JP2010514606A5 - - Google Patents
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- Publication number
- JP2010514606A5 JP2010514606A5 JP2009543239A JP2009543239A JP2010514606A5 JP 2010514606 A5 JP2010514606 A5 JP 2010514606A5 JP 2009543239 A JP2009543239 A JP 2009543239A JP 2009543239 A JP2009543239 A JP 2009543239A JP 2010514606 A5 JP2010514606 A5 JP 2010514606A5
- Authority
- JP
- Japan
- Prior art keywords
- brake system
- electric brake
- power mode
- operating
- performance
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 claims 9
- 230000001419 dependent effect Effects 0.000 claims 1
- 230000004044 response Effects 0.000 claims 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/614,953 US8204661B2 (en) | 2006-12-21 | 2006-12-21 | Reduced power mode for an aircraft electric brake system |
| US11/614,953 | 2006-12-21 | ||
| PCT/US2007/088461 WO2008080026A2 (en) | 2006-12-21 | 2007-12-20 | Reduced power mode for an aircraft electric brake system |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2010514606A JP2010514606A (ja) | 2010-05-06 |
| JP2010514606A5 true JP2010514606A5 (enExample) | 2011-02-03 |
| JP5184549B2 JP5184549B2 (ja) | 2013-04-17 |
Family
ID=39473922
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2009543239A Active JP5184549B2 (ja) | 2006-12-21 | 2007-12-20 | 航空機電気ブレーキシステムのための減少電力モード |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US8204661B2 (enExample) |
| EP (1) | EP2094549B1 (enExample) |
| JP (1) | JP5184549B2 (enExample) |
| CN (1) | CN101568458A (enExample) |
| CA (1) | CA2665622C (enExample) |
| ES (1) | ES2608052T3 (enExample) |
| WO (1) | WO2008080026A2 (enExample) |
Families Citing this family (23)
| 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 |
| US8641154B2 (en) * | 2006-10-09 | 2014-02-04 | The Boeing Company | Parking brake adjustment for an aircraft having an electric brake system |
| DE102008016132A1 (de) * | 2008-03-28 | 2009-10-01 | Continental Automotive Gmbh | Elektronisches Erfassen von manuellen Verstellungen einer elektrischen Parkbremse |
| US9227608B2 (en) * | 2009-08-12 | 2016-01-05 | Meggitt Aircraft Braking Systems | Decentralized electric brake system |
| FR2952010B1 (fr) * | 2009-10-30 | 2011-11-25 | Messier Bugatti | Architecture d'alimentation de freins d'aeronef equipes d'actionneurs electromecaniques |
| US20110226569A1 (en) * | 2010-03-19 | 2011-09-22 | Hydro-Aire, Inc. | Electronic motor actuators brake inhibit for aircraft braking system |
| DE102011088350A1 (de) | 2011-12-13 | 2013-06-13 | Robert Bosch Gmbh | Weckvorrichtung für eine Bremssystemkomponente eines Fahrzeugs und Verfahren zum Wecken mindestens einer Bremssystemkomponente eines Fahrzeugs |
| FR2984276B1 (fr) * | 2011-12-15 | 2014-03-07 | Messier Bugatti Dowty | Procede de gestion de systemes lies au train d'atterrissage d'un aeronef. |
| WO2014135946A1 (en) * | 2013-03-06 | 2014-09-12 | Bombardier Inc. | Electric braking system with power conservation and method of operating the same |
| 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 |
| CN104709463B (zh) * | 2015-02-05 | 2016-11-09 | 中电科(德阳广汉)特种飞机系统工程有限公司 | 一种主起落架控制方法及装置 |
| CN104808491B (zh) * | 2015-03-17 | 2018-02-27 | 南京航空航天大学 | 基于能量特征的多电飞机机电作动器建模方法及其模型 |
| GB2538081B (en) * | 2015-05-06 | 2017-08-16 | Rolls Royce Plc | Apparatus and methods for controlling velocity of aircraft during landing roll-out and/or taxiing |
| US9783171B2 (en) | 2015-07-02 | 2017-10-10 | Goodrich Corporation | Electromechanical braking systems and methods with power demand control |
| US10876329B2 (en) * | 2015-10-16 | 2020-12-29 | Magna Closures S.P.A. | Electrical door latch |
| US10507816B2 (en) * | 2016-08-30 | 2019-12-17 | GM Global Technology Operations LLC | Brake-by-wire system |
| US10259569B2 (en) * | 2016-10-17 | 2019-04-16 | Goodrich Corporation | Systems and methods for emergency aircraft brake operation |
| GB2555834A (en) * | 2016-11-11 | 2018-05-16 | Airbus Operations Ltd | Braking energy dissipation |
| US10435005B2 (en) * | 2017-05-31 | 2019-10-08 | Simmonds Precision Products, Inc. | Electro-mechanical braking monitoring systems and methods |
| JP6885843B2 (ja) * | 2017-10-24 | 2021-06-16 | 株式会社シマノ | ブレーキシステム |
| CN110673640B (zh) * | 2019-10-21 | 2022-02-08 | 深圳市道通智能航空技术股份有限公司 | 一种无人机控制方法、装置、设备和存储介质 |
