The invention provides a near space aircraft rigid deceleration control device and an aircraft, and relates to the technical field of aircraft deceleration control, the near space aircraft rigid deceleration control device is used for being arranged between a head cabin and a load cabin of a near space aircraft, the near space aircraft rigid deceleration control device comprises a deceleration control cabin, and the outer side of the deceleration control cabin is sequentially provided with a plurality of inner resistance plates and a plurality of outer resistance plates from inside to outside; the multiple inner resistance plates and the multiple outer resistance plates are evenly distributed along the circumference, a driving mechanism is arranged in the speed reduction control cabin, and the driving mechanism is connected with the inner resistance plates and the outer resistance plates and used for driving the inner resistance plates and the outer resistance plates to be opened and closed; the problems that in the prior art, a speed reduction structure of a near space aircraft is limited by the installation position and size design, and real-time speed regulation and aircraft attitude adjustment are difficult to conduct are solved.

    本发明提供一种临近空间飞行器刚性减速控制装置及飞行器,涉及飞行器减速控制技术领域,用于设置在临近空间飞行器的头舱和载荷舱之间,包括:减速控制舱,减速控制舱的外侧由内向外依次设置有多个内阻力板和多个外阻力板,多个内阻力板和多个外阻力板分别沿一圆周均布,减速控制舱的内部设置有驱动机构,驱动机构与内阻力板和外阻力板连接,并用于驱动内阻力板和外阻力板开合;解决现有技术中临近空间飞行器的减速结构受安装位置和尺寸设计所限,并且难以进行实时调速和飞行器姿态调整的问题。


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    Titel :

    Near space aircraft rigid deceleration control device and aircraft


    Weitere Titelangaben:

    一种临近空间飞行器刚性减速控制装置及飞行器


    Beteiligte:
    LI NA (Autor:in) / WENG MINGZE (Autor:in) / ZHU MENGLONG (Autor:in) / ZHANG YAJU (Autor:in) / LIU XINYU (Autor:in)

    Erscheinungsdatum :

    18.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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