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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 (20) for a helicopter (10) has a standoff mounting arm (22, 70) that extends outwardly from the helicopter body (18, 72) in a selected direction, preferably forwardly. The standoff arm (22, 70) has an outer end (24) that mounts a low lateral speed sensing probe (26, 88) that is positioned with an axis substantially parallel to the axis of a helicopter rotor (12), and within the downwash region of air movement caused by the rotor (12). The low lateral speed sensing probe (26, 88) has ports (30, 90) that are arranged annularly around the probe (26, 88), and the pressures sensed at selected annular or peripheral locations on the probe (26, 88) are measured to determine low air speeds. Additionally, the standoff arm (22, 70) can mount a plurality of other sensors (44, 50, 52, 56, 58, 60, 76, 78, 82, 94, 96, 98) such as a pilot pressure probe (44, 82) extending forwardly from the arm, a lateral pressure sensing probe (50, 52, 76, 78) along a lateral side of the arm (22, 70), and the arm (22) can mount outside air temperature sensors (56, 94), ice detectors (58, 96), and total air temperature sensors (60, 98), if desired.
机译:用于直升机(10)的支座臂和探针组件(20)具有支座安装臂(22、70),该支座安装臂(22、70)从直升机机体(18、72)沿选定的方向向外延伸,优选向前。支撑臂(22、70)具有外端(24),该外端安装有低横向速度感测探针(26、88),该探针的轴线基本平行于直升机旋翼(12)的轴线定位。由转子(12)引起的空气流动的向下冲洗区域。低侧向速度感测探头(26、88)具有围绕探头(26、88)环形布置的端口(30、90),并且在探头(26、88)上选定的环形或外围位置处感应到的压力为测量以确定低空速。另外,支座臂(22、70)可以安装多个其他传感器(44、50、52、56、58、60、76、78、82、94、96、98),例如先导压力探头(44) ,(82)从臂向前延伸,沿着臂(22、70)的侧面的侧向压力感测探针(50、52、76、78)和臂(22)可安装外部空气温度传感器(56) ,94),冰检测器(58、96)和总空气温度传感器(60、98)(如果需要)。

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