A multifunctional magnetic fuze is disclosed. The sensor includes an apparatus and method for counting each rotation of a projectile after firing from a weapon. A signal is generated which indicates the rotations of the projectile and a counter counts the turns so that the projectile may detonate at a predetermined nominal number of turns. The turns count may also be used to calculate spin rate and muzzle velocity so that the nominal turns count may be adjusted based on actual velocity. The fuze also may include a timer for counting a time to burst of a projectile. The turns count and/or the times count may be utilized to provide accurate detonation.

The invention relates to a safe and arm mechanism for an exploding projectile to be fired from a rifled gun. The projectile first experiences axial and angular accelera­tion which moves a setback ball (11) to initially arm the me­chanism. A third projectile parameter, angular velocity, functions to lock the ball in the armed position. During projectile flight, a spin actuated escapement mechanism moves toward a fully armed position, but may be precluded from reaching that fully armed position by a command arm arrangement. The projectile is then fully armed when a command arm signal releases the arrangement and the escape­ment mechanism is allowed to complete its motion to the fully armed position. When the projectile strikes a target, it experiences axial deceleration which moves a contact ball (17) partway to a detonating position. After the projectile passes through the target surface and into a void, e.g., into the hull of a ship, the deceleration ceases and the contact (17) ball moves under centrifugal force to a final posi­tion to detonate the projectile.

Movement of the setback ball (11) functions as one primary safety lock to preclude operation of the escape­ment mechanism. At rest, the ball (11) is positioned above a leaf spring. Axial and angular acceleration of the projec­tile depresses the spring (19) and the ball moves to another position. This motion releases the rotor (13) of the escapement mechanism. The rotor (13) is weighted so that rotation of the projectile causes it to tend to rotate. The cam follower of an electronically controlled actuator engages a cam track in the rotor and limits this rotation in stages from the fail safe position to an intermediate position where a command arming signal is required before the rotor (13) moves into the fully armed position. In the fully armed position, a contact ball (17) is brought into alignment with a switch housing.

When the projectile strikes a target and dece­lerates, the contact (17) ball moves upwardly into an annular region and when that deceleration ceases and the projectile is in a void such as inside a ship's hull, the ball (17) moves rearwardly and outwardly in the annular area connecting a pair of contacts and detonating the device some distance beyond the point of impact.

The invention relates to a safe and arm mechanism for an exploding projectile to be fired from a rifled gun. The projectile first experiences axial and angular accelera­tion which moves a setback ball (11) to initially arm the me­chanism. A third projectile parameter, angular velocity, functions to lock the ball in the armed position. During projectile flight, a spin actuated escapement mechanism moves toward a fully armed position, but may be precluded from reaching that fully armed position by a command arm arrangement. The projectile is then fully armed when a command arm signal releases the arrangement and the escape­ment mechanism is allowed to complete its motion to the fully armed position. When the projectile strikes a target, it experiences axial deceleration which moves a contact ball (17) partway to a detonating position. After the projectile passes through the target surface and into a void, e.g., into the hull of a ship, the deceleration ceases and the contact (17) ball moves under centrifugal force to a final posi­tion to detonate the projectile.

Movement of the setback ball (11) functions as one primary safety lock to preclude operation of the escape­ment mechanism. At rest, the ball (11) is positioned above a leaf spring. Axial and angular acceleration of the projec­tile depresses the spring (19) and the ball moves to another position. This motion releases the rotor (13) of the escapement mechanism. The rotor (13) is weighted so that rotation of the projectile causes it to tend to rotate. The cam follower of an electronically controlled actuator engages a cam track in the rotor and limits this rotation in stages from the fail safe position to an intermediate position where a command arming signal is required before the rotor (13) moves into the fully armed position. In the fully armed position, a contact ball (17) is brought into alignment with a switch housing.

When the projectile strikes a target and dece­lerates, the contact (17) ball moves upwardly into an annular region and when that deceleration ceases and the projectile is in a void such as inside a ship's hull, the ball (17) moves rearwardly and outwardly in the annular area connecting a pair of contacts and detonating the device some distance beyond the point of impact.

A fuze having an impact delay (15) implemented by strob- ing the count from a time-of-flight counter (26) to set a down counter (50) after an impact is sensed and then decrementing the down counter (50) to a predetermined count at which point a firing signal is passed.

A fuze having an impact delay (15) implemented by strob- ing the count from a time-of-flight counter (26) to set a down counter (50) after an impact is sensed and then decrementing the down counter (50) to a predetermined count at which point a firing signal is passed.

Die zum Zünden einer niederohmigen Zündpille (Z) erforderliche elektrische Energie wird bei kleinkalibrigen Geschossen in einem Speisekondensator (C1) gespeichert, der beim Abschuss durch einen Stromgenerator (U) aufgeladen wird. Damit beim Aufladen des Speisekondensators während des Abschusses die Zündpille nicht vorzeitig gezündet werden kann, sind Sicherheitsschaltungen angeordnet, ins besondere eine statische Sperrschaltung (B), eine dynamische Sperrschaltung (C) und eine statische Entriegelungsschaltung (A).