A decompression panel for use in a door of an aircraft disclosed herein includes bi-directional latching mechanisms. A differential pressure sensor disengages upon a decompression event in a compartment of an aircraft, allowing latch hooks to disengage from a panel latch of the decompression panel. Once disengaged, the decompression panel can rotate to vent air in a compartment of higher pressure to the compartment experiencing the decompression event.
Decompression panel and latch
2015-08-25
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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