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Method for testing one or more metal tubes of aircraft framework, and means for applying said method

机译:测试飞机框架的一根或多根金属管的方法以及应用该方法的装置

摘要

359,239. Testing aircraft structures. BROUWER, D., 82, Kampweg, Soesterberg, Holland. Nov. 7, 1930, No. 33487. Convention date, April 19. Drawings to Specification. [Class 4.] The tubes of aircraft structures are tested by subjecting their bores to internal pressure and by observing for failure to maintain the pressure applied. The bores of all tubes in a structure may be made to communicate by means of small holes at places of welding or joining or they may be divided into communicating groups each provided with a nipple for the application of fluid under pressure, for instance from a cylinder containing carbonic acid under high pressure, the cylinder having a pressure gauge between the discharge valve and the connector; alternatively each group of tubes may have a nipple for attachment of a pressure gauge.
机译:359,239。测试飞机结构。布鲁克·D·布鲁克,82岁,坎普维格,荷兰Soesterberg。 1930年11月7日,编号33487。会议日期,4月19日。 [等级4]。对飞机结构的管子的孔进行内部压力测试,并观察其是否无法维持施加的压力。可以通过焊接或连接处的小孔使结构中所有管子的孔连通,或者可以将它们分成连通组,每个连通组都设有一个接头,用于在压力下(例如从液压缸中)施加流体在高压下含有碳酸,该气缸在排放阀和连接器之间具有压力表。可替代地,每组管可以具有用于连接压力计的奶嘴。

著录项

  • 公开/公告号GB359239A

    专利类型

  • 公开/公告日1931-10-22

    原文格式PDF

  • 申请/专利权人 DIRK BROUWER;

    申请/专利号GB19300033487

  • 发明设计人

    申请日1930-11-07

  • 分类号G01M3/26;

  • 国家 GB

  • 入库时间 2022-08-24 08:19:22

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