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Adapter for connecting a pressure line to the perforated surface of a model to be tested in the wind tunnel

机译:用于将压力管线连接到要在风洞中测试的模型的穿孔表面的适配器

摘要

To measure the pressure distribution at an airplane model and the like, the surface of the model is provided with a number of holes (11) . An adapter (25) of elastomeric material adapted to be joined via a pressure duct (24) to a testing means is placed on each hole (11). A plurality of connecting hoses (13) extending out of the model (10) are joined to a measuring point selector (14). Each adapter (25) contains a self-adhesive flange by which the adapter may be sealingly mounted quickly and by simple means to a measuring bore.
机译:为了测量飞机模型等处的压力分布,模型的表面设置有多个孔(11)。适于通过压力导管(24)连接到测试装置的弹性材料的适配器(25)被放置在每个孔(11)上。延伸出模型(10)的多个连接软管(13)连接至测量点选择器(14)。每个适配器(25)都包含一个自粘式法兰,通过该法兰可以将适配器快速且简单地密封安装到测量孔中。

著录项

  • 公开/公告号US4653317A

    专利类型

  • 公开/公告日1987-03-31

    原文格式PDF

  • 申请/专利权人 DEUTSCHE FORSCH LUFT RAUMFAHRT;

    申请/专利号US19850752930

  • 发明设计人 BERTHOLD SCHTAFER;

    申请日1985-07-08

  • 分类号G01M19/00;

  • 国家 US

  • 入库时间 2022-08-22 07:09:29

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