US3112704A - Self-destroying fuze for a spinning projectile - Google Patents
Self-destroying fuze for a spinning projectile Download PDFInfo
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- US3112704A US3112704A US77865A US7786560A US3112704A US 3112704 A US3112704 A US 3112704A US 77865 A US77865 A US 77865A US 7786560 A US7786560 A US 7786560A US 3112704 A US3112704 A US 3112704A
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- slide member
- perforation
- pin
- striker pin
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/14—Double fuzes; Multiple fuzes
- F42C9/16—Double fuzes; Multiple fuzes for self-destruction of ammunition
- F42C9/18—Double fuzes; Multiple fuzes for self-destruction of ammunition when the spin rate falls below a predetermined limit, e.g. a spring force being stronger than the locking action of a centrifugally-operated lock
Definitions
- the invention relates to a self-destroying fuze for spinning projectiles more especially the invention relates to self-destroying fuzes having means whereby the detonation of the fuze is prevented until after a predetermined interopposing the action of a spring adapted to displace the firing pin in the axial direction of the projectile to detonate As the rotation of the projectile decreases the the striker pin is then forced against the detonator to explode the projectile.
- the invention aims to overcome this drawback by providing means to ensure a substantial safety margin before the mechanism is cocked or armed.
- the said means also ensures'that the projectile can be safely transported. This is achieved by providing a slide block for the axial movement of the striker pin in the securing or safety position, said slider being pressed against the shank of the striker pin by'the centrifugal forceon rotation of the projectile and its'centre of gravity being altered by the action of a. ball whereby the slide is displaced laterally by the centrifugal force so as to free the firing pin for the axial movement.
- the ball is retained by theforces of inertia and rests on the bottom of a borein a slide-supporting body disposed behind the slide, the wall of said bore being advantageously inclined outwardly through a' small angle with respect to the axis of the striker pin.
- the supporting body advantageously consists of plastic, but may also be made of any other suitable material.
- the slide may be surrouned by a band spring securing it in the locking position andexpandible radially outwards by centrifugal force so as to release said slide.
- the firing pin has projections which engage in corresponding recesses in the slide, in the locking position of the slide.
- FIGURE 1 is. a longitudinal section of a fuze of a projectile according to one embodiment of the invention.
- FIGURE 2 is a cross-section on line 22 of FIGURE
- FIGURE 3 is a longitudinal section of fuze of a pro- I to a; second embodiment of 'the'inven-
- equivalent parts designated by the same reference numerals.
- the fuze illustrated in the drawings is composed of two main structural groups, namely the group containing the self-destroying system and the group containing the safety-margin device.
- the self-destroying system is located in the screw cap 1, while the safety-margin device is housed in the fuze body 2.
- the self-destroying system comprises a sleeve 3 having a conical bearing surface 3', a ball carrier consisting of an upper part 4 and a lower part 4' with balls 5 and a spring 6.
- a pin 7 is provided connected to a guidehead 8 which is mounted in the nose of the cap 1.
- the safety-margin device comprises a slide 9 surrounding an extension of the firing or striker pin 7', and a. slide-supporting body Iii disposed behind said slide and mounted in the fuze body 2.
- the striker pin 7' has an abutment or shoulder 11 which rests against the slide 9 in the locking position.
- the slide 9 has a through bore 12 the axis of which extends parallel to the longitudinal axis of the fuze and to the longitudinal axis of the pin 7. Behind said bore 12 there is located in the slide-supporting body It ⁇ a guideway 13 which as shown comprises a through bore in which is located a ball 14. The wall of the guideway or bore 13 is inclined outwardly by a small amount with respect to the longitudinal axis of the fuze.
- the slide 9 is surrounded by a band spring 16 whichholds two pins 20 in a position locking the slide 9 to the slide supporting body 10.
- band spring 16 expands still more and the ball 5 of the self-destroying system tend to fly radially outward and to press the upper part 4 of the ball carrier against the pre-tensioned spring 6.
- the ball 14 begins to roll upwardly in the bore 13 in the body 10.
