Aeronautics and astronautics – Aircraft structure – Details
Patent
1992-06-12
1994-01-04
Huppert, Michael S.
Aeronautics and astronautics
Aircraft structure
Details
2441181, B64C 100
Patent
active
052753611
ABSTRACT:
An arrangement for venting a destructive internal pressure generated by an explosion within an enclosure, such as aircraft fuselage. The arrangement includes a pressure venting device for venting an exterior boundary, fuselage skin, of the enclosure; and an explosion sensitive sensor located within the enclosure. In response to an explosion within the enclosure, the sensor will send a signal to the pressure venting device. The pressure venting device creates a pressure relieving vent in the exterior boundary in advance of build up of destructive internal pressure within the enclosure.
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Bidwell Anne E.
British Aerospace Public Limited Company
Huppert Michael S.
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