PL3176655T3 - Układ uruchamiający do statku powietrznego - Google Patents

Układ uruchamiający do statku powietrznego

Info

Publication number
PL3176655T3
PL3176655T3 PL16201546T PL16201546T PL3176655T3 PL 3176655 T3 PL3176655 T3 PL 3176655T3 PL 16201546 T PL16201546 T PL 16201546T PL 16201546 T PL16201546 T PL 16201546T PL 3176655 T3 PL3176655 T3 PL 3176655T3
Authority
PL
Poland
Prior art keywords
aircraft
actuating system
actuating
Prior art date
Application number
PL16201546T
Other languages
English (en)
Inventor
Antoine MOUTAUX
Florent Nierlich
Original Assignee
Safran Landing Systems
Safran Helicopter Engines
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 Safran Landing Systems, Safran Helicopter Engines filed Critical Safran Landing Systems
Publication of PL3176655T3 publication Critical patent/PL3176655T3/pl

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P5/00—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B11/00—Automatic controllers
    • G05B11/01—Automatic controllers electric
    • 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
    • B64C25/24—Operating mechanisms electric
    • 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
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/68—Transmitting means, e.g. interrelated with initiating means or means acting on blades using electrical energy, e.g. having electrical power amplification
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B11/00—Automatic controllers
    • G05B11/01—Automatic controllers electric
    • G05B11/36—Automatic controllers electric with provision for obtaining particular characteristics, e.g. proportional, integral, differential
    • G05B11/42—Automatic controllers electric with provision for obtaining particular characteristics, e.g. proportional, integral, differential for obtaining a characteristic which is both proportional and time-dependent, e.g. P. I., P. I. D.
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/0205—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric not using a model or a simulator of the controlled system
    • G05B13/024—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric not using a model or a simulator of the controlled system in which a parameter or coefficient is automatically adjusted to optimise the performance
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D3/00—Control of position or direction
    • G05D3/12—Control of position or direction using feedback
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P5/00—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
    • H02P5/74—Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors controlling two or more ac dynamo-electric motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Artificial Intelligence (AREA)
  • Health & Medical Sciences (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Evolutionary Computation (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Power Engineering (AREA)
  • Control Of Electric Motors In General (AREA)
  • Braking Systems And Boosters (AREA)
  • Regulating Braking Force (AREA)
  • Braking Arrangements (AREA)
  • Safety Devices In Control Systems (AREA)
PL16201546T 2015-12-01 2016-11-30 Układ uruchamiający do statku powietrznego PL3176655T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1561679A FR3044432B1 (fr) 2015-12-01 2015-12-01 Systeme d'actionnement pour aeronef.
EP16201546.5A EP3176655B1 (fr) 2015-12-01 2016-11-30 Systeme d'actionnement pour aeronef

Publications (1)

Publication Number Publication Date
PL3176655T3 true PL3176655T3 (pl) 2021-01-11

Family

ID=56101501

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16201546T PL3176655T3 (pl) 2015-12-01 2016-11-30 Układ uruchamiający do statku powietrznego

Country Status (9)