- the time the ball 14 takes to reach the upper end of the bore 13 is determined by the angle of inclination of the bore and its axial length.
- the ball'14 eventually enters v I the bore 12 in the slide 9 and effects a displacement. of the centre of gravity of the slide and ball through in the direction of the side where the ball inlet is located. Under the action of centrifugal force, the slide 9 and ball 14 are displaced radially outwards out of engagement with are the abutment 11 of the striker pin 7, whereby the locking of the striker pin 7 is terminated.
- the pin 7 and the striker pin 7 is driven into the detonator 18. If the target is missed, the speed of the projectile decreases steadily owing to air friction and after a predetermined distance, the limit of speed at which the self-destruction occurs is reached.
- the centrifugal force acting on the balls has now become so small that it is no longer suliicient to balance the force of the spring 6. The latter is able to expand and exert pressure on the parts 4, 4, 5 and 11, to drive the striker pin 7' into the detonator 13. in this way, the self-destruction of the fuze is effected.
- the slide 9 engages the shank of the striker pin 7 and acts as a guide to keep it entral whereby the sliding of the projections It? out of the recesses 19 in the slide 9 is facilitated.
- the slide supporting body member it may be made of synthetic plastic.
- a fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and connected to said striker pin and being slidably guided into said fuze casing for a movement to and fro relative to said detonator, a sleeve disposed concentrically around said pin, said sleeve having in a direction opposite to said detonator a conical surface directed outwardly, a plurality of first balls arranged around said secondmentioned pin above said conical surface and resting on said conical surface before the firing of the projectile, a cage for said balls to hold them in position, a spring abutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided in said fuze casing and in said sleeve for movement to and fro relative to said deton
- a fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and secured to said striker pin and being slidably guided into said fuze casing for movement to and fro relative to said detonator, a sleeve disposed concentrically around said pin, said sleeve having a conical surface directed outwardly in a direction opposite to said detonator, a plurality of balls arranged around said second-mentioned pin above said conical surface and resting on said conical surface before firing the projectile, a cage for said balls to hold them in position, said cage being secured to said secondmentioned pin, a spring abutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided for movement to and fro of said detonator caused by running outwardly
- a fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and connected to said striker pin and being slidably guided into said fuze casing for movement to and fro, a sleeve disposed concentrically around said pin, said sleeve having a conical surface directed outwardly in a direction opposite to said detonator, a plurality of balls arranged around said second-mentioned pin above said conical surface and I resting on said conical surface before firing the projectile,
- a cage for holding said balls, said cage being secured to said second-mentioned pin, a springabutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided for movement to and fro caused by running outwardly of said balls along said conical surface of said sleeve under centrifugal force against the force of said spring, a single slide member slidably guided in said fuze casing for movement transversely to said striker pin, an axial perforation of said slide member fitting substantially half around said striker pin, said striker pin extending through said perforation of said slide member, an abutment arranged between said striker pin and said secondmentioned pin and connected thereto, said abutment having a cross'sectional area overlapping said perforation of said slide member and said abutment resting then with its underside on said slide member, said slide member having a second axial perforation extending transversely from said first-mentioned
- a fuze for spinning projectiles according to claim 4, in which said body guiding said slide member is composed of a plastic material.
Description
Dec. 3, 1963 F. SCHAADT SELF-DESTROYING FUZE FOR A SPINNING PROJECTILE Filed Dec. 23, 1960 3 Sheets-Sheet 1 Fig.1-
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F. SCHAADT Dec. 3, 1963 SELF DESTROYING FUZE FOR A SPINNING PROJECTILE 3 Sheets-Sheet 2 Filed Dec. 23, 1960 Jn vehfor: F 1-2722 'Jcllzzalt v the fuze.
