US2012152145A1PendingUtilityA1
Projectile for use with a rifled barrel
Est. expiryNov 2, 2030(~4.3 yrs left)· nominal 20-yr term from priority
Inventors:Todd Kuchman
F42B 12/66F41H 13/0006F42B 10/26
37
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Claims
Abstract
A multi-component projectile is disclosed. The multi-component projectile is designed for use with a rifled barrel and is configured to, upon exiting the rifled barrel, utilize the spinning forces imparted on the projectile while in the barrel to expand until the multi-component projectile achieves a predetermined pattern that is larger than an area of the barrel from which the projectile was fired. Methods of manufacturing the multi-component projectile are also disclosed.
Claims
exact text as granted — not AI-modified1 . A multi-projectile assembly, comprising:
at least a first projectile portion; at least a second projectile portion; and a multi-staged radial braking and tether restraint system that interconnects the at least a first and second projectile portions such that spin-generated forces imparted on the assembly cause the at least a first and second projectile portions to radially expand away from their original center of rotation up to a finite expansion limit defined by the multi-staged radial braking and tether restraint system.
2 . The multi-projectile assembly of claim 1 , wherein the at least a first and second projectile portions are arranged in a circular array and wherein the at least a first and second projectile portions are symmetrical such that they interconnect with one another primarily along their major axis and also along a second axis other than their major axis.
3 . The multi-projectile assembly of claim 2 , wherein the at least a first and second projectile portions are arranged in the circular array such that a left interfacing surface of the at least a first projectile portion interlocks primarily along its major axis and also along the second axis other than its major axis with a right interfacing surfacing of the at least a second projectile portion which is adjacent to the at least a first projectile portion.
4 . The multi-projectile assembly of claim 1 , wherein the at least a first and second projectile portions interconnect with one another such that a cavity is formed between the at least a first and second projectile portions, the cavity being configured to house the multi-staged radial braking and tether restraint system, and wherein the at least a first and second projectile portions further interconnect with one another in such a way that the at least a first and second projectile portions are configured to exit a barrel of a gun simultaneously.
5 . The multi-projectile assembly of claim 1 , wherein the at least a first and second projectile portions expand away from their original center of rotation substantially within a single plane of expansion and wherein a trajectory of the multi-projectile assembly is substantially orthogonal to the plane of expansion.
6 . The multi-projectile assembly of claim 1 , wherein the at least a first and second projectile portions benefit from gyroscopic stabilization as they expand from their original center of rotation.
7 . The multi-projectile assembly of claim 1 , further comprising at least a third projectile portion, wherein the multi-staged radial braking and tether restraint system interconnects the at least a first, second, and third projectile portions.
8 . The multi-projectile assembly of claim 7 , further comprising no more than five projectile portions, wherein the multi-staged radial braking and restraint system interconnects the projectile portions of the multi-projectile assembly.
9 . The multi-projectile assembly of claim 1 , wherein the at least a first and second projectile portions each comprise an anchor point where the multi-staged radial braking and tether restraint system applies forces to the projectile portion and wherein the anchor point is offset from a center of mass of the projectile portion thereby allowing each projectile portion to independently rotate and achieve an independent optimal aerodynamic position upon reaching the expansion limit.
10 . A cartridge including the multi-projectile assembly of claim 1 .
11 . A multi-staged radial braking and tether restraint system, comprising:
at least a first stage adapted to apply at least a first braking force to a plurality of projectile portions when the plurality of projectile portions expand away from their original center of rotation; and at least a second stage adapted to apply at least a second braking force to the plurality of projectile portions when the plurality of projectile portions expand away from their center of rotation.
12 . The multi-staged radial braking and tether restraint system of claim 11 , wherein the at least a first stage comprises a tether which applies the first braking force when the tether is under tension.
13 . The multi-staged radial braking and tether restraint system of claim 12 , wherein the at least a second stage comprises a plurality of braking applicators established on the tether.
14 . The multi-staged radial braking and tether restraint system of claim 13 , wherein the at least a second stage further comprises a deformation brake.
15 . The multi-staged radial braking and restraint system of claim 14 , wherein the deformation brake comprises at least one of an adhesive and a sleeve.
16 . The multi-staged radial braking and tether restraint system of claim 13 , wherein the tether is looped and laid back onto itself and the braking applicators comprise a breakable bond created at points of contact where the tether touches itself.
17 . The multi-staged radial braking and tether restraint system of claim 13 , wherein the tether is configured in such a way that consecutive loops are pulled through one after another and the braking applicators comprise a breakable bond created along points of contact where the tether touches itself.
18 . The multi-staged radial braking and tether restraint system of claim 13 , wherein the tether is spooled and wherein the braking applicators comprise a continuous or semi-continuous breakable bond created along points of contact where the tether touches itself.
19 . A projectile portion for use with an interlocking multi-projectile assembly that expands when spin-generated forces are imparted on the assembly, the projectile portion comprising:
an outer surface; a first mating surface a second mating surface, both of the mating surfaces being configured to interface with a corresponding mating surface of at least one other projectile portion in the multi-projectile assembly such that when the multi-projectile assembly is fired from a barrel of a rifle, the projectile portions of the multi-projectile assembly exit the barrel substantially simultaneously and wherein the first and second mating surfaces are symmetrically positioned about a major axis of the projectile portion so as to facilitate a circular array configuration of the multi-projectile assembly.
20 . The projectile portion of claim 19 , wherein the first and second mating surfaces comprise one or more features which facilitate a mono-directional expansion of the multi-projectile assembly, wherein the direction of mono-directional expansion is substantially orthogonal to a trajectory of the multi-projectile assembly and wherein spin-generated forces which cause the mono-directional expansion of the assembly also cause the assembly to be gyroscopically stabilized.Join the waitlist — get patent alerts
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