Fin deployment mechanism for missiles

Details Fin deployment mechanism for missiles Fin deployment mechanism for missiles

F - Mech Eng,Light,Heat,Weapons

42

B

102/5

F42B 10/14 (2006.01)

Patent

CA 1237945

ABSTRACT What is proposed by the invention is a fin deploy- ment mecanism for missiles in which a fin member can be extended from or retracted to the contour of a missile by means of a rotary to linear motion transmission system employing a rotatable screw shaft having respective ad- jacent portions embodying a left hand and a right hand thread for supporting respective ones of a pair of screw nuts, each of which are provided with a cam slot for re- ceiving a cam follower mounted on the fin member, or fin supporting member, so that when the screw shaft rotates the screw nuts are caused to move therealong in mutually opposite directions and via the cooperation between the cam slots and the cam followers the fin is caused to ro- tate through a given angle. In each of the extreme pos- itions of the fin member a locking engagement is effected for retaining such positions in a locked condition.

460554

Affiliated with

Also associated with

Rating

Fin deployment mechanism for missiles does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Fin deployment mechanism for missiles, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fin deployment mechanism for missiles will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1327309