Deployable wing mechanism

B - Operations – Transporting – 64 – C

Patent

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Details

244/44, 244/1.5

B64C 3/56 (2006.01) F42B 10/14 (2006.01)

Patent

CA 1113070

ABSTRACT A deployable wing assembly using an inner wing segment and an outer wing segment with the inner wing segment hinged longitudinally to the body of a missile, or the like, and with the outer wing segement hinged by a pin perpendicular to the surface of the wing segments at the junction, and including deploying means and locking means for both sections.

341765

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