This invention relates to Ammunition and more specifically to tracer projectiles.
After the advent of automatic weapon technology there emerged a need to be able to guide the stream of projectiles at night or under adverse conditions where conventional sighting methods were ineffective. Prior to and during World War 1 major military powers developed projectiles which included brightly burning chemical compounds that created a “trace” or streak of light that could be used in aiming.
Typically these “tracing projectiles” are interspersed with standard bullets, armor piercing variety or other types in a proportion of one to five per each five rounds depending on operational requirements. Due to the rapid firing rate of the automatic weapon and the comparatively slow response time of the human eye, the traces produced appear to be a continuous “beam of light” to the operator.
To produce a tracing round, a hollow base projectile is packed with a pyrotechnic composition or base charge designed to burn brightly in the visible or non-visible spectra. The base charge can be directly packed in the hollow base, a previously formed pyrotechnic compound pellet can be inserted into the cavity, or a previously similarly packed cup can be inserted into the cavity. During packing a conical shape of the surface of the chemical compound is finally impressed, to provide a larger surface area for ignition. An igniter charge is commonly layered over the base charge to facilitate ignition.
The base charge as well as any igniter charges are quite hydrophilic and are often sealed against moisture and protected with varying degrees of success. Conventionally, either no sealant is applied, varnish is applied to the surface as a sealant and moisture barrier, or copper discs are pressed into the base to protect the compound during storage prior to loading.
Unfortunately, since the invention of the tracing projectile more than one hundred years ago there has been little progress beyond improved chemical compositions for the main pyrotechnic charge. At the US Army Lake City Army Ammunition Plant (LCAAP) facility, machinery produced for WW-1 preparation of 0.30 caliber tracing projectiles and originally designed to be driven by overhead shafts and leather belts are still used today to make 7.62×51 mm M62 Tracers.
In addition, the current designs of tracing projectiles specify a thin Copper disc “seal” be placed over the base of the bullet covering the chemical compound which neither fulfills the function of preventing moisture intrusion nor enhances ignition of the compound due to its inflammable nature. Copper tracing projectile discs are apparently only present to protect the compound from damage from bullet tips when stored in bulk containers prior to loading into cartridges. Moisture penetration is confirmed by the fact that LCAAP projectiles are stored in desiccant containers to preserve their function and some current US specifications call for 70-yard minimum ignition which may be the best that can be achieved with an inflammable metal disc in the way of the flame from combustion within the cartridge.
An additional problem with conventional tracer projectiles is that the combustion of material from the large cavity quickly changes the ballistics of the projectile causing it to deviate from the path of the conventional projectiles fired with it. This result is exacerbated by the increased cavity needed to provide space for the conical depression to increase surface area.
It would be highly advantageous, therefore, to remedy the foregoing and other deficiencies inherent in the prior art.
An object of the present invention is to provide a sealed tracer projectile that protects the tracing compound, enhances ignition and provides a moisture resistant seal as well.
Briefly to achieve the desired objects and advantages of the instant invention in accordance with a preferred embodiment provided is a tracer projectile used in a tracer round for a firearm. The tracer projectile includes a body having a forwardly directed tip and a rearwardly directed trailing end. A cavity is formed in the trailing end of the body with a rearwardly directed opening. A tracer composition is contained in the cavity, and an igniter sealant overlies the tracer composition, closing and sealing the rearwardly directed opening of the cavity. The igniter sealant is a hardened layer protecting the underlying tracer composition, sealing the cavity from moisture ingress, and is flammable to ignite the underlying tracer composition.
Also provided is a method of fabricating a tracer projectile including the steps of providing a projectile body having a forward end, a trailing end, and a cavity in the trailing end with a rearwardly directed opening. A tracing composition is placed in the cavity, the tracing composition having a rearwardly facing surface. A fluid igniter sealant including an epoxy resin, a mercaptan hardener, and a flammable additive is mixed. The fluid igniter sealant is deposited over the surface of the tracing composition, closing the rearwardly directed opening. A hardened igniter sealant is formed by curing the fluid igniter sealant The hardened igniter sealant overlying the tracer composition, closing and sealing the rearwardly directed opening of the cavity, the hardened igniter sealant protecting the underlying tracer composition, sealing the cavity from moisture ingress, and being flammable to ignite the underlying tracer composition.
Specific objects and advantages of the invention will become readily apparent to those skilled in the art from the following detailed description of a preferred embodiment thereof, taken in conjunction with the drawings in which:
Turning now to the drawings in which like reference characters indicate corresponding elements throughout the several views, attention is directed to
An additional problem with conventional trace projectile 10 is that the combustion of material from the large cavity quickly changes the ballistics of the projectile causing it to deviate from the path of the conventional projectiles fired with it. This result is exacerbated by the increased cavity needed to provide space for conical depression 20.
Turning now to
It will be understood that while tracer projectile 30 includes a jacket 32, an unjacketed projectile can also be employed with cavity 35 formed in the base thereof. Referring now to
In the previous embodiments, igniter sealant 42, 142 can contain formulations which delay the ignition of the tracer while still assuring initiation. Upon firing, the projectile may appear dimly visible or visible only within the infrared spectrum until the surface combustion of the igniter sealant 42, 142 penetrates to underlying tracing composition 38, 138. At that time the tracer may be seen for a longer range by virtue of a delay in the ordinary ignition range of the projectile. Further extension of visible burning range is increased with the increased internal volume of tracing composition 38, 138 due to the elimination of the conical depression. Similar changes in the distance which trajectory disturbing imbalances accrue, enhancing accuracy and trajectory match also improve. In this manner, a reliably sealed and igniting tracer projectile can be produced that rather than burning from, for example, 70 yards to 2,950 yards with only a 660 yard match to the standard projectiles, the tracer may burn from an agreed upon ignition range, then last longer than the 2,880 yards above and loses balance more slowly due to more volume of compound at the base of the projectile. This enables an estimated distance of trajectory match to the other four rounds it is supposed to be guiding to the target to increase substantially.
In the previous embodiments, ignition sealant 42, 142 is an epoxy resin with hardener that will seal and protect the underlying tracer composition. The epoxy with hardener will cure very hard for protection and prevent moisture ingress. Flammable additives are added to both the resin and the hardener and can be adjusted for a quick hot burn or a slower cooler burn as desired. The flammable epoxy resin includes at least 60% by weight epoxy resin and 40% or less by weight flammable additive. The hardener is at least 60% hardener by weight and 40% or less by weight, flammable additive. The preferred hardener is a composition of Mercaptan Terminated Polymer (60-100% by weight), Substituted Aminophenol (7-13% by weight) and Carbon Black (1-5% by weight). The epoxy resin is preferably a Bisphenol A Epoxy Resin. To these compositions are added a flammable additive. The flammable additive can include one or more different agents including a carbonaceous agent and a metallic agent. The carbonaceous agent includes but is not limited to carbon black, nitrocellulose, nitrosamines, and hydrocarbons. Metallic agents include but are not limited to powdered metal such as powdered aluminum and the like.
Turning now to
The present invention is described above with reference to illustrative embodiments. Those skilled in the art will recognize that changes and modifications may be made in the described embodiments without departing from the nature and scope of the present invention. Various changes and modifications to the embodiments herein chosen for purposes of illustration will readily occur to those skilled in the art. To the extent that such modifications and variations do not depart from the spirit of the invention, they are intended to be included within the scope thereof.
This application claims the benefit of U.S. Provisional Patent Application No. 63/596,956, filed 7 Nov. 2023.
Number | Date | Country | |
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63596956 | Nov 2023 | US |