Torsion spring powered missile wing deployment system

Details Torsion spring powered missile wing deployment system Torsion spring powered missile wing deployment system

B - Operations, Transporting

64

C

102/5

B64C 3/56 (2006.01) F42B 10/18 (2006.01)

Patent

CA 1306384

13 Title of the Invention: TORSION SPRING POWERED MISSILE WING DEPLOYMENT SYSTEM Inventor: Arthur M. Frank ABSTRACT OF THE DISCLOSURE A foldable missile wing is deployed by means of an overcenter linkage powered by a torsion spring assembly capable of exerting a generally linear bias on the linkage over its full range of motion. A separate lock linkage maintains the foldable wing in a deployed position until release actuation of the lock linkage occurs thereby enabling wing deployment. .

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