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Composit rocket motor housing with integrated fins and its method of production

机译:具有集成翅片的复合火箭发动机壳体及其制造方法

摘要

A tubular preform (10), fins (30), and fin supports (20) are made independently, with the fins and the fin supports being made by laying fibrous cloth impregnated with polymerizable binder to take up the appropriate shapes, and then polymerizing the binder, whereas the tubular preform is made by winding a thread impregnated with a polymerizable binder. Each fin support has a base integrated with the periphery of the tubular preform, and has fin attachment portions projecting from its base, with the bases of the fin supports and the periphery of the tubular preform being shaped in such a manner as to ensure circumferential continuity of the structure. The fin supports are integrated with the tubular preform by gluing together with at least one position of localized overwinding at the gaps in the fin supports between the fin attachment portions, thereby providing a perform which is smooth in structure both inside and outside. The assembly constituted by the tubular preform, the fin supports, and the overwinding is polymerized in order to obtain a tube for constituting a rocket, and the fins are subsequently assembled to the fin support by gluing the sides of the fins onto the attachment portion of the fin supports.
机译:管状预成型件(10),散热片(30)和散热片支撑件(20)是独立制作的,散热片和散热片支撑件是通过放置浸渍有可聚合粘合剂的纤维布制成合适的形状,然后将其聚合而制成的。管状预成型件是通过缠绕浸渍有可聚合粘合剂的线制成的。每个翅片支撑件具有与管状预成型件的外围成一体的基底,并且具有从翅片支撑件的基部突出的翅片附接部分,翅片支撑件的基部和管状预成型件的外围以确保周向连续性的方式成形。结构。通过在鳍片附接部分之间的鳍片支撑件中的间隙处将至少一个局部缠绕的位置胶合在一起,鳍片支撑件与管状预成型件成为一体,从而提供在内部和外部结构均光滑的性能。由管状预型件,翅片支撑件和上卷构成的组件被聚合,以获得用于构成火箭的管,随后通过将翅片的侧面粘合到翅片的附接部分上,将翅片组装到翅片支撑件上。鳍支撑。

著录项

  • 公开/公告号EP0340088A1

    专利类型

  • 公开/公告日1989-11-02

    原文格式PDF

  • 申请/专利权人 SOCIETE EUROPEENNE DE PROPULSION;

    申请/专利号EP19890401133

  • 发明设计人 DAFFIX LOUIS D.;CRAPIZ DINO N.;

    申请日1989-04-21

  • 分类号F02K9/34;F42B10/04;

  • 国家 EP

  • 入库时间 2022-08-22 06:33:44

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