Arming delay, dual environment safe, fuze
AssigneeGeneral Electric Company
InventorRichard T. Ziemba
Life of this patent
Estimating the term…
Abstract
This invention provides a safing and arming mechanism for a fuze for a spinning projectile including a ball rotor journaled for rotation within a cavity in the fuze. A firing pin, said cavity and a booster charge lie along the longitudinal axis of the fuze. The rotor carries a stab sensitive detonator in its diametral bore. A first spring mounted on a first seat cut into the ball normally fixes the ball with the detonator, out of alignment with the longitudinal axis of the fuze. A second spring mounted on a second seat cut into the ball also fixes the ball out of alignment. To release the ball, the first spring must be shifted aftwardly by setback force to a third seat cut into the ball, and the second spring must be enlarged by centrifugal force and removed from said second seat.
Claims5
A delay armed fuze having a safed disposition and an armed disposition for a spinning projectile, comprising:
- a housing having a longitudinal axis extending fore and aft, and a substantially spherical cavity therein which is symmetrical about said axis, and has a first annular face and a second annular face;
- a substantially spherical rotor disposed in said cavity having an axis of mass symmetry and a diametral bore coaxial therewith and adapted to receive a detonating charge therein;
- a first annular groove formed into the periphery of said rotor perpendicular to a first diametrical axis, which first diametrical axis is angularly displaced from said axis of mass symmetry, and which first diametrical axis in the safed disposition, is coaxial with said housing longitudinal axis, and said groove is spaced aftwardly of said diametral bore;
- a second annular groove formed into the periphery of said rotor perpendicular to said first diametrical axis, and spaced forwardly of said diametral bore;
- a third annular groove formed into the periphery of said rotor perpendicular to said first diametrical axis, and spaced forward of said diametrical bore and adjacent and aftward of said second groove;
- a first annular cavity formed into said housing substantially coplanar with said first annular groove in said rotor;
- first means disposed in part in said first annular groove and engaged with said housing first face to preclude rotation of said rotor;
- second means disposed in part in said second annular groove and engaged with said housing second face to preclude rotation of said rotor;
- said fuze having a mode of operation wherein:
- upon set-back of said fuze, said second means to preclude rotation moves from said second annular groove to said third annular groove to disengage said second face, and
- upon spin-up of said fuze, said first means to preclude rotation moves from said first annular groove to said first annular cavity to disengage said first face,
- whereupon said rotor is free to rotate from said safed disposition to said armed disposition.
Dependencies are inferred from the claim text.