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Antenna rotation cross for helicopter radar system fitted to rotor head above rotor blades with carrier arms attached to central fitting

机译:直升机雷达系统的天线旋转十字,安装在旋翼叶片上方的旋翼头上,而支架臂则安装在中央配件上

摘要

The antenna rotation cross has individual carrier arms, each provided with a hollow space acting as an antenna housing for reception of an antenna and associated electronic components of a radar system with a synthetic aperture. The carrier arms are fitted to the rotor head parallel to the rotor blade plane via a central fitting (10) attached to the rotor head, with a hollow chamber (50) defined between upper and lower plates (11,12) having termination arms (15,16,17,18) and further hollow chambers (41,42,43,44) between the latter.
机译:天线旋转十字具有单独的承载臂,每个承载臂均具有用作天线外壳的中空空间,用于接收天线以及具有合成孔径的雷达系统的相关电子组件。承载臂通过连接到转子头的中心配件(10)平行于转子叶片平面安装到转子头上,在上板(11,12)和下板(11,12)之间限定了一个中空室(50),该中空室具有终端臂( 15、16、17、18)和在它们之间的其他中空室(41、42、43、44)。

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