' force of the striker pin spring overcomes that of the balls l in the directionof the arrows;
United States Patent 3,112,764 SELF-DESTROYING FUZE FQR A SPINNING I ROIEQTILE Franz Schaadt, Dusseldorf, Germany, assignor to Firrna Iihcinmetall G.m.b.H., Dusseldorf, Germany Filed Dec. 23, 1960, Ser. No. 77,865 Claims. (Ci. 102-71) The invention relates to a self-destroying fuze for spinning projectiles more especially the invention relates to self-destroying fuzes having means whereby the detonation of the fuze is prevented until after a predetermined interopposing the action of a spring adapted to displace the firing pin in the axial direction of the projectile to detonate As the rotation of the projectile decreases the the striker pin is then forced against the detonator to explode the projectile. In these known constructions, the cocking or arming of the striker pin is effected by the action of the centrifugal forces and the drawback of this is thanwhen the striker pin is cocked the projectile starts immediately to rotate on leaving the gun barrel and accordingly the safety margin is very small and thus if the projectile should strike an object a few metres after leaving the gun barrel it would be exposed with disastrous results to the gun crew.
The invention aims to overcome this drawback by providing means to ensure a substantial safety margin before the mechanism is cocked or armed. The said means also ensures'that the projectile can be safely transported. This is achieved by providing a slide block for the axial movement of the striker pin in the securing or safety position, said slider being pressed against the shank of the striker pin by'the centrifugal forceon rotation of the projectile and its'centre of gravity being altered by the action of a. ball whereby the slide is displaced laterally by the centrifugal force so as to free the firing pin for the axial movement. During the acceleration of the projectile on firing, the ball is retained by theforces of inertia and rests on the bottom of a borein a slide-supporting body disposed behind the slide, the wall of said bore being advantageously inclined outwardly through a' small angle with respect to the axis of the striker pin. The supporting body advantageously consists of plastic, but may also be made of any other suitable material.
According to one embodiment, the slide may be surrouned by a band spring securing it in the locking position andexpandible radially outwards by centrifugal force so as to release said slide.
According to another embodiment, in which there is ,no spring, the firing pin has projections which engage in corresponding recesses in the slide, in the locking position of the slide.
Details of the invention will now be described with reference to the accompanying drawings in which:
FIGURE 1 is. a longitudinal section of a fuze of a proiectile according to one embodiment of the invention;
FIGURE 2 is a cross-section on line 22 of FIGURE "FIGURE 3 is a longitudinal section of fuze of a pro- I to a; second embodiment of 'the'inven- In the accompanying drawings, equivalent parts designated by the same reference numerals.
The fuze, illustrated in the drawings is composed of two main structural groups, namely the group containing the self-destroying system and the group containing the safety-margin device.
The self-destroying system is located in the screw cap 1, while the safety-margin device is housed in the fuze body 2. r V
The self-destroying system comprises a sleeve 3 having a conical bearing surface 3', a ball carrier consisting of an upper part 4 and a lower part 4' with balls 5 and a spring 6. A pin 7 is provided connected to a guidehead 8 which is mounted in the nose of the cap 1.
The safety-margin device comprises a slide 9 surrounding an extension of the firing or striker pin 7', and a. slide-supporting body Iii disposed behind said slide and mounted in the fuze body 2.
The striker pin 7' has an abutment or shoulder 11 which rests against the slide 9 in the locking position. The slide 9 has a through bore 12 the axis of which extends parallel to the longitudinal axis of the fuze and to the longitudinal axis of the pin 7. Behind said bore 12 there is located in the slide-supporting body It} a guideway 13 which as shown comprises a through bore in which is located a ball 14. The wall of the guideway or bore 13 is inclined outwardly by a small amount with respect to the longitudinal axis of the fuze. a
To permit the slide 9 to shift radially with respect to the striker pin '7', it has a bore 15 which affords th necessary space for this radial movement.
In the embodiment illustrated in FIGURES 1 and 2 the slide 9 is surrounded by a band spring 16 whichholds two pins 20 in a position locking the slide 9 to the slide supporting body 10.
