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METHODS OF CONNECTING TESTING EQUIPMENT TO A MISSILE SYSTEM

机译:将测试设备连接到导弹系统的方法

摘要

A missile system includes a plurality of components, and a testing instrumentation platform secured within at least one of the plurality of components. The testing instrumentation platform is secured within the component(s) through at least one platform supporting adapter assembly. The platform supporting adapter assembly may include an adapter having a planar panel that supports one or more fasteners. The fastener(s) are configured to securely connect to a portion of a base of the testing instrumentation platform. At least one through-hole may be formed through a portion of the adapter. At least one tapered bolt is configured to be securely retained within the through-hole(s). The tapered bolt(s) securely connects the adapter to the component(s).
机译:一种导弹系统,包括多个部件,以及固定在所述多个部件中的至少一个内的测试仪器平台。测试仪器平台通过至少一个支撑适配器组件的平台固定在部件内。平台支撑适配器组件可包括适配器,该适配器具有支撑一个或多个紧固件的平板。紧固件被配置为牢固地连接到测试仪器平台的基座的一部分。可以穿过适配器的一部分形成至少一个通孔。至少一个锥形螺栓构造成牢固地保持在通孔内。锥形螺栓将适配器牢固地连接到组件。

著录项

  • 公开/公告号US2017074619A1

    专利类型

  • 公开/公告日2017-03-16

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201514850141

  • 发明设计人 KEVIN DOMINGUEZ;

    申请日2015-09-10

  • 分类号F41G7;

  • 国家 US

  • 入库时间 2022-08-21 13:50:27

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