The invention provides a separation wing device of a multi-stage cabin and a multi-stage cabin structure. The device comprises at least two wing tables which are connected in an inserted mode; a wing surface which is connected with the wing platform in an inserting manner; wherein the wing platform is connected with the separable multi-stage cabin body in an inserted mode. According to the device, the wing platform and the wing surface are connected in an inserted mode to form the separation wing device, the separation wing device is fixedly connected to the multi-stage cabin in an inserted mode, and therefore when the multi-stage cabin is separated, the effects of stably decelerating and preventing the aircraft from rotating are achieved; and the wing platform and the wing surface are simple in structure and convenient to produce and process.

    本发明提供一种多级舱体的分离翼装置及多级舱体结构,其中装置包括:至少两个相互插接的翼台;与所述翼台插接的翼面;所述翼台与可分离的多级舱体插接。本发明的方案通过将所述翼台与所述翼面插接构成分离翼装置,并将分离翼装置插接固定于所述多级舱体上,从而实现在所述多级舱体分离时,以达到稳定减速和防止飞行器自身旋转的效果;且所述翼台、所述翼面结构简单,便于生产加工。


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    Titel :

    Separation wing device of multi-stage cabin and multi-stage cabin structure


    Weitere Titelangaben:

    一种多级舱体的分离翼装置及多级舱体结构


    Beteiligte:
    ZHANG YI (Autor:in) / JI BAOFENG (Autor:in) / ZOU YUNXIANG (Autor:in) / GUO HAO (Autor:in) / YAO JINWEI (Autor:in)

    Erscheinungsdatum :

    2021-10-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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