Process for fabricating one-piece rocket motor heat barrier
    3.
    发明授权
    Process for fabricating one-piece rocket motor heat barrier 失效
    制造单件式火箭发动机热障的方法

    公开(公告)号:US3956453A

    公开(公告)日:1976-05-11

    申请号:US421307

    申请日:1973-12-03

    CPC分类号: B29C33/52 B29C43/00

    摘要: A method for molding one piece seamless contoured structures. The mold consists of a hollow, cylindrical mold member whose internal surface area defines the external surface of the piece to be molded, that is adaptive to receive a piston having a reservoir containing a fluid plastic and a mandrel mold member of low melting alloy whose shape defines the internal surface of the molded structure. The piston is forced upward to cause the fluid plastic to flow into the interstices and allowed to cure. Heat is applied to the mold assembly to melt the alloy to allow removal of the contoured structure when the mold assembly is disassembled.

    摘要翻译: 一种成型无缝轮廓结构的方法。 模具由中空的圆柱形模具构件组成,其内表面区域限定待模​​制件的外表面,其适于接收活塞,该活塞具有容纳流体塑料的储存器和低熔点合金的心轴模具构件,其形状 限定了模制结构的内表面。 活塞被向上推动以使流体塑料流入空隙并允许固化。 将热量施加到模具组件以熔化合金,以允许在拆卸模具组件时移除轮廓结构。