Aircraft shell module

Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation

Patent

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Details

52397, 52144, 181207, 105397, 105337, 105338, 244119, B64C 114

Patent

active

047996315

ABSTRACT:
Two arcuate panel sections having a dampening layer between two honeycomb layers form a module which is mounted in multiple elastomeric isolators located within channel members. Support brackets attached to the interior of the aircraft skin support the channels in the overhead area and along the port and starboard deck edge. The module is thereby spaced apart from the aircraft frame. There is a resulting diminution of acoustic transmission from the aircraft frame to its interior passenger area.

REFERENCES:
patent: 2111326 (1938-03-01), Norris
patent: 2912724 (1959-11-01), Wilkes
patent: 2925050 (1960-02-01), Candlin, Jr. et al.
patent: 3352078 (1967-11-01), Neal
patent: 4050208 (1977-09-01), Pompei et al.
patent: 4296692 (1981-10-01), Roux
patent: 4319528 (1982-03-01), Gutridge et al.
patent: 4674712 (1987-06-01), Whitener et al.

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