PROBLEM TO BE SOLVED: To reduce a volume occupied by a device provided in a first space having a large spacial limitation.SOLUTION: An electric actuator drive control device comprises: a drive unit located in a first space of equipment, and that applies power to an electric actuator; and a controller located in a second space of the equipment, and that transmits to the drive unit a power command signal including information on the power to be applied to the electric actuator. The first space where the drive unit is located is limited compared with the second space where the controller is located.SELECTED DRAWING: Figure 1

    【課題】空間的な制限が大きい第1空間に配置される装置が占める体積を削減する。【解決手段】電動アクチュエータ駆動制御装置は、機器の第1空間に位置し、電動アクチュエータに電力を印加する駆動部と、機器の第2空間に位置し、電動アクチュエータに印加する電力に関する情報を含む電力指令信号を駆動部へ送信する制御部と、を備える。駆動部が位置する第1空間は、制御部が位置する第2空間に比べて制限されている。【選択図】図1


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    Title :

    ELECTRIC ACTUATOR DRIVE CONTROL DEVICE AND AIRCRAFT


    Additional title:

    電動アクチュエータ駆動制御装置及び航空機


    Contributors:

    Publication date :

    2018-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B64C AEROPLANES , Flugzeuge



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