ATE467807T1

Deployment mechanism for stowable fins in missiles

Abstract

A deployment mechanism ( 414 ) in combination with a missile ( 10 ), guided projectile ( 410 ) or other ordnance that automatically pivots and rotates a fin ( 412 ) from a stowed orientation to a deployed orientation. The deployment mechanism ( 414 ) includes a tubular cam ( 434 ) having a retention mechanism ( 455 ) that retains the fin ( 412 ) simply and reliably in the stowed orientation. The tubular cam also guides the fin ( 412 ) quickly to the deployed orientation.

Term

Term ended

Projected expiry passed 14 March 2023, 3.5 years ago.

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13 members in 7 offices

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Priority claims
DocumentOfficeKindDate
10203202United States of AmericaA
0307931United States of AmericaW

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DocumentOfficeKind
US2003178527A1United States of AmericaA1
WO03081165A1World Intellectual Property Organization (WIPO)A1
AU2003220289A1AustraliaA1
US6761331B2United States of AmericaB2
US2004144888A1United States of AmericaA1
EP1485668A1European Patent Office (EPO)A1
US6905093B2United States of AmericaB2
RU2004130842ARussian FederationA
RU2320952C2Russian FederationC2
EP1485668B1European Patent Office (EPO)B1
AT467807TAustriaT
ATE467807T1This recordAustriaT1
DE60332526D1GermanyD1