1. Field of the Invention
The present invention relates generally to projectiles used primarily for low lethality antipersonnel end use, as for example for crowd control by a municipality police force, and more particularly relates to improvements for assuring that a projectile in use will have the requisite low lethality consequence upon impact, and thus avoiding unintentional severe injury to any individual.
2. Discussion of the Related Art
The need for low lethality projectiles is well known in the art, and additionally can be inferred from the promulgation by the National Institute of Justice of low lethality-qualifying standards exemplified by its standard 0101.03 tests. A known projectile which currently is a low lethality munition of choice consists of a flat bag which is folded in half to fit within a 12 gauge shotgun shell, and after exiting from the muzzle is supposed to unfold into a flat bag shape and impact in this flat bag shape upon a target. As such the kinetic energy is distributed over the area of the bag instead of at a point as in regular ammunition. As a consequence there is less of a possibility of an undesirable penetration while permitting the delivery of a desirable incapacitating impact.
The shape of the above described projectile at impact is not always predictable based solely on its construction as a bag, because the bag can be flat at impact only if it unfolds after exiting from the muzzle. However, on numerous occasions in practice it does not unfold and contacts a target with its folded together side edges and thus, with a shape that can, and often does, inflict serious injury. The inability to predict the projectile shape that will contact the target is believed to occur when several shapes are involved such as, in the case of the above described projectile, i.e., a first shape to accommodate the size dimensions to facilitate being loaded into the 12 gauge shotgun shell, and a second shape to achieve a low lethality consequence upon impact.
Logic dictates that the need to change shapes during flight is a happenstance that perhaps most often will occur but which might not occur on occasion due to the shape-change complication.
Broadly, it is an object of the present invention to provide a low lethality anti-personnel projectile overcoming the foregoing and other shortcomings of the prior art.
More particularly, it is an object to impose a low lethality contacting surface of the projectile at impact by the manner in which it is loaded into a weapon shell, thus requiring no shape change but maintaining in flight the singular shape involved, all as will be better understood as the description proceeds.
The description of the invention which follows, together with the accompanying drawings should not be construed as limiting the invention to the example shown and described, because those skilled in the art to which this invention appertains will be able to devise other forms thereof within the ambit of the appended claims.
By way of one example of many to serve as background in understanding the present invention, in police management of an unruly crowd, even kept at bay by a barricade, it often escalates to a confrontation between the police and an individual crossing the barricade, which necessitates management of the individual. It is police standard operating procedure to limit force in such a confrontation commensurate to the danger posed. A first and lowest level of force dictated by the circumstances would be to strike the individual, typically at eight to twenty yards, with a low lethality munition, i.e., a munition that does not kill or seriously maim the individual. If, however, continuing with the example, the individual withdraws a concealed weapon, the use of a lethal munition would be dictated.
To qualify a munition as being of low lethality, and as best understood from
Underlying the present invention is the recognition that projectile 10, although having physical attributes that might disqualify it as low lethality, can be shaped preparatory to being fired along a path of flight 18 to the target 12 with a blunt or flat end 20 and, most important, that this optimum shaped end 20 is effectively maintained during flight 18 by air resistant forces 22 exerted against the front or blunt end 20 of the projectile 10 and the opposite direction flight-propelling forces 24 exerted against the rear end 26 of the projectile 10. Stated somewhat differently, the opposing forces 22 and 24 maintain an interposed cylindrical shape 28 in the body of the projectile 10, and this shape 28 is characterized by the noted blunt end 20 and, as a result, does not impact upon the target 12 with a lethal consequence.
In practice in fact, the opposite directional forces 22 and 24 cause the projectile blunt end 20 to undergo a progressive expanse during flight, as noted at 21, and at impact, as noted at 23.
