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STANDOFF MOUNTING FOR AIR DATA SENSING PROBES ON A HELICOPTER

机译:直升机上空气数据检测问题的停靠安装

摘要

A standoff arm and probe assembly for a helicopter has a standoff mounting arm that extends outwardly from the helicopter body in a selected direction, preferably forwardly. The standoff arm has an outer end that mounts a low lateral speed sensing probe that is positioned with an axis substantially parallel to the axis of a helicopter rotor, and within the downwash region of air movement causes by the rotor. The low lateral speed sensing probe has ports that are arranged annularly around the probe, and the pressures sensed at selected annular or peripheral locations on the probe are measured to determine low air speeds. Additionally, the standoff arm can mount a plurality of other sensors such as a pitot pressure probe extending forwardly from the arm, a lateral pressure sensing probe along a lateral side of the arm, and the arm can mount outside air temperature sensors, ice detectors, and total air temperature sensors, if desired.
机译:用于直升机的支座臂和探针组件具有支座安装臂,该支座安装臂从直升机机身沿选定的方向向外延伸,优选向前延伸。支座臂具有外端,该外端安装有低横向速度感测探针,该探针的轴线基本平行于直升机旋翼的轴线,并且位于由旋翼引起的空气运动的向下冲洗区域内。低横向速度感测探针具有环形地围绕探针布置的端口,并且测量在探针上选定的环形或外围位置处感测到的压力以确定低空气速度。此外,对峙臂还可以安装多个其他传感器,例如从该臂向前延伸的皮托管压力探头,沿着该臂侧面的横向压力感测探头,并且该臂可以安装外部空气温度传感器,冰探测器,以及总空气温度传感器(如果需要)。

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