Spin-stabilized artillery projectile having gas pressure...

Ammunition and explosives – Projectiles – Composite

Reexamination Certificate

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Details

C102S524000, C102S517000, C102S516000, C102S514000

Reexamination Certificate

active

06237497

ABSTRACT:

CROSS REFERENCE TO RELATED APPLICATION
This application claims the priority of German Application No. 198 15 295.7 filed Apr. 6, 1998, which is incorporated herein by reference.
BACKGROUND OF THE INVENTION
This invention relates to a spin-stabilized artillery projectile of the type fired from a weapon barrel and having a projectile body which is ogive-shaped in its frontal region.
Projectiles of the above-outlined type are known, for example, from German Gebrauchsmuster (utility model) G 84 33 256.5. The projectile body of these types of artillery projectiles conventionally carries a circumferential guide band at a rearward part of the projectile body. The guide band is of metal, for example, soft iron or copper or may consist of a plastic material. The outer diameter of the guide band is greater than the caliber diameter of the barrel so that upon firing of the projectile, the guide band is pressed into the barrel rifling and prevents combustion gases from flowing past the projectile. As the projectile moves forward in the barrel, the rifling imparts a stabilizing rotation on the projectile via the guide band.
It is further known from the above-identified German utility model to provide an additional polymer obturator ring adjacent the guide band and facing the rear terminus of the projectile.
Guide bands of artillery projectiles which, for reaching a high muzzle velocity, are fired from long (for example, 52 caliber) barrels, are exposed to substantial wear. As a result, the spin transmission and sealing functions of the guide bands are frequently not performed reliably and, particularly in projectiles having a conventional obturator and a copper guide band, after firing, partially deep engravings on the projectile body may appear. Such a “body-engraving” leads to an increased wear of the weapon barrel and negatively affects the trajectory of the projectile. Also, risks are considerable that explosive projectile payload detonates prematurely within the weapon barrel.
SUMMARY OF THE INVENTION
It is an object of the invention to provide an improved spin-stabilized artillery projectile which, upon firing from the weapon barrel, has a reduced guide band wear as compared to known projectiles and in which, in particular, a body-engraving is significantly diminished. This object and others to become apparent as the specification progresses, are accomplished by the invention, according to which, briefly stated, the spin-stabilized projectile adapted to be fired from a weapon barrel includes a projectile body having a length dimension, a rear length portion, an ogive-shaped front length portion and an intermediate cylindrical length portion situated between the rear and front length portions; a metal guide band circumferentially mounted on the projectile body; and an undercut provided circumferentially in the intermediate length portion to define an annular chamber with an inner surface of the weapon barrel during travel of the projectile in the weapon barrel upon firing for effecting a pressure equalization of propellant gases flowing past the metal guide band to center the projectile within the weapon barrel.
The invention is based on the principle to provide, between the guide band and the ogive-shaped frontal region of the projectile body, at least in one partial zone thereof, an undercut which extends annularly about the projectile and which is so configured that in the annular chamber formed between the outer surface of the projectile body and the inner wall of the weapon barrel, a pressure equalization of the combustion gases flowing past the projectile is effected. In this manner, a centering of the projectile in the weapon barrel occurs, as a result of which the projectile, after leaving the weapon barrel, follows its predetermined flight path. Further, the unilateral stresses imparted to the weapon barrel by the conventional projectiles are significantly reduced. Tests have shown that for achieving a sufficient projectile stabilization, the length L1 of the undercut should be between 70% and 80%, preferably approximately 75%, of the total length L0 of the cylindrical projectile part which extends between the guide band and the ogive-shaped frontal region of the projectile. The depth of the undercut should be approximately between 0.3% and 0.6% of one half of the maximum projectile diameter.
It has been found to be advantageous to provide that the undercut does not adjoin immediately the guide band but is separated therefrom by approximately 30-35% of the remaining length &dgr;L=L0−L1.
A further significant reduction of the guide band wear is obtained by providing that the guide band is of soft iron instead of copper and that the projectile, in addition to the guide band, has an obturator made of a heat-resistant elastomer. Particularly nylon has been found to be a satisfactory material for the obturator.


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