Ring airfoil glider expendable cartridge and glider launching method
First Claim
1. A munition for launching in a barrel of a breech loading gun, comprising:
- a circular base supported within the breech, said base including a vent for directing compressed gas toward a sabot;
a generally cylindrical rod extending toward a muzzle of the barrel from the center of said base;
a ring airfoil projectile adapted and configured to be launched from within the barrel;
a sabot having a central passage that accepts therein said rod, the central passage and said rod being in sliding contact, said sabot having two opposite surfaces with one surface facing said base and being in fluid communication with the vent and the opposing surface being adapted and configured to push said projectile;
wherein compressed gas flowing through the vent acts on the one surface of said sabot to push said projectile through the barrel;
said projectile separates from the sabot prior to reaching the muzzle of the barrel.
1 Assignment
0 Petitions
Accused Products
Abstract
My Ring Airfoil Glider Expendable Cartridge and Glider Launching Method is form launching a reduced caliber ring airfoil glider from a conventional grenade launcher barrel with preferred application for less lethal use. A caseless ammunition base contains a primer communicating with a propellant in a rupture disk sealed chamber with a vent used to create, seal and channel propelling gas into a space behind a sabot mounted on a central guide on the base, whereupon releasing the gas, the sabot aligns, seals, pushes and rotates the glider in passage down the barrel, to a point of maximum velocity, whereon, the propelling gas is vented ahead of the glider by the central passage in the sabot as it leaves the guide, whereupon, the bore decelerates the sabot by friction freeing the glider to fly down the bore centered by a turbulent boundary layer of air until it exits the muzzle.
164 Citations
18 Claims
-
1. A munition for launching in a barrel of a breech loading gun, comprising:
-
a circular base supported within the breech, said base including a vent for directing compressed gas toward a sabot; a generally cylindrical rod extending toward a muzzle of the barrel from the center of said base; a ring airfoil projectile adapted and configured to be launched from within the barrel; a sabot having a central passage that accepts therein said rod, the central passage and said rod being in sliding contact, said sabot having two opposite surfaces with one surface facing said base and being in fluid communication with the vent and the opposing surface being adapted and configured to push said projectile; wherein compressed gas flowing through the vent acts on the one surface of said sabot to push said projectile through the barrel; said projectile separates from the sabot prior to reaching the muzzle of the barrel. - View Dependent Claims (2, 3, 4, 5, 6, 7)
-
-
8. A munition for launching in a barrel of a breech loading gun, comprising:
-
a circular base supported within the breech; a rod protruding from the center of said base and extending toward a muzzle of the barrel, said rod having a rifled outer surface; a ring airfoil projectile adapted and configured to be launched from within the barrel, said projectile having a maximum outer diameter that is smaller than the inner diameter of the barrel; a sabot having a central passage that accepts therein said rod, said sabot being guided by the rifling of said rod, said sabot being adapted and configured to push said projectile; and a source of compressed gas; wherein compressed gas provides a pressure force to push said sabot along said rod, the rifling of said rod interacting with the central passage to spin said sabot, said sabot spinning said projectile and pushing said projectile through the barrel, said sabot and said projectile separating from each other within the barrel. - View Dependent Claims (9, 10, 11, 12, 13, 14, 15)
-
-
16. A reduced lethality munition for launching in a barrel of a breech loading gun, comprising:
-
a circular base supported within the breech, said base having a periphery in contact with the barrel; a generally cylindrical rod extending toward the muzzle of the barrel from the center of said base; a ring airfoil projectile adapted and configured to be launched from within the barrel, said projectile having a maximum outer diameter that is smaller than the inner diameter of the barrel, the maximum diameter being more than about 35 millimeters and less than about 40 millimeters, the projectile having a weight that is less than about fifteen grams; a sabot having a central passage that is in sliding contact with said rod, said sabot being adapted and configured to push said projectile; and a source of compressed gas; wherein the compressed gas provides a pressure force to push said sabot along said rod such that said projectile exits the muzzle with a velocity of more than about ninety meters per second; wherein said projectile separates from said sabot prior to reaching the muzzle end of the barrel. - View Dependent Claims (17, 18)
-
Specification