Method of making rocket motor case with integral nozzle
    1.
    发明授权
    Method of making rocket motor case with integral nozzle 失效
    制造具有整体喷嘴的火箭发动机壳体的方法

    公开(公告)号:US4440587A

    公开(公告)日:1984-04-03

    申请号:US404253

    申请日:1982-08-02

    Abstract: A method of making a rocket motor case with an integral nozzle in which the rocket motor has a large length to diameter ratio and is made by applying a linear wrap of fibers as a first layer on a mandrel and then by applying radial wraps over said linear wrap and also conforming the linear fibers to the shape of the nozzle after applying the linear fibers on said mandrel to provide a structure that has sufficient stiffness to accomplish the desired result of a large length to diameter rocket motor case.

    Abstract translation: 一种制造具有整体喷嘴的火箭发动机壳体的方法,其中火箭发动机具有大的长径比,并且通过将纤维的线性包裹作为第一层施加在心轴上,然后通过在所述直线上施加径向包裹而制成 在将线性纤维施加到所述心轴上之后,使线性纤维与喷嘴的形状一致,以提供具有足够刚度以实现大直径火箭发动机壳体的期望结果的结构。

    Filament/epoxy camouflage launch tubes
    2.
    发明授权
    Filament/epoxy camouflage launch tubes 失效
    长丝/环氧伪装发射管

    公开(公告)号:US4137351A

    公开(公告)日:1979-01-30

    申请号:US892542

    申请日:1978-04-03

    CPC classification number: C08G59/4215 F41A21/20 F41H3/00 Y10S428/919

    Abstract: Filament/epoxy camouflage launch tubes in which the launch tubes are fabrted using conventional filament winding processes and materials and in which each tube is bonded together with an epoxy resin system in which the epoxy resin system includes coloring agents for coloring the launch tubes in a camouflage color that colors the launch tube through and through. The exact color of the launch tube can be varied by varying the amount of the coloring agent.

    Abstract translation: 长丝/环氧伪装发射管,其中发射管使用常规的丝缠绕工艺和材料制造,并且其中每个管与环氧树脂体系结合在一起,其中环氧树脂体系包括着色剂,用于在伪装中着色发射管 颜色使发射管穿过和穿过。 可以通过改变着色剂的量来改变发射管的确切颜色。

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