A header assembly is configured to be secured between an inboard structure and an outboard structure within an internal cabin of an aircraft. The header assembly may include a main body including a first panel connected to an opposed second panel by a base panel. The main body is configured to limit light from passing therethrough. At least three anchoring members are configured to securely connect the main body to at least three reciprocal structures of the inboard and outboard structures.
LIGHT-LIMITING HEADER ASSEMBLY FOR A TRANSITION AREA WITHIN AN INTERIOR CABIN OF AN AIRCRAFT
2016-06-16
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
LIGHT-LIMITING HEADER ASSEMBLY FOR A TRANSITION AREA WITHIN AN INTERIOR CABIN OF AN AIRCRAFT
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