Gyrostabilized projectile

Abstract

A projectile includes a hollow body carrying a payload formed of inert sub-projectiles that can be dispersed on trajectory contained in a cup including a piston closing one of its ends, the body at its rear part with a base housing a pyrotechnic charge separated from the sub-projectiles by the piston, which can translate with respect to the body of the projectile to push the cup and the sub-projectiles axially out of the body. The cup is formed of independent sectors. The piston is secured to the sectors when contained in the body and the cup is secured to the body by a connecting apparatus weakened to break under the force of the piston pushed by the gases generated by the pyrotechnic charge. An ogive is secured to the cup by a securing apparatus that is coaxial with the longitudinal axis of the projectile and locked by the sectors.

Claims

1. A gyrostabilized projectile including a hollow body carrying a payload formed of a set of sub-projectiles, wherein the sub-projectiles are inert and configured to be dispersed on a trajectory, the projectile including a single cup that contains the sub-projectiles and includes a piston closing one of the ends of the cup, a rear part of the body being provided with a base housing a pyrotechnic charge separated from the sub-projectiles by the piston, wherein the piston configured to translate with respect to the body so as to push the cup and the sub-projectiles axially out of the body, the cup being substantially cylindrical and of a diameter corresponding to that of a cylindrical bore inside the body, the cup being formed by assembly of at least two sectors, independent of each other and joined along edges thereof that are parallel to a longitudinal axis of the projectile, wherein the piston is secured to the sectors when the piston and the sectors are contained in the body and the cup is secured to the body by a weakened connecting means configured to break under a force applied by the piston when the piston is pushed by gases generated by the pyrotechnic charge, an ogive being secured to the cup with a securing means that is coaxial with the longitudinal axis of the projectile and locked by the sectors of the cup.

2. The projectile according to claim 1, wherein the weakened connecting means includes screws connecting the body and the piston, said screws having a section calibrated to break.

3. The projectile according to claim 2, wherein the screws are oriented radially to the longitudinal axis of the projectile.

4. The projectile according to claim 3, wherein each screw also passes through a sector to connect said sector to the piston.

5. The projectile according to claim 2, wherein the screws are oriented parallel to the longitudinal axis of the projectile.

6. The projectile according to claim 1, wherein the weakened connecting means includes a socket screwed into a bore in a rear face of the piston, the socket including a shoulder arranged so that a part of the body is clamped between the shoulder and the rear face of the piston, thereby securing the cup to the body, the socket including a weakened zone calibrated for tensile failure.

7. The projectile according to claim 1, wherein the securing means includes a screw with a polygonal head, front ends of the sectors of the cup being joined together around the polygonal head so as to form an embedded connection with the polygonal head when the cup is in the body, separation of the sectors releasing the head.

8. The projectile according to claim 7, wherein the ogive has a rim and is screwed onto the screw so as to have the rim bearing on the body.

9. The projectile according to claim 1, wherein the projectile includes at least one key engaged in a correspondingly shaped housing located between each sector of the cup and the body, so as to connect said sector of the cup and the body for rotation about the longitudinal axis of the projectile without hindering ejection of the cup from the body.

Description

(1) The invention will be better understood from the following description, which is made in the light of the annexed drawings in which:

(2) FIG. 1 shows a cross-sectional view of a projectile according to a first embodiment of the invention.

(3) FIG. 2 shows a detailed cross-sectional view of a projectile according to the first embodiment of the invention.

(4) FIG. 3 shows a cross-sectional view of a projectile according to a second embodiment of the invention.

(5) FIG. 4 shows a cross-sectional view of a projectile according to a third embodiment of the invention.

(6) FIG. 5 shows a three-quarter view of a projectile according to the invention, during operation on trajectory.

(7) According to FIG. 1, a medium-caliber projectile 1 (caliber between 20 mm and 70 mm) includes a hollow body 2 provided with a base 3 at its rear part. The front part of the body 2 is closed by a ballistic ogive 4. The hollow body 2 includes a substantially cylindrical cavity 2a opening out at the front of the body 2 and said cavity contains a correspondingly shaped cup 5.

(8) The cup 5 is filled with inert sub-projectiles 11 forming a payload that can be dispersed on trajectory as will be discussed below.

(9) The cup 5 includes sectors 5a that are independent of each other and joined along their edges parallel to the longitudinal axis X of the projectile 1. There are three sectors here.

