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Pressure tap structures for barometric altimeters for unmanned aerial vehicles

机译:无人机气压高度计的压力抽头结构

摘要

Various embodiments include a structure configured to at least partially expose a barometric altimeter of an unmanned aerial vehicle (UAV) to air pressure at a location on the UAV where there is reduced pressure perturbations caused by downwash of propellers. The structure may include a proximal portion configured to encompass a barometric altimeter of a circuit board of the UAV. The proximal portion may form at least a partial barrier between the barometric altimeter and a first ambient air pressure that is disturbed by a downwash from propellers of the UAV during flight of the UAV. The structure may also include a distal portion extending away from the barometric altimeter, with the distal portion configured to channel to the barometric altimeter a second ambient air pressure that is disturbed less than the first ambient air pressure by the downwash from propellers of the UAV during flight of the UAV.
机译:各种实施例包括构造成将无人机的大气压高度计至少部分地暴露于在UAV上的位置处的空气压力下的结构,在该位置处由于螺旋桨的向下冲洗而引起的压力扰动减小。该结构可以包括被配置成包含无人机的电路板的气压高度计的近端部分。近侧部分可以在气压高度计和第一环境空气压力之间形成至少部分屏障,该第一环境空气压力在UAV的飞行期间受到来自UAV的螺旋桨的向下冲洗的干扰。该结构还可以包括远离气压高度计延伸的远端部分,该远端部分被配置为将第二环境气压引导至气压高度计,该第二环境气压在第一飞行期间受到来自无人机的螺旋桨的向下冲洗的干扰小于第一环境气压。无人机的飞行。

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