The invention discloses a small rocket take-off stability augmentation platform which comprises a pressurization module and an execution module. The pressurization module comprises a pressurization plate, a pressurization column, a pressurization barrel, a pressurization barrel support, a spiral shaft support, a pressurization gear, a pressurization motor support, a pressurization motor, a pressurization driving gear, a spiral shaft, a supporting panel, a buffer fan and a buffer fan support. The execution module is arranged so that a large amount of gas generated at a bottom during rocket launching can be collected, and an airflow is converted into power; the pressurization module is cooperated so that perpendicularity of a rocket during launching can be improved, and a rocket launching failure probability can be reduced; and a tubular air wall can be formed around the rocket through the arrangement of a protection ring and a deck, the perpendicularity of the rocket during launching can be improved, and a phenomenon that birds impact a rocket shell can be prevented.

    本发明公开了一种小型火箭起飞增稳平台,包括增压模块和执行模块,所述的增压模块包括增压板、增压柱、增压桶、增压桶支架、螺旋轴支架、增压齿轮、增压电机支架、增压电机、增压主动齿轮、螺旋轴、支撑面板、缓冲扇和缓冲扇支架。本发明通过设置执行模块,可以将火箭发射时底部产生的大量气体收集起来,并且将气流转化为动力,并且配合增压模块,可以提高火箭起飞时的垂直度,从而可以降低火箭发射失败的概率,通过设置保护环和甲板,可以在火箭的周围形成一个管状的风墙,不仅可以提高火箭发射时的垂直度,而且还可以防止鸟儿撞击火箭外壳现象的发生。


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    Title :

    Small rocket take-off stability augmentation platform


    Additional title:

    一种小型火箭起飞增稳平台


    Contributors:
    CAO JIANBAO (author)

    Publication date :

    2020-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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