The size of a propellant force generator in the axial direction of a rotational shaft of a motor is reduced while making the pitch angles of rotational blades driven by the motor variable. The propellant force generator (1) includes a propellant-force generating motor (2) adapted to generate a propellant force for rotational blades (H1 to H3), a pitch varying motor (5) adapted to generate a rotational motion for changing pitch angles of the rotational blades (H1 to H3), a rotation-linear motion converting unit (7) adapted to convert the rotational motion generated by the pitch varying motor (5) into a linear motion, and a linear motion-rotation converting unit (8) adapted to convert the linear motions converted by the rotation-linear motion converting unit (7) into rotational motions. At least a part of the linear motion-rotation converting unit (7) is located within the propellant-force generating motor (2).


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    Titel :

    THRUST GENERATING DEVICE


    Weitere Titelangaben:

    SCHUBERZEUGUNGSVORRICHTUNG
    DISPOSITIF DE GÉNÉRATION DE POUSSÉE


    Beteiligte:
    KUMAGAI HIROYASU (Autor:in) / GUNJI DAISUKE (Autor:in)

    Erscheinungsdatum :

    27.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U / F16H Getriebe , GEARING



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