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Multifunction probe for primary references for aircraft, associated measuring system, aircraft and method for obtaining physical quantities

机译:用于飞机的主要参考的多功能探头,相关的测量系统,飞机以及获得物理量的方法

摘要

A multifunction probe for primary references for an aircraft, an associated measuring system, aircraft and method for obtaining physical quantities are disclosed. In one aspect, the multifunction probe includes a base designed to be fastened on the cockpit of an aircraft, a plurality of static pressure taps arranged through the base and connected to pressure measuring devices and an optical window transparent to laser radiation and positioned in the base for the passage of laser radiation through the base. The multifunction probe further includes at least one laser anemometry optical head positioned to take laser anemometry measurements through the optical window and a static temperature probe mounted on the base.
机译:公开了一种用于飞机的主要参考的多功能探针,相关的测量系统,飞机以及用于获得物理量的方法。一方面,该多功能探头包括:被设计成固定在飞机的驾驶舱上的基座;多个穿过基座布置并连接至压力测量装置的静压接头;以及对激光辐射透明并位于基座中的光学窗口。用于使激光辐射穿过基座。多功能探头还包括至少一个激光风速仪光学头,其位置设置为通过光学窗口进行激光风速仪测量;静态温度探头安装在底座上。

著录项

  • 公开/公告号US10495662B2

    专利类型

  • 公开/公告日2019-12-03

    原文格式PDF

  • 申请/专利权人 THALES;

    申请/专利号US201615132978

  • 申请日2016-04-19

  • 分类号G01P3/36;G01P13/02;G01S17/58;G01C23;B64D43/02;G01P5/14;G01P5/26;G01P21/02;G01S17/02;G01S17/95;G01S7/481;

  • 国家 US

  • 入库时间 2022-08-21 11:25:39

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