Deployment and drive device for projectile control surfaces
View Patent ↗A deployment and orientation device for projectile control surfaces, the deployment being carried out by means of springs between a loading position in which the control surfaces are folded inside the projectile and held against the action of the spring means using blocking means, and a deployed position in which the control surfaces may be oriented with respect to the projectile, device wherein it incorporates motors ensuring firstly the deployment of the control surfaces and secondly their orientation, the blocking means for the control surfaces being single means ensuring the immobilization of all the control surface and enabling them to be released simultaneously, the blocking means being immobilized by first locking means released by the pivoting of the bodies of the motors.
1. A deployment and orientation device for control surfaces for a projectile, said device, comprising:
springs means for deploying said control surfaces from a loaded position in which said control surfaces are folded inside a projectile, to a deployed position in which said control surfaces extend externally from a projectile;
a pair of motors each having a shaft rotatably supported in a motor body, which motor body is capable of rotation about its longitudinal axis for acting in combination with said spring means to deploy said control surfaces;
blocking means for immobilizing said control surfaces and releasing them simultaneously; and
first locking means for holding and releasing said blocking means from an immobilizing position by rotating the bodies of said motors.
2. The device according to claim 1 , said first locking means comprising fingers activated by a spring and cooperating with a ring integral with the body of each motor.
3. The device according to claim 2 , each ring has a notch for receiving an end of one of said fingers, wherein the displacement of all of said fingers releases said blocking means and prevents the rotation of said bodies of said motors.
4. The device according to claim 1 , wherein two of said control surfaces are connected to a control shaft to be located transverse to a projectile, said motors for rotating each shaft.
5. The device according to claim 4 , said motor connected to said control shaft with a lever for acting on a rod connected to said shaft.
6. The device according to claim 4 , each said projectile control surfaces are connected to said control shaft with a support and an arm articulated with respect to said support.
7. The device according to claim 6 , further comprising a spring for acting upon said arm to rotate each of said projectile control surfaces with respect to said support.
8. The device according to claim 7 , further comprising second locking means for locking said projectile control surfaces and said support in said deployed position.
9. The device according to claim 8 , said second locking means comprising a pin positioned in a drill hole in each of said projectile control surfaces for connecting each of said projectile control surfaces with said support.