This disclosure relates generally to ordnance and, more particularly, to ballistic ordnance including ballistic weapons and ammunition.
A ballistic weapon typically fires ballistic ammunition in a straight line subject to ballistic conditions, like gravity and wind. Projectiles of ballistic ammunition are generally spherical or cylindrical and, when fired from a weapon, travel in a generally straight line subject to ballistic conditions. Although such ballistic ordnance is effective for conventional battlefield operations, it is not always well suited for modern urban firefights.
Urban firefights usually involve engaging enemy combatants positioned around corners of buildings, on roofs of buildings, on opposite sides of buildings, and the like. It is difficult to shoot enemy combatants when they are so positioned, and use of airstrikes or use of other ordnance such as grenades are not always suitable alternatives.
One exemplary embodiment of a projectile for a gun includes a boomerang-shaped body having a longitudinal axis, longitudinally opposite end portions, and an external surface having an alignment feature extending parallel to the longitudinal axis between said end portions.
In accordance with another exemplary embodiment, there is provided an ammunition cartridge comprising the projectile recited above.
In accordance with an additional exemplary embodiment, there is provided a weapon barrel through which a boomerang-shaped projectile is fired, said barrel comprising an elongated hollow body having a longitudinal axis, a breech end, and a muzzle end longitudinally opposite said breech end, a bore extending through said body from said breech end to said muzzle end, and an alignment feature in at least a portion of said bore and extending parallel to the longitudinal axis between said ends for orienting said projectile.
Features and advantages of one or more of the disclosed embodiments of this disclosure will be apparent to those of ordinary skill in the art from the following detailed description of exemplary embodiments and the claims, with reference to the accompanying drawings in which:
In general, ballistic ordnance will be described using one or more examples of exemplary embodiments of ballistic projectiles and related weapons that include features to allow projectiles to be fired according to boomerang-like flight paths. The example embodiments will be described with reference to use in firearms. However, it will be appreciated as the description proceeds that the invention is useful in many different applications and may be implemented in many other embodiments. In this regard, and as used herein and in the claims, it will be understood that the term projectile and weapon refers not only to firearm applications, but also to other ordnance applications.
Referring specifically to the drawings,
The cartridge 10 may be of any suitable caliber and any suitable type. Likewise, the propellant 20, primer 22, and wad 24 may be of any suitable type. Although the case 14 may be generally similar to conventional cases at the rearward end 16, the rest of the case 14 may be adapted to the shape of the projectile 12.
Unlike conventional projectiles, which are round or generally cylindrical, the projectile 12 is boomerang-shaped. As used herein, the terminology “boomerang-shaped” includes any shape suitable to cause a projectile to have a flight path that is curved, and to have a rotational axis of constantly changing orientation, for example, according to gyroscopic precession.
The projectile 12 has a longitudinal axis A, longitudinally opposite rearward and forward end portions 26, 28, and an external surface 30 having one or more alignment features 32 extending parallel to the longitudinal axis A between the end portions 26, 28. If a plurality of alignment features 32 are used, they may be spaced apart and parallel to one another. The projectile 12 may extend beyond the forward end 18 of the case 14, or may be generally contained within the case 14 as shown with an open ended aperture in the case 14 corresponding to the alignment feature 32.
In this first embodiment, the projectile 12 is V-shaped with a central portion 34 and two lobes 36, 38 extending therefrom according to the classic and familiar boomerang design. Accordingly, the alignment feature 32 is interrupted by a space between the lobes. The projectile 12 may be weighted asymmetrically about the longitudinal axis A. For example, the projectile 12 may have a greater weight on one side of the longitudinal axis A than on the opposite side of the longitudinal axis. Also, the projectile 12 may be weighted heavier at one longitudinal end than at the other. Furthermore, a mild rifling of a corresponding weapon barrel throughout the length of barrel or only at the muzzle end may be used to initiate rotation of the projectile 12.
In the illustrated embodiment, the rearward end 16 of the case 14 may be round or cylindrical as shown in
Referring to
In the illustrated embodiment, a rearward end 116 of a case 114 may be elliptical as shown in
Referring to
In the illustrated embodiment, a rearward end 216 of a case 214 may be rectangular as shown in
Referring to
In another embodiment, shown in
In general, the components of the disclosed cartridges and weapon barrels may be manufactured and assembled according to techniques known to those skilled in the art, including casting, forging, molding, machining, stamping, and/or the like. Likewise, any suitable materials can be used in making the components, such as metals, composites, polymeric materials, and/or the like.
However, the weapon barrels disclosed herein may be initially produced as generally cylindrical or tubular components and then may be formed into suitable cross-sectional shapes according to the projectiles and/or the cases. For instance, although not shown, a mandrel may be inserted into a cylindrical bore of a barrel and then the barrel may be pressed or otherwise formed to conform the bore to the mandrel into the desired shape that corresponds with the projectile and/or case.
One or more of the features of the exemplary embodiments described above, may provide one or more of the following benefits. Enemy combatants may be shot with a projectile from a weapon even though they are not in a direct line of fire from the weapon, for example, when they are positioned around corners of buildings, on roofs of buildings, on opposite sides of buildings, and the like. Moreover, the presently disclosed ordnance would confuse enemy combatants as to the origin of projectile firing. In other words, the origin of the projectile firing would be effectively disguised.
For example,
In another example,
Finally, the foregoing description is not a definition of the invention, but is a description of one or more examples of exemplary embodiments of the invention. The statements contained in the foregoing description relate to the particular examples and are not to be construed as limitations on the scope of the invention as claimed below or on the definition of terminology used in the claims, except where terminology is expressly defined above. And although the present invention has been disclosed using a limited number of examples, many other examples are possible and it is not intended herein to mention all of the possible manifestations of the invention. In fact, other modifications, variations, forms, ramifications, substitutions, and/or equivalents will become apparent to those skilled in the art in view of the foregoing description. The present invention is intended to embrace such forms, ramifications, modifications, variations, substitutions, and/or equivalents as fall within the spirit and broad scope of the following claims. In other words, the present invention encompasses many substitutions or equivalents of limitations recited in the following claims. For example, the materials, sizes, and shapes, described above could be readily modified or substituted with other similar materials, sizes, shapes, and/or the like. Therefore, the invention is not limited to the particular examples of exemplary embodiments disclosed herein, but instead is defined solely by the claims below.
This application claims the benefit of U.S. Provisional Application No. 61/310,749, filed Mar. 5, 2010. The content of the above application is incorporated herein by reference in its entirety.
Number | Date | Country | |
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61310749 | Mar 2010 | US |