In the embodiment illustrated in FIGURES 3 and 4 no spring such as 16, is provided. Instead, the abutment or shoulder 11 of the striker pin 7' has projections 17 on its side facing the slide, said projections engaging in correas long as the forces of inertia operate, all the axially Y movable parts of the fuze remain blocked in the position 7 illustrated, that is in the locking position. The centrifugal forces occurring as a result of the incipient rotation of the projectile, however cause an expansion of the band spring 16, and at the same time cause the pins ZO'to move radially outwardly and to release the slide 9. The slide 9 I is caused to exert a pressure against the striker pin 7', whereby the slide is held in engagement under the shoulder 11 and the securing action is maintained. On cessation of the acceleration of translation andthe full speed of ro-;
tation being reached at the mouth of the gun barrel, forces of inertia no longer act on the parts of the fuze, but centrifugal forces come into full play. In consequence, the
If the projectile hits the target, the pin 7 and the striker pin 7 is driven into the detonator 18. If the target is missed, the speed of the projectile decreases steadily owing to air friction and after a predetermined distance, the limit of speed at which the self-destruction occurs is reached. The centrifugal force acting on the balls has now become so small that it is no longer suliicient to balance the force of the spring 6. The latter is able to expand and exert pressure on the parts 4, 4, 5 and 11, to drive the striker pin 7' into the detonator 13. in this way, the self-destruction of the fuze is effected.
In the embodiment according to FIGURES 3 and 4 the initial operation will be substantially as described above in connection with FIGURES 1 and 2. In this case however in order to release the locking action of the striker pin the projections 17 on the striker-pin have to be pushed out of the recesses 19 in the slide 9. This is done by the pin 7 and the striker pin '7' being lifted, when the full speed of rotation is reached, by the action of the outwardly flying balls 5 in opposition to the pressure of the spring 6 which results in the raising of the bail carrier 4, 4 since said ball carrier is fixedly connected to the pin 7.
During the initial stages of the lifting of the pin 7 y the outwardly flying balls 5, the slide 9 engages the shank of the striker pin 7 and acts as a guide to keep it entral whereby the sliding of the projections It? out of the recesses 19 in the slide 9 is facilitated.
The slide supporting body member it may be made of synthetic plastic.
I claim:
1. A fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and connected to said striker pin and being slidably guided into said fuze casing for a movement to and fro relative to said detonator, a sleeve disposed concentrically around said pin, said sleeve having in a direction opposite to said detonator a conical surface directed outwardly, a plurality of first balls arranged around said secondmentioned pin above said conical surface and resting on said conical surface before the firing of the projectile, a cage for said balls to hold them in position, a spring abutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided in said fuze casing and in said sleeve for movement to and fro relative to said detonator caused by running outwardly of said balls along said conical surface of said sleeve under centrifugal force against the force of said spring, a single slide member guided in said fuze casing for a movement transversely to said striker pin, said slide member having an axial perforation therein fitting substantially half around said striker pin, said striker pin extending through said perforation of said slide member, an abutment arranged between said striker pin and said second-mentioned pin and connected to said striker pin, said abutment having a cross sectional area overlapping said perforation of said slide member and said abutment rests with its underside on said slide member, said slide member having a second axial perforation extending transversely from said first-mentioned perforation, said second perforation having a cross sectional area larger than the cross sectional area of said abutment so that said abutment can pass through when said slide member is moving transversely with its firstmentioned perforation away from said striker pin, said slide member having a hole therein at least open towards said detonator and disposed diametrically to said secondmentioned perforation, said slide member having a center of gravity arranged radially out of the axis of said firstmentioned perforation in a direction toward said second-mentioned perforation so that under centrifugal force said slide member will be urged transversely towards said striker pin, a second ball disposed before firing of the projectile in said fuze casing between said detonator and said slide member, a guide way for said second-mentioned ball directed toward said hole in said slide member, said guide way being disposed substantially axially but slightly inclined outwardly toward said hole of said slide member so that by centrifugal force said secondmentioned ball is forced to move toward said slide member and to enter said hole of said slide member, said slide member and said second-mentioned ball being dc signed so that by entering of said second-mentioned ball into said hole the center of gravity of said slide member changes across the axis of said first-mentioned perforation toward said hole causing by centrifugal force a transverse movement of said slide member away from said striker pin and bringing said second-mentioned perforation in a position for passing through of said abutment.
