An engine for an aircraft is presented that includes a rotor, an electric motor that drives the rotor in rotation, and an ECU that controls the electric motor, where rotation of the rotor provides a primary airflow that induces thrust of the engine, and where the ECU is located within a volume defined by the primary airflow.

    提出了一种用于飞行器的发动机,其包括转子、驱使转子旋转的电动机和控制电动机的ECU,其中转子的旋转提供引起发动机的推力的主气流,并且其中ECU位于由主气流限定的体积内。


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    Titel :

    Aircraft engine


    Weitere Titelangaben:

    飞行器发动机


    Beteiligte:

    Erscheinungsdatum :

    30.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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