FR3057681B1 - Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef - Google Patents

Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef Download PDF

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Publication number
FR3057681B1
FR3057681B1 FR1659926A FR1659926A FR3057681B1 FR 3057681 B1 FR3057681 B1 FR 3057681B1 FR 1659926 A FR1659926 A FR 1659926A FR 1659926 A FR1659926 A FR 1659926A FR 3057681 B1 FR3057681 B1 FR 3057681B1
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FR
France
Prior art keywords
aircraft
control
board
electrically controlled
power
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
FR1659926A
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English (en)
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FR3057681A1 (fr
Inventor
Florent Nierlich
Jean-Pierre Garcia
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.)
Safran Electrical and Power SAS
Original Assignee
Safran Electrical and Power SAS
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 Electrical and Power SAS filed Critical Safran Electrical and Power SAS
Priority to FR1659926A priority Critical patent/FR3057681B1/fr
Priority to PCT/FR2017/052784 priority patent/WO2018069637A1/fr
Priority to US16/340,842 priority patent/US20190263533A1/en
Publication of FR3057681A1 publication Critical patent/FR3057681A1/fr
Application granted granted Critical
Publication of FR3057681B1 publication Critical patent/FR3057681B1/fr
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Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • 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
    • 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
    • G05B19/00—Programme-control systems
    • G05B19/02—Programme-control systems electric
    • G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
    • G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
    • G05B19/0423—Input/output
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H1/00—Details of emergency protective circuit arrangements
    • H02H1/0007—Details of emergency protective circuit arrangements concerning the detecting means
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
    • H02H7/20—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for electronic equipment
    • 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
    • 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
    • H02P6/00—Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/04—Arrangements for controlling or regulating the speed or torque of more than one motor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/25—Pc structure of the system
    • G05B2219/25022—LAN local area network for controllers
    • 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
    • G05B2219/00—Program-control systems
    • G05B2219/20—Pc systems
    • G05B2219/26—Pc applications
    • G05B2219/2637—Vehicle, car, auto, wheelchair
    • 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
    • H02P2101/00—Special adaptation of control arrangements for generators
    • H02P2101/30—Special adaptation of control arrangements for generators for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Multiple Motors (AREA)

Abstract

L'invention se situe dans le domaine de l'alimentation et de la commande d'actionneurs électriques (32A, 32B, 32C) embarqués dans un aéronef. Elle concerne en particulier un système d'alimentation et de commande (31) d'une pluralité d'actionneurs à commande électrique embarqués dans un aéronef ainsi qu'un système d'actionnement (30) pour un aéronef comprenant lesdits actionneurs à commande électrique et un système pour leur alimentation et leur commande. Selon l'invention, le système (31) comprend : ▪ P unités d'alimentation électrique (312A, 312B, 312C) chacune apte à générer un signal de puissance pour alimenter un actionneur, ▪ Q unités de commande (311A, 311B, 311C, 311D), chacune configurée pour exécuter au moins un algorithme d'asservissement pilotant un module de puissance d'un actionneur, et ▪ un module de communication réseau (314) connectant chaque unité de commande à un réseau informatique pour communiquer avec chaque actionneur.
FR1659926A 2016-10-13 2016-10-13 Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef Active FR3057681B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1659926A FR3057681B1 (fr) 2016-10-13 2016-10-13 Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef
PCT/FR2017/052784 WO2018069637A1 (fr) 2016-10-13 2017-10-11 Système pour l'alimentation et la commande d'actionneurs à commande électrique embarqués dans un aéronef
US16/340,842 US20190263533A1 (en) 2016-10-13 2017-10-11 System for the power supply and control of electrically controlled actuators on board an aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1659926A FR3057681B1 (fr) 2016-10-13 2016-10-13 Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef
FR1659926 2016-10-13

Publications (2)

Publication Number Publication Date
FR3057681A1 FR3057681A1 (fr) 2018-04-20
FR3057681B1 true FR3057681B1 (fr) 2021-02-12

Family

ID=57750182

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1659926A Active FR3057681B1 (fr) 2016-10-13 2016-10-13 Systeme pour l'alimentation et la commande d'actionneurs a commande electrique embarques dans un aeronef

Country Status (3)

Country Link
US (1) US20190263533A1 (fr)
FR (1) FR3057681B1 (fr)
WO (1) WO2018069637A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3093870B1 (fr) * 2019-03-15 2021-04-02 Safran Electrical & Power Système de commande d’un réseau électrique d’avion
EP3725676A1 (fr) * 2019-04-16 2020-10-21 Volocopter GmbH Procédé de commande d'un système d'actionneur, système de commande d'urgence et aéronef équipé d'un tel système
US11472539B2 (en) 2020-03-05 2022-10-18 Goodrich Corporation Distributed landing gear system architecture for electromechanical actuation
US11552582B2 (en) 2020-06-15 2023-01-10 Woodward, Inc. Setpoint identification on retrofit electric actuation
FR3114410B1 (fr) * 2020-09-24 2022-09-02 Safran Electronics & Defense Architecture distribuée de système embarqué
KR20240012583A (ko) 2021-06-30 2024-01-29 레겟 앤드 플랫 캐나다 코포레이션 로컬 지능을 이용한 스마트 모터 시스템들 및 방법들

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070007385A1 (en) * 2005-06-27 2007-01-11 Honeywell International, Inc. Electric flight control surface actuation system electronic architecture
FR2934430B1 (fr) * 2008-07-23 2010-08-27 Sagem Defense Securite Ensemble d'actionneurs et d'un systeme d'alimentation electrique a partir d'un reseau
JP6396006B2 (ja) * 2013-08-30 2018-09-26 ナブテスコ株式会社 航空機用電動アクチュエータ駆動装置

Also Published As

Publication number Publication date
WO2018069637A1 (fr) 2018-04-19
FR3057681A1 (fr) 2018-04-20
US20190263533A1 (en) 2019-08-29

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