2. A fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and secured to said striker pin and being slidably guided into said fuze casing for movement to and fro relative to said detonator, a sleeve disposed concentrically around said pin, said sleeve having a conical surface directed outwardly in a direction opposite to said detonator, a plurality of balls arranged around said second-mentioned pin above said conical surface and resting on said conical surface before firing the projectile, a cage for said balls to hold them in position, said cage being secured to said secondmentioned pin, a spring abutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided for movement to and fro of said detonator caused by running outwardly of said balls along said conical surface of said sleeve under centrifugal force against the force of said spring, a single slide member slidably guided in said fuze casing for movement transversely to said striker pin, said slide member having an axial perforation therein fitting substantially half around said striker pin, said striker pin extending through said first perforation of said slide member, an abutment arranged between said striker pin and said second-mentioned pin and connected to both pins, said abutment having a cross sectional area overlapping said perforation of said slide member and said abutment resting then with its underside on said slide member, said slide member having a second axial perforation extending transversely from said first-mentioned perforation, said second-mentioned perforation having a cross sectional area larger than the cross sectional area of said abutment so that said abutment can pass through when said slide member is moving transversely with its first-mentioned perforation away from said striker pin, said slide member having a hole therein extending in a substantially axial direction at least open towards said detonator and disposed diametrically to said second-mentioned perforation, said slide member having a center of gravity situated radially out of the axis of said first-mentioned perforation and toward said second-mentioned perforation so that under centrifugal force said slide member is pressed transversely toward said striker pin, a second ball disposed before firing of the projectile in said fuze casing between said detonator and said slide member, a guide way for said second-mentioned ball directed toward said hole in said slide member, said guide way being disposed substantially axially but slightly inclined relative to said hole of said slide member so that by centrifugal force said second-mentioned ball is forced to move toward said slide member and to enter said hole of said slide member, said slide member and said secondmentioned ball being designed so that by entering of said second-mentioned ball into said hole the center of gravity of said slide member changes across the axis of said firstmentioned perforation toward said hole causing by centrifugal force a transverse movement of said slide member away from said striker pin and bringing said secondmentioned perforation in a position for passing through of said abutment.
3. A fuze for spinning projectiles comprising in combination a detonator, a fuze casing, a striker pin axially slidably guided in said fuze casing, a pin arranged axially and connected to said striker pin and being slidably guided into said fuze casing for movement to and fro, a sleeve disposed concentrically around said pin, said sleeve having a conical surface directed outwardly in a direction opposite to said detonator, a plurality of balls arranged around said second-mentioned pin above said conical surface and I resting on said conical surface before firing the projectile,
