To provide a control device for an electric aircraft that can suppress noise and an exhaust gas emitted from an internal combustion engine at the time of takeoff.SOLUTION: A control device 6 controls an electric aircraft 100 that includes: a motor 2 for driving a rotor 1; a storage battery 3 for supplying power to the motor 2; a power generator 4 using an internal combustion engine 5 as a power source and capable of supplying power to the motor 2 and the storage battery 3; and an altitude acquisition device 7 for acquiring a flight altitude. The control device 6 supplies power to the motor 2 from the storage battery 3 while stopping the internal combustion engine 5 to cause the electric aircraft 100 to take off, after the takeoff of the electric aircraft 100, determines whether an altitude H of the electric aircraft 100 is equal to or higher than an altitude threshold Ht, and when the altitude H of the electric aircraft 100 acquired by the altitude acquisition device 7 is equal to or more than the altitude threshold Ht, activates the internal combustion engine 5.SELECTED DRAWING: Figure 3

    【課題】離陸時に内燃機関から発生する騒音や排出ガスを抑制できる電動航空機の制御装置を提供する。【解決手段】回転翼1を駆動するモータ2と、モータ2に電力を供給する蓄電池3と、内燃機関5を動力源としモータ2と蓄電池3に電力を供給し得る発電機4と、飛行高度を取得する高度取得装置7とを備える電動航空機100を制御する制御装置6であって、制御装置6は、内燃機関5を停止させたまま蓄電池3から電力をモータ2に供給して電動航空機100を離陸させ、電動航空機100の離陸後、電動航空機100の高度Hが高度閾値Ht以上か否かを判定し、高度取得装置7により取得した電動航空機100の高度Hが高度閾値Ht以上の場合に、内燃機関5を起動する。【選択図】図3


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    Title :

    CONTROL DEVICE FOR ELECTRIC AIRCRAFT AND METHOD FOR CONTROLLING ELECTRIC AIRCRAFT


    Additional title:

    電動航空機の制御装置および電動航空機の制御方法


    Contributors:

    Publication date :

    2025-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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