The invention is applicable to the technical field of aircrafts, and provides a saucer-shaped aircraft which comprises an aircraft main body, the aircraft main body is provided with a saucer-shaped wing, and a plurality of functional wings which are rotationally connected to the aircraft main body, can be unfolded downwards and are used for buffering in the landing process are arranged below the saucer-shaped wing. The functional fins are arranged around the center of the aircraft main body, and the aircraft main body is further provided with a driving control mechanism used for driving the functional fins to rotate; the upper end of each functional wing panel is connected to the aircraft main body through a rotating structure; and the rotating structure is positioned below the dish-shaped wing and is close to the outer edge of the dish-shaped wing. And the aircraft main body is provided with a locking device for locking the functional wing panel when the aircraft main body is folded. When the saucer-shaped aircraft lands, the saucer-shaped aircraft is unfolded downwards through the functional wing panels, effective buffering can be provided, impact during landing is reduced, and the service life is prolonged.

    本发明适用于飞行器技术领域,提供了一种碟形飞行器,包括飞行器主体,所述飞行器主体设置有碟形翼,碟形翼的下方设置有转动连接于飞行器主体且可向下展开并用于降落过程缓冲的功能翼片,功能翼片设置有多个,且各功能翼片沿飞行器主体的中心环绕设置,飞行器主体还设置有用于驱动功能翼片转动的驱动控制机构;各功能翼片的上端通过转动结构连接于飞行器主体,转动结构位于所述碟形翼的下方且靠近于碟形翼的外沿。所述飞行器主体设置有用于锁定收起时所述功能翼片的锁定装置。本发明提供的一种碟形飞行器,降落时通过功能翼片向下展开,可以提供有效缓冲,减少着陆时受到的冲击,提高使用寿命。


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    Titel :

    Saucer-shaped aircraft


    Weitere Titelangaben:

    一种碟形飞行器


    Beteiligte:
    GUO YINGHUI (Autor:in)

    Erscheinungsdatum :

    2023-10-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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