This invention relates to ammunition, specifically ammunition used in small arms having armor piercing capabilities.
Prior art armor piercing projectiles have been developed for use on a variety of weapons specifically by the military in a number of user specific requirements. Such military projectiles use a depleted uranium core due to its dense properties. Examples of projectile ammunition can also be seen in U.S. Pat. Nos. 5,009,166, 6,105,506, 7,520,224, and U.S. Pat. 8,161,886.
In U.S. Pat. 5,009,166 is directed to a low cost penetrator projectile having a hard metal core with a hollow conical shape formed from low carbon steel in a series of progressive dies to achieve a Rockwell hardness of C50 and C55.
U.S. Pat. No. 6,105,506 claims a bullet body and an nonrotable sabot slug for shotguns with a jacketed bullet with a forward end hollow point and a metal sabot that comes in contact with the rifling in the gun barrel.
U.S. Pat. No. 7,520,224 discloses an advanced armor piercing projectile having a precision machine outer and inner component. The inner component is of a higher density than the outer and higher than that of armor plate such as tungsten.
U.S. Pat. No. 8,161,886 is directed to a short magnum shot shell cartridge and firing assembly wherein a sabot retaining shot shell cartridge chamber has a sub-caliber projectile.
An armor piercing projectile cartridge having a composite penetration core of hardened steel within a steel jacket formed socket. A stabilization sabot of synthetic resin material with elastic base insert surrounds the jacketed composite projectile defining a twelve-gauge armor piercing projectile within a cartridge hull having a propellant and primer.
Referring now to
A composite projectile assembly 10 of the invention is capable of penetrating AR500 grade designated armor plate AP graphically illustrated for reference purposes in broken lines in
The bi-metal projectile 16 has a monolithic cylindrical body member 20 with a conical engagement end portion 20A and oppositely disposed base end surface 20B. The projectile 16 is formed of hardened steel which in this example 4142 steel hardened C58/62 and is illustrated as a twelve-gauge shell dimension.
The projectile 16 conical engagement end portion 20A is of a length L1 greater than that of its overall length indicated at L2 in
It will be evident that dimensional variances are not limited to the preferred embodiment designation, but can vary depending on application user venue.
A steel projectile jacket 21 encases the cylindrical portion of the overall body member 20 forming a projectile receiving pocket 22 therein having a uniform continuous upstanding integrated sidewall 23 and a base 24 of increased dimensional thickness in comparison thereto.
The sidewall 23 has a free annular upper edge 25 tapered to be aerodynamically compliant with the conical end portion 20A of the projectile 16, when assembled. The composite assembly bi-metal projectile 16 and jacket 21 is in turn fitted within the stabilization sabot 26 made from plastic, in this example, defining a shroud thereabout. The sabot 26 has an annular sidewall 26A with multiple spaced cuts C thereabout, an offset annular base 26B of increased dimension mass. The sabot 26 will thus support and stabilize the composite bi-metal projectile 16 during its initial flight and then separate and split open as seen in
Referring back now to
The contoured cartridge wad 19, as best seen in
The armor piercing projectile cartridge 10 will therefore provide for optimum ballistic performance co-efficiency of the composite bi-metal projectile 16 for maximum piercing impact with the targeted armor plate AP, as described.
It will thus be seen that a new and novel composite armor piercing cartridge 10 of the invention has been illustrated and described and it will be apparent to those skilled in the art that various changes and modifications may be made thereto without departing from the spirit of the invention. Therefore, I claim: