The invention provides a vertical take-off and landing aircraft. In a vertical take-off and landing aircraft (10), a plurality of VTOL rotors (20) are divided into a plurality of groups, each VTOL rotor (20) is included in any one of the groups, and after wings (a front wing (14) and a rear wing (16)) generate lift force, a controller (46) sequentially stops the rotation of the plurality of VTOL rotors (20) in groups. Therefore, deterioration of riding comfort of the VTOL aircraft can be suppressed.

    本发明提供一种垂直起降航空器。在垂直起降航空器(10)中,多个VTOL旋翼(20)被分为多个组,每个VTOL旋翼(20)包含于任一个组中,在机翼(前翼(14)、后翼(16))产生升力后,控制器(46)使多个VTOL旋翼(20)的旋转以组为单位依次停止。据此,能够抑制VTOL飞机的乘机舒适感的恶化。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vertical take-off and landing aircraft


    Weitere Titelangaben:

    垂直起降航空器


    Beteiligte:
    AIZAWA SHIGERU (Autor:in) / TSUKAMOTO TOSHINORI (Autor:in) / MASATO KATO (Autor:in) / UCHIDA KENTA (Autor:in) / YOSHIMURA SUKESAKU (Autor:in)

    Erscheinungsdatum :

    2024-01-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge