PROBLEM TO BE SOLVED: To provide an electric starter system which is loaded on an aircraft, and of which complexity and a cost are reduced.SOLUTION: A starter system for an aircraft comprises: an electrically-driven mechanical actuator 25 including a non-volatile memory 60 in which memory object data 61 including a specific configuration data 62 is stored; a control unit 22 which uses the configuration data for mounting a servo control loop, and in which an output signal of the servo control loop is a digital signal which controls an electric motor of the electrically-driven mechanical actuator; and at least one digital transmission channel 50 which connects the control unit and the electrically-driven mechanical actuator to each other.SELECTED DRAWING: Figure 6

    【課題】複雑さ及びコストを削減する、航空機搭載の電気起動システムを提供する。【解決手段】航空機用の起動システムにおいて、電動機械アクチュエータに特定的な構成データ62を含む記憶対象データ61が記憶されている不揮発性メモリ60を含む電動機械アクチュエータ25と、サーボ制御ループを実装するために構成データを使用する制御ユニット22であって、サーボ制御ループの出力信号が、電動機械アクチュエータの電動機を制御するデジタル信号である制御ユニットと、制御ユニットと電動機械アクチュエータを接続する少なくとも1つのデジタル伝送チャネル50と、を備えた起動システム。【選択図】図6


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    Title :

    STARTER SYSTEM FOR AIRCRAFT


    Additional title:

    航空機用の起動システム


    Contributors:

    Publication date :

    2017-06-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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