Patent ID: 7430964

Claim:
A method for operating a safe and arm detonation device comprising the steps of: applying a pulling force to an arming lanyard attached to a sealing plug, wherein said sealing plug is in direct contact with a firing pin; releasing said firing pin by breaking a shear pin in contact with said firing pin wherein said pulling force when applied to said arming lanyard causes a first translational movement of said firing pin and said first translational movement of said sealing plug away from said firing pin; opening a high pressure path for a high pressure air movement into a diaphragm, wherein said high pressure air movement flows into and inflates said diaphragm when said sealing plug is removed away from said firing pin; opening a low pressure path for a low pressure air movement, wherein said low pressure air movement is caused by an inflation of said diaphragm; moving a piston in a straight line motion using an inflation force generated by the inflation of said diaphragm; opposing the straight line motion of said piston using a biasing spring in contact with said piston, said biasing spring opposing the straight line motion of said piston until a compression force which compresses said biasing spring is attained; compressing a drive spring positioned in a drive shaft, wherein said drive spring is compressed by said straight line motion of said piston which pushes against said drive shaft causing a second translational movement of said drive shaft; rotating a rotor from a safe position to an armed position by converting said second translational movement of said drive shaft to rotational movement of said rotor, wherein said rotor includes a plurality of electrically initiated detonators, said detonators being connected to a plurality of shorting contacts when said rotor is in the safe position and aligned with a plurality of detonating contacts when said rotor is in said armed position, said rotor being axially aligned with said diaphragm, said firing pin, said biasing spring and said drive shaft; adjusting a rate of air exhaustion from a low pressure area connected to said low pressure path utilizing an exhaust regulator located within said low pressure path, wherein said rate of air exhaustion determines a time period required for said rotor to rotate from said safe position to said armed position; and detonating said plurality of electrically initiated detonators with an electrical pulse generated by piezo crystals when said rotor is in the armed position and said piezo crystals are impacted by said firing pin which causes said electrically initiated detonators to detonate.