| GB2604604A (en) | 2021-03-08 | 2022-09-14 | Airbus Operations Ltd | An aircraft brake control system |
| CN113895415B (zh) * | 2021-09-13 | 2023-08-18 | 西安航空制动科技有限公司 | 一种飞机机轮刹车系统工作模式转换方法 |
Family Cites Families (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4986610A (en) * | 1989-02-21 | 1991-01-22 | Aircraft Braking Systems Corporation | Brake system with brake selection means |
| FR2701006B1 (fr) * | 1993-02-01 | 1995-03-10 | Messier Bugatti | Procédé de pilotage d'un dispositif de freinage électro-hydraulique d'un train de roues d'aéronef, et dispositif de mise en Óoeuvre dudit procédé. |
| EP0686106B1 (en) * | 1993-03-06 | 1998-11-18 | Dunlop Limited | Sequential selective operation of aircraft brakes |
| JP3612091B2 (ja) * | 1994-08-08 | 2005-01-19 | 曙ブレーキ工業株式会社 | 車両用停止維持装置 |
| US6003640A (en) * | 1997-05-09 | 1999-12-21 | The B.F. Goodrich Company | Electronic braking system with brake wear measurement and running clearance adjustment |
| US6095293A (en) * | 1998-02-13 | 2000-08-01 | The B. F. Goodrich Company | Aircraft brake and method with electromechanical actuator modules |
| US6913326B1 (en) * | 1998-08-28 | 2005-07-05 | Toyota Jidosha Kabushiki Kaisha | Apparatus for increasing brake cylinder pressure by controlling pump motor and reducing the pressure by controlling electric energy applied to control valve |
| US6183051B1 (en) * | 1999-02-01 | 2001-02-06 | Aircraft Braking Systems Corp. | Fail safe electrical brake control system for aircraft |
| 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 |
| US6530625B2 (en) * | 1999-08-27 | 2003-03-11 | Alliedsignal Inc. | Electrically actuated brake with vibration damping |
| US20050173980A1 (en) * | 2000-10-24 | 2005-08-11 | Continental Teves Ag & Co. Ohg | Method and device for controlling or regulating the brake system of a motor vehicle according to the "brake by wire" principle |
| JP2002154414A (ja) * | 2000-11-20 | 2002-05-28 | Bosch Braking Systems Co Ltd | 電気駆動ブレーキ装置 |
| JP2003097612A (ja) * | 2001-09-25 | 2003-04-03 | Aisin Seiki Co Ltd | 電動駐車ブレーキ装置 |
| US7128376B2 (en) * | 2003-05-30 | 2006-10-31 | Goodrich Corporation | Redundant architecture for brake-by-wire system |
| JP2005117759A (ja) * | 2003-10-06 | 2005-04-28 | Sumitomo Electric Ind Ltd | 車載システム |
| FR2862942B1 (fr) * | 2003-12-01 | 2006-03-03 | Messier Bugatti | Procede de gestion d'une architecture de systeme de freinage pour aeronef equipe de freins a actionneurs electromecaniques, et architecture faisant application |
| FR2864024B1 (fr) * | 2003-12-22 | 2006-04-07 | Messier Bugatti | Procede de gestion d'une architecture de systeme de freinage d'aeronef, et architecture de systeme de freinage faisant application |
| JP4333443B2 (ja) * | 2004-03-30 | 2009-09-16 | トヨタ自動車株式会社 | 電動ブレーキ制御装置 |
| US7317981B2 (en) * | 2004-11-19 | 2008-01-08 | Honeywell International, Inc. | Aircraft brake actuation system and method including anti-hysteresis control |
| US7410224B2 (en) * | 2006-01-19 | 2008-08-12 | Hydro-Aire, Inc. | Method and system to increase electric brake clamping force accuracy |
| WO2007088461A1 (en) | 2006-02-02 | 2007-08-09 | Element Six (Production) (Proprietary) Limited | Glass coated hard and ultra-hard abrasive particles and a method of making them |
| US20070284939A1 (en) * | 2006-06-12 | 2007-12-13 | Honeywell International | Aircraft electric brake and generator therefor |
| US9656641B2 (en) * | 2006-08-04 | 2017-05-23 | The Boeing Company | Aircraft electrical brake control system architecture |
| US7766431B2 (en) * | 2006-12-22 | 2010-08-03 | The Boeing Company | System and method for an autobrake function for an aircraft electric brake system |
-
2006
- 2006-12-21 US US11/614,953 patent/US8204661B2/en active Active
-
2007
- 2007-12-20 JP JP2009543239A patent/JP5184549B2/ja active Active
- 2007-12-20 WO PCT/US2007/088461 patent/WO2008080026A2/en not_active Ceased
- 2007-12-20 ES ES07865943.0T patent/ES2608052T3/es active Active
- 2007-12-20 EP EP07865943.0A patent/EP2094549B1/en active Active
- 2007-12-20 CN CNA2007800476247A patent/CN101568458A/zh active Pending
- 2007-12-20 CA CA2665622A patent/CA2665622C/en active Active
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