A cockpit window panel that is easily installed and removed that reduces glare and heat and improves overall cockpit environment and pilot comfort. The panels include a clear polycarbonate sheet contoured to match an aircraft window, a bonding film applied to the polycarbonate sheet and a tinted film applied to the bonding film. The polycarbonate panel is bound by a flexible trim having a channel frictionally received over the peripheral edge of the panel and a conformable gasket that engages the interior window ledges when the panel is in an installed position. At least one pull tab is provided along the edge of the panel. The panels are easily installed by simply pressing them into place within the window well and secured by friction through the conformable gasket trim.
REMOVABLE TINTED WINDOW PANELS FOR AIRCRAFT COCKPIT WINDOWS
2019-05-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
REMOVABLE TINTED WINDOW PANELS FOR AIRCRAFT COCKPIT WINDOWS
European Patent Office | 2024
|REMOVABLE TINTED WINDOW PANELS FOR AIRCRAFT COCKPIT WINDOWS
European Patent Office | 2022
|REMOVABLE TINTED WINDOW PANELS FOR AIRCRAFT COCKPIT WINDOWS
European Patent Office | 2020
|REMOVABLE TINTED WINDOW PANELS FOR AIRCRAFT COCKPIT WINDOWS
European Patent Office | 2024
|