Integrally damped composite aircraft floor panels

Acoustics – Sound-modifying means – Sound absorbing fence or screen

Reexamination Certificate

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Details

C181S292000, C181S288000

Reexamination Certificate

active

07419031

ABSTRACT:
In accordance with the present invention an aircraft floor panel is provided comprising a honeycomb core element having an upper core surface, a lower core surface, and a core thickness. An upper face sheet assembly is mounted to and seals the upper core surface and includes at least one upper material sheet impregnated with an upper epoxy resin. A lower damping face sheet assembly is mounted to and seals the lower core surface and includes at least one lower material sheet infused with a highly damped lower epoxy resin. The lower damping face sheet assembly dampens vibrational noise.

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