The invention discloses a shoulder-carrying type electric vertical take-off and landing aircraft and a vertical type electric vertical take-off and landing aircraft. The vertical shoulder-carrying type small electric vertical take-off and landing aircraft comprises a rack, a driving mechanism and a control mechanism. The rack comprises a transverse supporting device and a vertical supporting device connected with the transverse supporting device, and two ends of the transverse supporting device are connected with driving mechanisms respectively. The control mechanism comprises a pushing deviceused for pushing the driving mechanism and a control device used for controlling a running direction of the aircraft.

    本发明公开了一种肩背式电动垂直起降飞行器及直立式电动垂直起降飞行器。直立肩背式小型电动垂直起降飞行器包括机架、驱动机构以及操控机构;所述机架包括横向支撑装置和与横向支撑装置连接的竖向支撑装置,所述横向支撑装置的两端分别连接有驱动机构;所述操控机构包括用于推动驱动机构的推动装置和用于操控飞行器运行方向的操控装置。


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    Titel :

    Shoulder-carrying type electric vertical take-off and landing aircraft and vertical type electric vertical take-off and landing aircraft


    Weitere Titelangaben:

    肩背式电动垂直起降飞行器及直立式电动垂直起降飞行器


    Beteiligte:
    YANG SHOULI (Autor:in)

    Erscheinungsdatum :

    04.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G08C Übertragungssysteme für Messwerte, Regel-, Steuer- oder ähnliche Signale , TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS



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