Relief of inter-compartment differential pressure in aircraft

Aeronautics and astronautics – Aircraft structure – Load accommodation

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52 98, 137 68R, 244121, B64C 118

Patent

active

040492214

ABSTRACT:
Apparatus for equalizing the pressure between two compartments of an airplane in the event of sudden depressurization of one of the compartments, and including a closure panel disposed across an opening between the two compartments and functioning as either a blowout panel to be forced bodily from the opening upon development of an excessive differential pressure between the two compartments, or as a frangible panel which is shattered in response to attainment of the undesired differential pressure, to thus allow very open communication between the compartments preventing damage to a wall therebetween.

REFERENCES:
patent: 2679467 (1954-05-01), Sherts
patent: 3332175 (1967-07-01), Hawes et al.
patent: 3938764 (1976-02-01), McIntyre et al.

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