The invention provides a flexible and foldable large porthole spacecraft configuration. The flexible and foldable large porthole spacecraft configuration comprises a watchtower tower, a flexible cabin, a connecting cover, a stopping mechanism and a cabin door. The stopping mechanism of the spacecraft can be docked with other aircrafts in an on-orbit mode. The flexible cabin is in a compressed state during launching and can be inflated and unfolded to form a flexible inflatable cabin body after orbit injection operation; the watchtower is provided with a 360-DEG large-area immersed porthole composed of seven parts, and a porthole protection cover can be unfolded on orbit. The cabin door is arranged inside the stopping mechanism, and can be opened outwards, an astronaut enters the spacecraftthrough the stopping mechanism and the cabin door, passes by the flexible cabin, reaches the lookout tower and can observe and look out to the outside space through the porthole, and the porthole also has the functions of improving the living environment of the astronaut and relieving and releasing psychological pressure in a space closed environment while providing a large-view observation window. The connecting cover is used for connecting the stopping mechanism and the lookout tower in the launching stage and plays a role in protecting the flexible cabin and bearing force at the same time,and before the cabin body is inflated and unfolded on the orbit, the connecting cover is disconnected with the watchtower.

    本发明提供一种柔性可折展的大舷窗航天器构型,包括瞭望塔、柔性舱、连接罩、停靠机构、舱门。所述航天器的停靠机构可在轨与其他飞行器进行对接;柔性舱在发射时处于压缩状态,入轨运行后可充气展开形成柔性充气舱体;瞭望塔有7个部分组成的360°大面积沉浸式舷窗,舷窗保护罩可在轨展开;舱门在停靠机构内部,可向外打开,航天员通过停靠机构和舱门进入该航天器,经过柔性舱到达瞭望塔,可透过舷窗向外界空间观察瞭望,舷窗提供大视野观察窗口的同时也起到改善航天员生活环境,缓解释放空间密闭环境下心理压力的功能;连接罩用于发射阶段连接停靠机构与瞭望塔,同时起到保护柔性舱和承力的作用,舱体在轨充气展开之前,连接罩与瞭望塔断开连接。


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    Title :

    Flexible and foldable large porthole spacecraft configuration


    Additional title:

    一种柔性可折展的大舷窗航天器构型


    Contributors:
    LOU QIAO (author) / SUN XIAOZHU (author) / LIN FUXIN (author) / LI LICHUN (author) / DU ZEHONG (author) / ZHU JUNJIE (author) / BAI HEMIN (author) / LIU LUJIANG (author) / WANG HUA (author) / WANG CHANGHUAN (author)

    Publication date :

    2020-07-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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