Universal cabin sidewall panel for aircraft

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244117R, 2441185, B64D 1100, B64C 114

Patent

active

050445782

ABSTRACT:
A single-size interior cabin sidewall panel fits aircraft of different sizes. The panel is fabricated so that in its "relaxed" state it has a curved configuration which requires the panel to be unbended to fit in the aircraft. Larger aircraft require more unbending of the panel than do smaller aircraft. This results in a uniform pressure across the panel which promotes a close fit between adjacent overlapping sidewall panels.

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