a cage for holding said balls, said cage being secured to said second-mentioned pin, a springabutting at one end in said fuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided for movement to and fro caused by running outwardly of said balls along said conical surface of said sleeve under centrifugal force against the force of said spring, a single slide member slidably guided in said fuze casing for movement transversely to said striker pin, an axial perforation of said slide member fitting substantially half around said striker pin, said striker pin extending through said perforation of said slide member, an abutment arranged between said striker pin and said secondmentioned pin and connected thereto, said abutment having a cross'sectional area overlapping said perforation of said slide member and said abutment resting then with its underside on said slide member, said slide member having a second axial perforation extending transversely from said first-mentioned perforation, said second-mentioned perforation having a cross sectional area larger than the cross sectional area of said abutment so that said abutment can pass through when said slide member is moving transversely with its first-mentioned perforation away from said striker pin, said slide member having a groove around 7 said first-mentioned perforation, projections on the underside of said abutment gripping in said groove of said slide member before firing the projectile and holding said slide member in a transverse direction, said slide member hav- -ing a hole therein at least open towards said detonator and disposed diametrically to said second-mentioned perforation, said slide member having a center of gravity being situated radially out of the axis of said first-mentioned perforation toward said second perforation so that under centrifugal force said slide member is pressed transversely relative to said striker pin, a second ball disposed before firing of the projectile in said fuze casing between said detonator and said slide member, a guide way for said second-mentioned ball directed toward said hole in said slide member, said guide way being disposed substantially axially but slightly inclined outwardly to said hole of said slide member so that by centrifugal force said second ball is forced to move toward said slide member and to enter said hole of said slide member, said slide member and said second-mentioned ball being designed so that by entering of said second-mentioned ball into said hole the center of gravity of said slide member changes directed outwardly in a direction opposite to said detona tor, a plurality of balls arranged around said pin above them therein, a spring abutting at one end in said ttuze casing and the other end against said cage on its side opposite to said detonator, said cage being guided for a movement caused by running outwardly of said balls along said conicai surface of said sleeve under centrifugal force against the force of said spring, a single slide member slidably guided in said fuze casing, said slide member having an axial perforation fitting substantially half around said striker pin, said striker pin extending through said perforation of said slide member, an abutment arranged between said striker pin and said second-mentioned pin and connected to said striker pin, said abutment having a cross sectional area overlapping said perforation of said slide member and said abutment resting then with its underside on said siide member, said slide member having a second axial perforation extending transversely from said first-mentioned perforation, said second-mentioned perforation having a cross sectional area larger than the cross sectional area of said abutment so that said abutment can pass through when said slide member is moving transversely with its first-mentioned perforation away from said striker pin, said slide member having a hole therein at least open towards said detonator and disposed diametrically to said second-mentioned perforation, said slide member having a center of gravity being situated radially out of the axis of said first-mentioned perforation toward said second-mentioned perforation so that under centrifugal force said slide member will be forced toward said striker pin, a second ball disposed before firing of the projectile in said fuze casing between