Country Link
US (1) US10023303B2 (pl)
EP (1) EP3176655B1 (pl)
JP (1) JP6462647B2 (pl)
KR (1) KR101913169B1 (pl)
CN (1) CN106849762B (pl)
CA (1) CA2949963C (pl)
FR (1) FR3044432B1 (pl)
PL (1) PL3176655T3 (pl)
RU (1) RU2664025C2 (pl)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3073203B1 (fr) * 2017-11-08 2019-12-13 Safran Landing Systems Architecture de systeme de freinage pour aeronef
KR102631522B1 (ko) * 2017-12-08 2024-01-31 에어로 컨트롤렉스 그룹 인코포레이티드 드래그 브레이크를 갖는 블로우 다운 액추에이터 조립체
FR3075491B1 (fr) * 2017-12-14 2019-12-20 Safran Landing Systems Harnais electrique
US10549864B2 (en) * 2018-05-07 2020-02-04 Hamilton Sundstrand Corporation RFID actuator over-torque indicator
KR102093784B1 (ko) * 2018-08-13 2020-03-26 한국항공우주산업 주식회사 항공기 액추에이터 구동용 스위칭 장치 및 이의 스위칭 방법
FR3099461B1 (fr) 2019-07-30 2021-08-13 Safran Landing Systems Dispositif de freinage d’une roue
FR3104190B1 (fr) * 2019-12-09 2021-12-24 Somfy Activites Sa Procédé de pilotage d’un actionneur, actionneur électromécanique et installation de fermeture, d’occultation ou de protection solaire associés
US11428247B2 (en) 2020-02-07 2022-08-30 Woodward, Inc. Electro-hydraulic servovalve control with input
US11472539B2 (en) 2020-03-05 2022-10-18 Goodrich Corporation Distributed landing gear system architecture for electromechanical actuation
CN113753223A (zh) * 2020-06-02 2021-12-07 北京航天易联科技发展有限公司 一种起落架的控制方法及装置、电子设备、存储介质
US11346377B2 (en) 2020-08-24 2022-05-31 Epiroc Drilling Solutions, Llc System and method for automatic calibration of actuators
US11796990B2 (en) 2021-08-24 2023-10-24 Woodward, Inc. Model based monitoring of faults in electro-hydraulic valves
KR102696190B1 (ko) * 2022-10-19 2024-08-19 주식회사 이노템즈 단일통로항공기 전륜 조향용 전기식 작동장치의 모니터링 시스템

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5248922A (en) * 1992-04-27 1993-09-28 Motion Control Technologies, Inc. Multi-DSP, multi-functional motion controller
RU2066873C1 (ru) * 1992-05-21 1996-09-20 Андрей Николаевич Семенюк Электромеханический привод с тормозным устройством
US6003640A (en) * 1997-05-09 1999-12-21 The B.F. Goodrich Company Electronic braking system with brake wear measurement and running clearance adjustment
US6658370B2 (en) * 2001-08-15 2003-12-02 Pitney Bowes Inc. Adaptive servo motor retuning method and system
US7437201B2 (en) * 2003-01-14 2008-10-14 Cullen Christopher P Electric motor controller
US7166982B2 (en) * 2003-10-15 2007-01-23 International Rectifier Corporation Hardware based configurable motion control apparatus and method
JP2006136166A (ja) * 2004-11-09 2006-05-25 Matsushita Electric Ind Co Ltd 電動機の運転制御装置
EP1977297A4 (en) * 2006-01-17 2010-02-24 Gulfstream Aerospace Corp APPARATUS AND METHOD FOR CONTROLLING RELIEF USED IN DISTRIBUTED FLIGHT CONTROL SYSTEM
JP5037823B2 (ja) * 2006-01-18 2012-10-03 マックス株式会社 電動装置システム
US8080966B2 (en) * 2008-07-03 2011-12-20 Honeywell International Inc. Motor control architecture for simultaneously controlling multiple motors
FR2972712B1 (fr) * 2011-03-16 2014-09-05 Airbus Operations Sas Surveillance d'un actionneur de commande de vol d'un aeronef
JP2012206696A (ja) * 2011-03-30 2012-10-25 Mitsubishi Heavy Ind Ltd アクチュエータ監視システム
US9209721B2 (en) * 2014-04-29 2015-12-08 The Boeing Company Systems and methods for the control and operation of a parallel motor controller architecture

Also Published As

Publication number Publication date
US20170152022A1 (en) 2017-06-01
CA2949963C (fr) 2020-03-24
JP6462647B2 (ja) 2019-01-30
RU2016147088A (ru) 2018-05-30
KR20170064491A (ko) 2017-06-09
RU2016147088A3 (pl) 2018-05-30
JP2017100712A (ja) 2017-06-08
CN106849762A (zh) 2017-06-13
CA2949963A1 (fr) 2017-06-01
EP3176655A1 (fr) 2017-06-07
EP3176655B1 (fr) 2020-09-09
FR3044432A1 (fr) 2017-06-02
FR3044432B1 (fr) 2017-12-29
CN106849762B (zh) 2020-06-05
RU2664025C2 (ru) 2018-08-14
KR101913169B1 (ko) 2018-10-30
US10023303B2 (en) 2018-07-17

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