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.
Precipitation static charge drain system for an aircraft window
2016-02-23
Patent
Electronic Resource
English
Aircraft Precipitation Static Certification
SAE Technical Papers | 2023
Precipitation-Static (P-Static) Overview of Composite Aircraft
SAE Technical Papers | 2001
|AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN
European Patent Office | 2018
|AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN
European Patent Office | 2019
|AIRCRAFT TRANSPARENCY WITH PRESSURE SEAL AND/OR ANTI-STATIC DRAIN
European Patent Office | 2015
|