said detonator and said slide member, a guide way for said second-mentioned ball directed toward said hole in said slide member, said guide way being disposed substantially axially but slightly inclined outwardly to said hole of said slide member so that by centrifugal fonce said second-mentioned ball is forced to move to enter said hole of said slide member, said slide member and said second-mentioned bal-l being designed so that by entering of said secondmentioned ball into said hole the center of gravity of said slide member changes across the axis of said first-mentioned perforation toward said hole causing by centrifugal force a transverse movement of said slide member away from said striker pin and bringing said second-mentioned perforation in a position so that said abutment can pass therethrough, a body disposed inside said fuze casing and guiding said slide member in transverse direction, said guide way for said second-mentioned ball being formed in said body, said cage resting on the upperside of said abutment transmitting the force of said spring to said abutment.
5. A fuze for spinning projectiles according to claim 4, in which said body guiding said slide member is composed of a plastic material.
References (iited in the file of this patent UNITED STATES PATENTS 2,405,653 Honger Aug. 13, 1946 2,650,541 Rosselet Sept. 1, 1953 2,871,788 Guerne Feb. 3, 1959 2,896,540 Vo land July 28,1959
FOREIGN PATENTS 113,992 Sweden May 2, 1945 1,087,643 France Aug. 25, 1954-
Claims (1)
1. A FUZE FOR SPINNING PROJECTILES COMPRISING IN COMBINATION A DETONATOR, A FUZE CASING, A STRIKER PIN AXIALLY SLIDABLY GUIDED IN SAID FUZE CASING, A PIN ARRANGED AXIALLY AND CONNECTED TO SAID STRIKER PIN AND BEING SLIDABLY GUIDED INTO SAID FUZE CASING FOR A MOVEMENT TO AND FRO RELATIVE TO SAID DETONATOR, A SLEEVE DISPOSED CONCENTRICALLY AROUND SAID PIN, SAID SLEEVE HAVING IN A DIRECTION OPPOSITE TO SAID DETONATOR A CONICAL SURFACE DIRECTED OUTWARDLY, A PLURALITY OF FIRST BALLS ARRANGED AROUND SAID SECOND-MENTIONED PIN ABOVE SAID CONICAL SURFACE AND RESTING ON SAID CONICAL SURFACE BEFORE THE FIRING OF THE PROJECTILE, A CAGE FOR SAID BALLS TO HOLD THEM IN POSITION, A SPRING ABUTTING AT ONE END IN SAID FUZE CASING AND THE OTHER END AGAINST SAID CAGE ON ITS SIDE OPPOSITE TO SAID DETONATOR, SAID CAGE BEING GUIDED IN SAID FUZE CASING AND IN SAID SLEEVE FOR MOVEMENT TO AND FRO RELATIVE TO SAID DETONATOR CAUSED BY RUNNING OUTWARDLY OF SAID BALLS ALONG SAID CONICAL SURFACE OF SAID SLEEVE UNDER CENTRIFUGAL FORCE AGAINST THE FORCE OF SAID SPRING, A SINGLE SLIDE MEMBER GUIDED IN SAID FUZE CASING FOR A MOVEMENT TRANSVERSELY TO SAID STRIKER PIN, SAID SLIDE MEMBER HAVING AN AXIAL PERFORATION THEREIN FITTING SUBSTANTIALLY HALF AROUND SAID STRIKER PIN, SAID STRIKER PIN EXTENDING THROUGH SAID PERFORATION OF SAID SLIDE MEMBER, AN ABUTMENT ARRANGED BETWEEN SAID STRIKER PIN AND SAID SECOND-MENTIONED PIN AND CONNECTED TO SAID STRIKER PIN, SAID ABUTMENT HAVING A CROSS SECTIONAL AREA OVERLAPPING SAID PERFORATION OF SAID SLIDE MEMBER AND SAID ABUTMENT RESTS WITH ITS UNDERSIDE ON SAID SLIDE MEMBER, SAID SLIDE MEMBER HAVING A SECOND AXIAL PERFORATION EXTENDING TRANSVERSELY FROM SAID FIRST-MENTIONED PERFORATION, SAID SECOND PERFORATION HAVING A CROSS SECTIONAL AREA LARGER THAN THE CROSS SECTIONAL AREA OF SAID ABUTMENT SO THAT SAID ABUTMENT CAN PASS THROUGH WHEN SAID SLIDE MEMBER IS MOVING TRANSVERSELY WITH ITS FIRSTMENTIONED PERFORATION AWAY FROM SAID STRIKER PIN, SAID SLIDE MEMBER HAVING A HOLE THEREIN AT LEAST OPEN TOWARDS SAID DETONATOR AND DISPOSED DIAMETRICALLY TO SAID SECONDMENTIONED PERFORATION, SAID SLIDE MEMBER HAVING A CENTER OF GRAVITY ARRANGED RADIALLY OUT OF THE AXIS OF SAID FIRSTMENTIONED PERFORATION IN A DIRECTION TOWARD SAID SECOND-MENTIONED PERFORATION SO THAT UNDER CENTRIFUGAL FORCE SAID SLIDE MEMBER WILL BE URGED TRANSVERSELY TOWARDS SAID STRIKER PIN, A SECOND BALL DISPOSED BEFORE FIRING OF THE PROJECTILE IN SAID FUZE CASING BETWEEN SAID DETONATOR AND SAID SLIDE MEMBER, A GUIDE WAY FOR SAID SECOND-MENTIONED