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Methods and apparatus for an in-flight precipitation static sensor

机译:机上降水静态传感器的方法和设备

摘要

A precipitation static sensor includes a bottom flexible dielectric layer (e.g., a layer of urethane tape) configured to be attached to a wing or other external surface of an aircraft, a flexible conductive layer (e.g., a layer of aluminum tape) formed over a portion of the first flexible dielectric layer, and a conductor (such as a twisted-pair wire) coupled to the flexible conductive layer. A top flexible dielectric layer is formed over a portion of the bottom dielectric layer and a portion of the flexible conductive layer, thus forming an exposed detector region. In accordance with a further embodiment, multiple such precipitation static sensors are used and coupled to a meter device (e.g., a picoammeter), which may also be coupled to a data acquisition and display for providing a visual indication of the charge accumulated by the precipitation static sensors.
机译:降水静态传感器包括构造成附接到飞机的机翼或其他外表面的底部柔性电介质层(例如,氨基甲酸乙酯带层),形成在底部上方的柔性导电层(例如,铝带层)。第一柔性介电层的一部分,和耦合到柔性导电层的导体(例如双绞线)。在底部电介质层的一部分和柔性导电层的一部分上形成顶部柔性电介质层,从而形成暴露的检测器区域。根据另一实施例,使用多个这样的降水静态传感器,并且将其耦合至仪表装置(例如皮安计),该仪表装置还可以耦合至数据采集和显示,以提供由降水积累的电荷的视觉指示。静态传感器。

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