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US09266622B2 Precipitation static charge drain system for an aircraft window 有权
用于飞机窗的降水静电荷排放系统

Precipitation static charge drain system for an aircraft window
Abstract:
A static charge drain system for an aircraft window includes a resistive probe penetrating an outer ply of the aircraft window, a first end of the probe being exposed at an outer surface of the outer ply of the aircraft window. A second end of the probe penetrates an inner surface of the outer ply of the aircraft window. A conductive drain element is disposed between the outer ply of the aircraft window and an inner ply of the aircraft window and is electrically connected between the second end of the probe and a ground point of the aircraft window.
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