To provide a redundant propulsion device and an electric aircraft, which can properly cool a plurality of electric motors without increasing the size of a nacelle.SOLUTION: A redundant propulsion device 20 comprises a propeller 21, and a plurality of electric motors 23A-23E for driving the propeller 21. The plurality of electric motors are disposed with respect to a propeller shaft 21a of the propeller so that, around the propeller shaft, at least one of the electric motors is disposed at each of a plurality of locations in the extending direction of the propeller shaft, and the electric motors are disposed at positions respectively where an output shaft 23a of each of the plurality electric motors does not overlap any one of output shafts of the other electric motors as viewed in a direction along the propeller shaft from the propeller side.SELECTED DRAWING: Figure 2

    【課題】ナセルのサイズを増大させることなく、複数の電動モータを適切に冷却することが可能な冗長系推進装置や電動航空機を提供する。【解決手段】プロペラ21と、プロペラ21を駆動する複数の電動モータ23A〜23Eと、を備える冗長系推進装置20において、複数の電動モータは、プロペラのプロペラ軸21aに対してその延在方向の複数箇所に少なくとも1基ずつプロペラ軸の周囲に配置されており、かつ、プロペラ側からプロペラ軸に沿う方向に見た場合に、複数の電動モータの各出力軸23aが他の電動モータの出力軸のいずれとも重ならない位置にそれぞれ配置されている。【選択図】図2


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    Title :

    REDUNDANT PROPULSION DEVICE AND ELECTRIC AIRCRAFT


    Additional title:

    冗長系推進装置及び電動航空機


    Contributors:

    Publication date :

    2021-02-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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