[0001] The invention is referring to a self disarming fuze that can be used in grenades
of artillery cargo munition, as well as in rotating mortars, bombs, and rockets.
[0002] The fuzes in use today, in cargo munitions, do not solve the significant problem
of not exploded granades in the battlefield, or in the training field.
[0003] The unexploded grenades are dangerous for the troops that will go through the bombarded
areas, as well as for the field cleaning personel.
[0004] The armies that are currently using cargo munitions, demand the use of a fuze, for
the grenades, that will be self-destructive in the case that they will not operate,
for any reason, after the impact on the target.
[0005] The only way of self distruction, that has been devised up to now is pyrotechnical.
This solution is not acceptable by the users, because, besides the high cost, in a
case that the self destruction mechanism will not operate, even to a low percentage,
it will render the grenades more hazardous than the ones that are using common fuzes.
[0006] The described fuze, that constitutes the opject of the invention is self disarming,
in the occasion that it will not operate after the impact on the target, making the
grenade entirely harmless.
[0007] For the rare occasion that the fuze will not operate explosively and it will not
self disarm after the impact of the grenade on the target, the fuze is again harmless
for the troops that will go through the field and accidentally step on a grenade.
[0008] In figure 1, an overall picture of the fuze is given, with the slider (2) of the
detonator (7), in a safe position that is achieved by the pressure of the spring (6).
[0009] In this case, the detonator (7) and the striker (3), are off line. In addition the
slider (2) cannot move in the armed position, because the end of the striker (3) is
inside an opening of the slider (2),and retained in this position by the safety (5).
The entire system of the slider (2) and the striker (3) and the safety (5), is inside
the shell (1) and enclosed with the metal plate (11). In figure 2 (side section) the
fuze is shown in the armed position. By the rotation of the fuze, the safety (5) of
figure 1 is separated and the striker (3) has been retracted from the slider (2) because
of the expansion of the spring (4) of figures 1 and 2. The slider (2), because of
the centrifugal force, has moved in a way that the detonator (7) is on line with the
striker (3) making the spring (6) be compressed.
[0010] The exact position of the slider (2), is determined by the end stopper (2a), that
is freely sliding in an opposite groove (12) of the shell (1).
[0011] The upright position of the grenade during the fall is assured by the ribbon (13),
that is firmly attached on the top of the fuze with the metal straps (9) and (14).
The metal straps (9a) and (9b), in the ribbon ends, during the rotation maintain the
ribbon in an almost horizontal position, simulating in this maner the helicopter blades.
The metal straps (9a) and (9b) can be omitted if the ribbon, when rotating, has enough
weight to maintain its horizontal position during the rotation of the grenade.
[0012] In figure 3 (side view) is shown the fuze when the grenade is hitting the target.
The striker (3), because of the inertia, has struck the detonator (7), causing its
explosion. In figure (4) the slider (2) is shown in top and side view. In location
(1) the detonator (7) of figures 1,2,3 is placed. In location (3) the end of the striker
(3) figures 1,2,3 is inserted when the fuze is in safe position.
[0013] The groove (4) is making the movement of the slider (2) easier during the arming
procedure. The movable cylinder or sphere (6), is located in groove (5).
[0014] The reason for the cylinder of sphere (6) is to maintain the slider (2) in armed
position when the spin of the fuze is reduced or stopped.
[0015] In figure 5 (down view of the shell (1) of figures 1,2, and 3) are shown:
[0016] -The groove (12) in which the stopper (2a) of figures 1,2 and 3 can slide freely.
[0017] -The two holes (16) and (16a), are used to mount the fuze on the grenade.
[0018] -The cylindrical cavity (10) inside which the striker (3) can move in figures 1,2,
and 3.
[0019] -The opening (15) that is used for partial entry of the cylinder (6) of figure 4
when due to the centrifugal force, the slider (2) of the detonator of figure 4 has
stopped in the armed position.
[0020] The section of the cylinder (6) in figure 4 that has moved in to groove (15) restricts
the movement of the slider to the safe position, despite the pressure of the spring
(16) in figures 1,2, and 3.
[0021] If during the impact, and for any reason, the detonator (7) of figures 1,2,3 will
not explode, then, because of the shock, the small cylinder (6) of figure 4, is retract
toward the groove (5) of figure 4 and the slider (2) with the pressure of the spring
(6) of figures 1,2 and 3 returns to the safe position as in figure 1.
[0022] In figurs 6,7 and 8, are shown the above mentioned metal plates (14) (9) and (11)
of figures 1 and 2.
[0023] In figure 9,is shown the fuze as it will be assembled and ready for shipping. The
safety pin (17), is holding the ribbon (13) tight in place and also helps the loading
of the shell with grenades in a special order.
1. The self disarming fuze for cargo munition grenades which consists of the following.
a. The cell (1), figure 1.
b. The slider, figure 4.
c. The striker (3), figure 1.
d. The safely pin (5), figure 1.
e. The spring (4), of the striker (3) figure 1.
f. The spring (6), of the slider (2) figure 1.
g. The ribbon (13), figure 2.
h. The metalsheet (9), in figure 2, which holds the ribbon.
i. The metal sheets (9a) and (9b), figure 2.
j. The cylinder or small sphere (6), figure 4.
k. The metal sheet (14), figure 6.
1. The metal sheet (11), figure 8.
2.The self disarming fuze for cargo munition grenades, as in claim 1, is distinguished
from the ribbon (13), figure 2 which is securely attached on the top of the fuze,
and rotates with the grenade, assuring this way the vertical fall of the granade
to the ground or to the target.
3.The self disarming fuze for cargo munition grenades, as in claim 1, is distinguished
from the striker (3) in figure 1, which is independent from the ribbon and is retracted
from the detonator (7), figure 2 with the help of the spring (4) figure 2, after its
impact to the detonator (7), figure 2.
4.The self disarming fuze for cargo munition grenades as in claim 1, which is distringuished
from the fact that the slider (2) of the detomator (7), figure 2, (the details can
be seen in figure 4 ) , moves to the armed position because of the centrifugal force,
overcoming the spring (6) force, figures 1,2, and 3.
5.The shelf disarming fuze for cargo munition grenades as in clain 1, which is distinguished
by the fact that the cylinder or sphere system (6) of figure 4 that enters the groove
(15), figure 5, because of the centrifugal force and holds the slider (2), as in figure
2, in the armed position, even ifthe spin is reduced or stopped during the free fall
of the grenade.
6.The shelf disarming fuze for cargo munition grenades as in claim 1, which is distinguished
by fact that the safety (5), figure 1, is holding the slider (2), figure 1, in a
non armed position, until the expulsion of the grenades from the shell.
7.The self disarming fuze for cargo munition grenades as in claim 1, which is distinguished
by the fact that the shell (1), figure 1, has certain grooves, that the slider (2),
the striker (3), and the safeties operate properly. Top view of the shell can be
seen in figure 5.
8.The self disarming fuze for cargo munition granades as in claim 1, which is distinguished
by the fact that the metal sheets (14) and (11) of figures 6, and 8 respectively,
are holding the fuze as an assembly, and also increasing the strength and endurance
of the fuze in the extremely high accelerations of 15.000 Gs that are exerted on the projectile during the firing of the cannon.