Fin erection mechanism
AssigneeGeneral Dynamics Corporation
InventorLadislao Pazmany
Life of this patent
Estimating the term…
Abstract
A plurality of fins for a missile which are capable of being folded to conform to the general cylindrical contour of the missile body and which are biased to unfold to an erect position and which includes an interconnection mechanism for connecting all the fins together to ensure simultaneous erection and for distributing the erection moment of individual fins to all fins; said interconnection means further being capable of acting without interfering with the movement of the fins for flight control without need for disengagement after erection.
Claims7
Fin erection mechanism for a missile having a longitudinally cylindrical body frame and a plurality of foldable fins for flight control comprising,
- means longitudinally of said missile for connecting said fins to said missile,
- means for bracing said fins toward an erect position,
- means for interconnecting said fins together so that erection of all of said fins occurs simultaneously, said means for interconnecting comprises cable means for connecting one fin to fins located on each side of said one fin so that erection of said one fin influences the erection of said finds located on each side of one fin,
- each fin of said fins is formed with a pulley means and wherein said cable means is attached and guided by said pulley means during the erection of said fins, and
- control means disposed radially of said main axis of said missile for rotating said fins while erected for flight control and wherein said pulley means is located on the axis of rotation of said control means so that said cable means do not interfere with limited rotation of said fins.
Dependencies are inferred from the claim text.