To achieve low lethality utility, projectile 10 is constructed using a tubular sock-like body of stretchable fabric construction material 32 having a closed front end 34 and a rear edge 36 bounding an opening 38 into a body compartment 40. In a work-in-process condition, as illustrated in
To launch or propel the constructed projectile of
Each shell is generally designated 50, and the
For completeness' sake, it is noted that although the dimensions of the 37 mm weapon shell are well known, that these dimensions as related to the loading of the projectile 10 within the compartment 54 are a compartment length 72 of 3.5 inches with the propellant 66 in place and a diameter 74 of approximately 1.5 inches, and that the 40 mm weapon shell similarly has a compartment length of 3.5 inches, not including the propellant 66, and a slightly larger diameter. It is noted that in practice best results are achieved with a constructed projectile 10 having a length 76 from its closed end 34 to the applied tie of approximately 4 inches and, flattened by slight finger pressure, a maximum width 78 of approximately 2 inches. The tail 48 is cut to length 80 but preferably should not exceed 4 inches.
The dimensions of the 12-gauge shell are also well known. These dimensions are related to the loading of the projectile 10 within the compartment 54 and are a compartment length 72 of 2{fraction (1/16)}ths inches and a diameter 74 of ⅜ths of an inch. It is noted that best results have been observed with a constructed projectile 10 having a length 76 from its closed end 34 to the applied tie of approximately 1¾ inches and, flattened by slight finger pressure, a maximum width 78 of approximately 1 inch. The tail 48 is cut to length 80 but preferably should not exceed 2½ inches.
The bulk of the
In the preferred loading sequence of the projectile 10 into the shell compartment 54, the tail 48 is folded into a resulting bulk, as at 84, and in this folded configuration is urged in movement 86 into the compartment 54, as illustrated in
Alternatively, the projectile 10 can be inserted through a funnel (not shown); preferably tail first, and will assume a folded configuration as a result of being compressed between the deformable mass-filled body 32 and the rear confines of the shell 50. After either loading sequence, the shell front end opening 58 in then closed in a well known fashion by an appropriate closure 88 appropriately seated and held in place in the end opening 58.
The propellant 66 is then ignited, in a well understood manner, by the primer 68 which, also in a well understood manner, causes the projectile 10 in the shape illustrated in
It should be noted that force 24 exists as an applied influence on the shaping of the projectile 10 during flight as a result of the reaction to the decelerating force 22, but not as part of the force causing the projectile 10 to be accelerated down the barrel of the launching weapon which, as generally understood, is a force of the expanding gas phenomenon of the ignited primer 68, since said expanding gas force ceases when the projectile 10 exits from the weapon barrel.
It is further to be noted that the projectile 10 requires ballast which as hereinbefore noted preferably is to consist of the deformable mass 42 which in practice provides a desired volume, a weight not exceeding 60 grams in the size fabric body 32 noted and is particulate in nature. However, it is to be understood that deformable masses 42 and particulate ballast pellets of materials other than rubber can be used and provide similar projectile weight and volume to achieve a low lethality consequence.
While the apparatus for practicing the within inventive method, as well as said method herein shown and disclosed in detail is fully capable of attaining the objects and providing the advantages hereinbefore stated, it is to be understood that it is merely illustrative of the presently preferred embodiment of the invention and that no limitations are intended to the detail of construction or design herein shown other than as defined in the appended claims.
Although the invention has been described in detail with reference to one or more particular preferred embodiments, persons possessing ordinary skill in the art to which this invention pertains will appreciate that various modifications and enhancements may be made without departing from the spirit and scope of the claims that follow.
This application is a continuation of U.S. application Ser. No. 10/114,726 filed Apr. 4, 2002, which is a continuation of earlier filed U.S. application Ser. No. 09/648,559 filed Aug. 28, 2000, which is a continuation-in-part of U.S. patent application Ser. No. 09/434,453 filed Nov. 5, 1999, now U.S. Pat. No. 6,202,562.
Number | Date | Country | |
---|---|---|---|
Parent | 10114726 | Apr 2002 | US |
Child | 10873331 | Jun 2004 | US |
Parent | 09648559 | Aug 2000 | US |
Child | 10114726 | Apr 2002 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 09434453 | Nov 1999 | US |
Child | 09648559 | Aug 2000 | US |