BALL DIRECTED TOWARD SAID HOLE IN SAID SLIDE MEMBER, SAID GUIDE WAY BEING DISPOSED SUBSTANTIALLY AXIALLY BUT SLIGHTLY INCLINED OUTWARDLY TOWARD SAID HOLE OF SAID SLIDE MEMBER SO THAT BY CENTRIFUGAL FORCE SAID SECONDMENTIONED BALL IS FORCED TO MOVE TOWARD SAID SLIDE MEMBER AND TO ENTER SAID HOLE OF SAID SLIDE MEMBER, SAID SLIDE MEMBER AND SAID SECOND-MENTIONED BALL BEING DESIGNED SO THAT BY ENTERING OF SAID SECOND-MENTIONED BALL INTO SAID HOLE THE CENTER OF GRAVITY OF SAID SLIDE MEMBER CHANGES ACROSS THE AXIS OF SAID FIRST-MENTIONED PERFORATION TOWARD SAID HOLE CAUSING BY CENTRIFUGAL FORCE A TRANSVERSE MOVEMENT OF SAID SLIDE MEMBER AWAY FROM SAID STRIKER PIN AND BRINGING SAID SECOND-MENTIONED PERFORATION IN A POSITION FOR PASSING THROUGH OF SAID ABUTMENT.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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FR847646A FR1276499A (en) | 1960-12-21 | 1960-12-21 | Self-destructing rocket with safety margin |
US77865A US3112704A (en) | 1960-12-23 | 1960-12-23 | Self-destroying fuze for a spinning projectile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77865A US3112704A (en) | 1960-12-23 | 1960-12-23 | Self-destroying fuze for a spinning projectile |
Publications (1)
Publication Number | Publication Date |
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US3112704A true US3112704A (en) | 1963-12-03 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US77865A Expired - Lifetime US3112704A (en) | 1960-12-21 | 1960-12-23 | Self-destroying fuze for a spinning projectile |
Country Status (1)
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US (1) | US3112704A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3249051A (en) * | 1963-11-12 | 1966-05-03 | Junghans Geb Ag | Self-destroying fuze for rotating projectiles |
US3347166A (en) * | 1965-04-02 | 1967-10-17 | Mefina Sa | Fuse for a missile to be fired by a gun with rifled bore |
US3353489A (en) * | 1965-02-26 | 1967-11-21 | Rheinmetall Gmbh | Impact fuze for a spinning projectile |
US4040358A (en) * | 1965-12-14 | 1977-08-09 | Avco Corporation | Hydraulic delayed arming fuze |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE113992C1 (en) * | 1943-03-05 | 1945-05-02 | ||
US2405653A (en) * | 1940-07-09 | 1946-08-13 | Honger Guido | Fuse for automatic destruction of shells |
US2650541A (en) * | 1948-05-28 | 1953-09-01 | Rosselet Jean | Fuze |
FR1087643A (en) * | 1952-11-21 | 1955-02-25 | Oerlikon Buehrle Ag | Safety devices for projectile initiation rockets |
US2871788A (en) * | 1955-05-24 | 1959-02-03 | Brevets Aero Mecaniques | Impact fuzes for explosive projectiles including a mechanical self-destruction device |
US2896540A (en) * | 1954-12-06 | 1959-07-28 | Voland Andre | Control device for the percussion pin of a projectile fuse |
-
1960
- 1960-12-23 US US77865A patent/US3112704A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405653A (en) * | 1940-07-09 | 1946-08-13 | Honger Guido | Fuse for automatic destruction of shells |
SE113992C1 (en) * | 1943-03-05 | 1945-05-02 | ||
US2650541A (en) * | 1948-05-28 | 1953-09-01 | Rosselet Jean | Fuze |
FR1087643A (en) * | 1952-11-21 | 1955-02-25 | Oerlikon Buehrle Ag | Safety devices for projectile initiation rockets |
US2896540A (en) * | 1954-12-06 | 1959-07-28 | Voland Andre | Control device for the percussion pin of a projectile fuse |
US2871788A (en) * | 1955-05-24 | 1959-02-03 | Brevets Aero Mecaniques | Impact fuzes for explosive projectiles including a mechanical self-destruction device |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3249051A (en) * | 1963-11-12 | 1966-05-03 | Junghans Geb Ag | Self-destroying fuze for rotating projectiles |
US3353489A (en) * | 1965-02-26 | 1967-11-21 | Rheinmetall Gmbh | Impact fuze for a spinning projectile |
US3347166A (en) * | 1965-04-02 | 1967-10-17 | Mefina Sa | Fuse for a missile to be fired by a gun with rifled bore |
US4040358A (en) * | 1965-12-14 | 1977-08-09 | Avco Corporation | Hydraulic delayed arming fuze |
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