(10) The rear end of the cup 5 carries a piston 5b that closes its rear part. On the front part of the cup 5, the sectors 5a are joined together around a polygonal head 6a of a screw 6, coaxial with the projectile 1, so as to form an embedded connection of the screw 6 relative to the cup 5.

(11) The screw 6 forms a means 6 for securing the cup 5 to the ogive 4. The threaded part of the screw 6 makes it possible to screw the ogive 4 until its rim 4a comes bearing against the front edge of the body 2.

(12) Between each sector 5a of the cup 5 and the body 2 of the projectile 1, at least one key 7 is engaged in a correspondingly shaped housing 14 (the body 2 and the sector 5a in question sharing the housing). The keys 7 make it possible to connect the cup 5 and the body 2 for rotation about the longitudinal axis X of the projectile 1. There are two keys 7 per sector 5a here.

(13) As can be seen in FIG. 5, the housing 14 for each key 7 is oriented parallel to the longitudinal axis X of the projectile 1 so as not to hinder the sliding ejection of the cup 5 out of the body 2.

(14) In the embodiment shown in FIG. 1, the cup 5 is secured to the body 2 by means of screws 8 arranged radially to the longitudinal axis X of the projectile. The screws 8 form a securing means and penetrate the body 2 and the piston 5b while passing through the sectors 5a, thus connecting each sector 5a to the piston 5b.

(15) In this way, the ogive 4 is strongly attached to the body 2 by means of the cup 5, which transfers any impact stresses experienced by the ogive 4 towards the interior of the projectile, to areas where the connection with the body is less weak.

(16) As detailed in FIG. 2, the screws 8 are weakened connecting means as they have a shear weakening zone 8a located at the junction between the cup 5 and the body 2, providing to the connecting means 8 a shearable nature that is not disrupted by radial impacts on the ogive 4 for example.

(17) The weakening zone includes, for example, a section 8a calibrated so as to break following the reaching of a stress threshold, which is obtained by the thrust of the piston 5b to which the pressure of the gases generated by the initiation of a pyrotechnic charge 10 is applied, the charge being located behind the piston 5b, in a chamber 3a at the base 3 of the projectile 1.

(18) It is to be noted that the piston 5b includes a shoulder 5c on which the rear ends of the sectors 5a bear, which enables it, once the screws 8 have been broken, to push the sectors 5a, the sub-projectiles 11 and the ogive 4 in front of the body 2 in the direction of the trajectory of the projectile 1, as shown in FIG. 5.

(19) As soon as the sectors 5a are ejected from the body 2, since the projectile 1 is gyrostabilized, the sectors 5a undergo centrifugal forces tending to spread them radially, thereby releasing the screw head 6 and thus the ogive 4.

(20) The sub-projectiles 11 are also released and spread out into the surrounding space by centrifugal forces in order to bring their kinetic effects to bear on a target not shown, said kinetic effects being due to the velocity of the projectile 1 plus the velocity of projection provided by the thrust of the piston 5b. For the sake of readability of FIG. 5, the sub-projectiles 11 are shown before they are dispersed.

(21) According to a second embodiment shown in FIG. 3, the weakened connecting means 8 are still screws 8 but they are oriented parallel to the longitudinal axis X of the projectile 1 and connect a rear part of the body 2 to a rear face of the piston 5b.

(22) The weakened connecting means will therefore be dimensioned to break as a result of a tensile stress produced by the pressure of the gases generated by the charge 10. The sectors 5a of cup 5 are secured to the piston by pins 12. The pins 12 are cylindrical and have no protuberance at their end, which allows the easy separation of the sectors 5a from the piston 5 once the cup 5 has been ejected from the body 2, as shown in FIG. 5. On the other hand, when the cup 5 is in the body 2, the sliding fit of the cup 5 relative to the body 2 prevents any separation of the sectors from the piston 5b. The result is thus a monolithic assembly which strongly connects the ogive 4 to the projectile body.

(23) According to FIG. 4, the weakened connecting means 8 includes a socket 8 that is screwed into a bore in the rear face of the piston 5b and that has a shoulder arranged so that a part of the body 2 is clamped between the shoulder 8b and the rear face of the piston 5b, thereby securing the cup 5 to the body 2.

(24) The socket 8 has a weakened area calibrated for tensile failure so that the cup 5 can be ejected once the threshold pressure in chamber 3a is reached.