filing Date
CA2745738A Active CA2745738C (en) 2006-09-26 2007-08-24 Operating an aircraft electric brake system exposed to power interrupt conditions

Country Status (9)

Country Link
US (1) US7784882B2 (enExample)
EP (2) EP2069170B1 (enExample)
JP (2) JP5330244B2 (enExample)
CN (1) CN101516695B (enExample)
AT (1) ATE486753T1 (enExample)
CA (2) CA2659444C (enExample)
DE (1) DE602007010328D1 (enExample)
ES (2) ES2424234T3 (enExample)
WO (1) WO2008105821A2 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8244428B2 (en) * 2006-05-10 2012-08-14 The Boeing Company Automatic fore-aft detection for an aircraft
US7784882B2 (en) * 2006-09-26 2010-08-31 The Boeing Company Power interrupt management for an aircraft electric brake system
US20100038188A1 (en) * 2006-10-24 2010-02-18 Goodrich Corporation Aircraft brake actuation measurement unit
US7857107B2 (en) * 2006-11-01 2010-12-28 The Boeing Company Ground towing power architecture for an electric brake system of an aircraft
DE102009046231A1 (de) * 2009-10-30 2011-05-05 Robert Bosch Gmbh Elektrisches Bremssystem, insbesondere elektromechanisches Bremssystem
US8423256B2 (en) * 2009-12-23 2013-04-16 Goodrich Corporation Systems and methods for adaptive deceleration
CN102092373B (zh) * 2010-12-16 2013-09-04 西安航空制动科技有限公司 一种飞机自动刹车方法及装置
US9811130B2 (en) 2011-09-12 2017-11-07 The Boeing Company Power management control system
EP2709230B1 (en) * 2012-09-12 2018-04-18 The Boeing Company Power management control system and method
EP2964501B1 (en) * 2013-03-06 2020-12-02 Airbus Canada Limited Partnership Electric braking system and method relying on voltage hysteresis for applied brake power control
JP6297883B2 (ja) * 2014-03-28 2018-03-20 マツダ株式会社 電動ブレーキ装置
US10308352B2 (en) * 2014-12-12 2019-06-04 Borealis Technical Limited Monitoring system for aircraft drive wheel system
GB2555834A (en) * 2016-11-11 2018-05-16 Airbus Operations Ltd Braking energy dissipation
FR3115014B1 (fr) * 2020-10-08 2024-04-26 Safran Landing Systems Architecture de freinage distribuée à sûreté améliorée

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1004A (en) * 1838-11-09 Abnee e
FR2608975B1 (fr) * 1986-12-26 1989-11-17 Messier Hispano Sa Dispositif de commande de freinage d'avion
JP2807837B2 (ja) * 1989-12-01 1998-10-08 日清紡績株式会社 アンチスキッド制御装置の故障検出回路
DE4117099A1 (de) * 1991-03-30 1992-10-01 Teves Gmbh Alfred Schaltungsanordnung fuer einen regler
DE4339570B4 (de) * 1993-11-19 2004-03-04 Robert Bosch Gmbh Elektronisches Bremssystem
US6003640A (en) 1997-05-09 1999-12-21 The B.F. Goodrich Company Electronic braking system with brake wear measurement and running clearance adjustment
WO1999026820A1 (de) * 1997-11-22 1999-06-03 Continental Teves Ag & Co. Ohg Elektromechanisches bremssystem
US6095293A (en) 1998-02-13 2000-08-01 The B. F. Goodrich Company Aircraft brake and method with electromechanical actuator modules
WO2000069721A1 (en) * 1999-05-14 2000-11-23 Hydro-Aire, Inc. Dual redundant active/active brake-by-wire architecture
US6513885B1 (en) * 1999-05-14 2003-02-04 Hydro-Aire, Inc. Dual redundant active/active brake-by-wire architecture
US6402259B2 (en) * 1999-07-14 2002-06-11 Goodrich Corporation Electromechanical braking system with power distribution and redundancy
JP3867268B2 (ja) * 2001-12-28 2007-01-10 株式会社日立製作所 電動ディスクブレーキ装置
FR2852144B1 (fr) 2003-03-05 2005-06-10 Commissariat Energie Atomique Procede de delimitation d'un element conducteur dispose sur une couche isolante, dispositif et transistor obtenus par ce procede
US7128376B2 (en) * 2003-05-30 2006-10-31 Goodrich Corporation Redundant architecture for brake-by-wire system
JP4715079B2 (ja) * 2003-06-26 2011-07-06 パナソニック株式会社 車両用電源装置
FR2857642B1 (fr) * 2003-07-16 2006-02-03 Messier Bugatti Dispositif de protection contre les freinages intempestifs specialement adapte a un frein electromecanique
US6984001B2 (en) * 2003-09-29 2006-01-10 Haldex Brake Products Ab Power supply network for brake system
US20060061210A1 (en) * 2004-09-17 2006-03-23 Mihai Ralea Electromechanical braking system with electrical energy back-up
FR2880602B1 (fr) * 2005-01-11 2007-03-16 Messier Bugatti Sa Procede de protection dans un systeme de freinage de vehicule a freins electriques
US7784882B2 (en) * 2006-09-26 2010-08-31 The Boeing Company Power interrupt management for an aircraft electric brake system

Also Published As

Publication number Publication date
EP2069170B1 (en) 2010-11-03
CA2745738C (en) 2014-03-18
US7784882B2 (en) 2010-08-31
ES2424234T3 (es) 2013-09-30
ES2353627T3 (es) 2011-03-03
CN101516695B (zh) 2012-09-05
EP2277752A1 (en) 2011-01-26
US20080073970A1 (en) 2008-03-27
CA2745738A1 (en) 2008-09-04
DE602007010328D1 (de) 2010-12-16
JP5643848B2 (ja) 2014-12-17
JP2010504875A (ja) 2010-02-18
EP2277752B1 (en) 2013-07-03
JP5330244B2 (ja) 2013-10-30
CA2659444A1 (en) 2008-09-04
CN101516695A (zh) 2009-08-26
EP2069170A2 (en) 2009-06-17
WO2008105821A2 (en) 2008-09-04
WO2008105821A3 (en) 2008-11-13
JP2013100097A (ja) 2013-05-23
ATE486753T1 (de) 2010-11-15

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