Article comprising a canister closure with pressure-pulse release

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United States of America Patent

PATENT NO 7685920
APP PUB NO 20060090635A1
SERIAL NO

11141165

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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The illustrative embodiment of the present invention is a launch system that includes a closure that, in use, is attached to one or both ends of a missile canister. The closure is blown off of the canister before there is any contact between it and the nose of the missile. The closure incorporates an actuation mechanism that releases the closure when there is a rapid increase in pressure within the canister, such as when the booster of a canistered missile fires. The actuation mechanism is not, however, responsive to the magnitude of the pressure within the canister. As a consequence, the closure will not release if there is a slow build-up of pressure within the missile canister.

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Patent Owner(s)

Patent OwnerAddress
LOCKHEED MARTIN CORPORATION6801 ROCKLEDGE DRIVE BETHESDA MD 20817

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Paul, Buddy R Perry Hall, US 7 25

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