PENETRATING AND EXPLOSIVE PROJECTILE WITH STABILIZING FIN ASSEMBLY
20220214149 ยท 2022-07-07
Assignee
Inventors
Cpc classification
F42B10/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42C1/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The invention relates to a penetrating and explosive projectile (1) provided with a trajectory-stabilizing fin assembly (8) which is secured to a body of the projectile by a mechanical connection. The fin assembly (8) includes a tapped tube (14) which engages on a threaded rear cylindrical shank (10) of a tail (9) connected to the projectile body (2), thereby forming a threaded mechanical connection (13) between the tail unit (8) and the body (2). This projectile (1) is characterized in that it includes means ensuring the fragilization of the threaded connection (13) on impact on a target, the fin assembly then separating from the projectile body.
Claims
1- A penetrating and explosive projectile provided with a trajectory-stabilizing fin assembly which is secured to a body of the projectile by a mechanical connection, the fin assembly including a tapped tube which engages on a threaded rear cylindrical shank of a tail connected to the projectile body, thereby said mechanical connection is a threaded mechanical connection between the fin assembly and the body, wherein the projectile includes means ensuring fragilization of the threaded mechanical connection on impact on a target, so that the fin assembly then separates from the projectile body.
2- The penetrating and explosive projectile according to claim 1, wherein the projectile includes a fuze arranged at a rear part of the projectile, and the tail carrying the fin assembly includes a conical portion which connects to the body of the projectile.
3- The penetrating and explosive projectile according to claim 2, wherein the fin assembly also includes fragilization means consisting of breakage initiators arranged on the tapped tube of the tail, between fins of the fin assembly, wherein said breakage initiators are made as longitudinal grooves that ensure a thinning of the thickness of the tapped tube, an inertial advance motion of the fin assembly on the conical portion, upon impact of the projectile on the target, causing the grooves to break.
4- The penetrating and explosive projectile according to claim 3, wherein each fin includes a conical front part cooperating with the conical portion of the tail.
5- The penetrating and explosive projectile according to claim 3, wherein the front part of the tapped tube also includes a conical part in continuation of conical front parts of the fins.
Description
[0011] The invention will be better understood upon reading the following description of various embodiments, description made with reference to the annexed drawings in which:
[0012] [
[0013] [
[0014] [
[0015] Referring to
[0016] The explosive charge 3 is intended to be initiated by a detonation relay 5 which is itself initiated by a fuze 6 which is arranged in a base 7 secured to the rear part of the body 2, for example by a thread.
[0017] The projectile 1 also includes a stabilizing fin assembly 8 which is secured to the body 2 of the projectile by means of a threaded mechanical connection that includes a tail 9. This tail 9 includes a rear cylindrical shank 10, extended at the front by a conical portion 11 which connects to the body 2 of the projectile at a threaded bearing surface 12 of the base 7.
[0018] The cylindrical shank 10 includes a thread on which is screwed a tapped tube 14 that carries the fins 15 of the fin assembly 8. The thread of the shank 10 and the tapped hole of the tube 14 form the threaded connection 13.
[0019] As can be seen in
[0020] According to the invention, the projectile 1 includes means ensuring the fragilization of the threaded connection 13 between the thread of the shank 10 and the tapped hole of the tube 14 upon impact of the projectile on a target.
[0021] Thus, the inertial forces exerted on the fin assembly 8 at the impact will cause the fragilization means to break, thus ensuring the separation of the fin assembly 8 and the body 2 of the projectile 1.
[0022] For example, a simple transverse groove on the shank 10, between the threaded part and the conical portion 11, could be defined as fragilization means.
[0023] This groove will weaken the shank 10 which will break upon impact on a target.
[0024] The fin assembly 8 will then detach from the projectile 1 and will not interfere with the operation of the fuze.
[0025] It should be noted that the external profile of the conical portion 11 also ensures a deflection of the fin assembly 8, thus protecting the fuze 6 against the impacts caused by the latter.
[0026] It can be seen in
[0027] Therefore, if the fins 15 or the fin assembly 8 hit the projectile body 2, the impact will occur at a distance from the fuze 6 and will not disrupt the operation of the fuze.
[0028] In a particular embodiment of the invention, it is noted in
[0029] These grooves 19 ensure a thinning of the thickness of the tube 14 and constitute breakage initiators for the wall of the tube 14. It is also noted that each fin 15 includes a front part with conical profile 20 which is intended to cooperate with the conical portion 11 of the tail 9. This front part with conical profile 20 also extends at the front part of the tube 14 which is also conical.
[0030] As can be seen in
[0031] This advance motion of the fin assembly 8 leads to a sliding of the conical part 20 of each fin 15 (and of the tube 14) on the profile of the conical portion 11 of the tail 9. This results in a radial stress leading to an enlargement of the internal diameter of the tube 14. This stress causes the grooves 19 to break and the fins 15 to move away from each other (arrows A1 and A2).
[0032] Each fin 15 thus follows a trajectory that moves it away from the fuze 6.
[0033] Such an arrangement makes the breakage of the threaded connection 13 more reliable and ensures that the impacts that the fin assembly 8 could cause on the fuze 6 are reduced to a minimum.