Carpet installation for frangible aircraft floors

Static structures (e.g. – buildings) – Frangible section or means

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Details

49141, 244117R, 244118P, 244121, 2441291, 52 1, 52390, B64C 110, B64C 100

Patent

active

040891402

ABSTRACT:
A carpet installation for use with a frangible panel to assist in the disintegration and breakup of the panel permitting ventilation through an aircraft floor. The carpet installation utilizes positioning and hold-down tiles to reduce adhesive contact with the frangible panel and isolators to limit the support for the panel and increase the shear forces on the panel during breakup of the panel.

REFERENCES:
patent: 1930024 (1933-10-01), Varden
patent: 1951897 (1934-03-01), Binckley
patent: 2679467 (1954-05-01), Sherts
patent: 2942811 (1960-06-01), Bell
patent: 3288992 (1966-11-01), Matsadaira
patent: 3363376 (1968-01-01), Wendel
patent: 3386215 (1968-06-01), Wendel
patent: 3392489 (1968-07-01), Johnson
patent: 3425333 (1969-02-01), Wachter
patent: 3643899 (1969-02-01), Firestone
patent: 3729154 (1973-04-01), Peplante
patent: 3742968 (1973-07-01), Kennedy
patent: 3834076 (1974-09-01), Vallee
patent: 3938764 (1976-12-01), McIntyre

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