Patent Application
20230366644
A gas piston is used in firearms to drive an operating rod after a round is fired to first eject a spent casing and reload the next round into the chamber. The gas piston is responsive to expanding propellant gases of the fired round. The gas piston is subject to exposure to not only the propellant gases but also other particulates contained in the gas such as carbon deposits from gunpowder and extreme heat resulting from combustion. Gas piston driven firearms are reliable and proven and seldom are subject to redesigns or major improvements. For example, the gas piston design of the M14 has remained unchanged for over 50 years.
A gas piston according to various aspects of the present technology comprises a helical groove disposed along an exterior surface. The helical groove may comprise curved edges at transitions between a crest and root of the helical groove. The helical groove allows for easier movement of the gas piston within its operating cylinder, provides enhanced resistance to particulate build up, and improves firing accuracy.
A more complete understanding of the present technology may be derived by referring to the detailed description when considered in connection with the following illustrative figures. In the following figures, like reference numbers refer to similar elements and steps throughout the figures.
The present technology may be described in terms of functional block components and various processing steps. Such functional blocks may be realized by any number of components configured to perform the specified functions and achieve the various results. For example, the present technology may employ various materials, finishes, dimensions, and geometries, which may carry out a variety of operations suited to a specified application or environment. In addition, the present technology may be practiced in conjunction with any number of systems configured for operation with firearms, and the system described is merely one exemplary application for the technology. Further, the present technology may employ any number of conventional techniques for machining, metalworking, and gunsmithing.
Methods and apparatus for a gas piston for a firearm according to various aspects of the present technology may operate in conjunction with any type of rifle or mechanisms used in firearms. Various representative implementations of the present technology may be applied to retrofitting an existing automatic or semi-automatic rifle, modifying a new firearm, or manufacturing a new firearm. For example, the described technology may be used to replace or modify an original factory installed gas piston mechanism in a M14 rifle to provide improved operation.
Referring now to
The first chamber 302 is positioned within the first section 102 and comprises an opening located at a first end portion 306 of the gas piston 100 such that propellant gases may flow freely out of the first end portion 306. The second chamber 304 is positioned within the second section 104 of the gas piston 100 and may extend slightly into the first section 102. The second chamber 304 has a smaller diameter than that of the first chamber 302. The first and second chambers 302, 304 are interconnected with each other at or near the mid-portion of the dual chambered body proximate the gas port 202 such that propellant gas is able flow into both chambers 302, 304 after passing through the gas port 202. The second chamber 304 is sealed at or near a second end portion 308 of the gas piston 100 such that propellant gas acts on the second end portion 308 to move the gas piston 100 within its operating cylinder (not shown) of the firearm.
The series of individual grooves 106 form parallel channels between the first end portion 306 and the gas port 202. The series of individual grooves 106 allow gas exiting out of the opening in the first end portion 306 to pass over the exterior of the gas piston 100 and out of an exhaust port of the firearm during operation.
With reference now to
With particular reference now to
The roots 802 may comprise any suitable size or shape. The roots 802 may have a width (distance between adjacent crests 804) of any suitable amount and may be less than, equal to, or greater than the width of an individual crest 804. For example, in one embodiment, the roots 802 may comprise a squared channel having a width that is equal to the width of the crests 804. In another embodiment, the roots 802 may comprise a radiused cut having a smoothly curved surface that extends between adjacent crests 804. A depth of each root 802 may be approximately equal to the width between crests 802. For example, in one embodiment, the roots 802 may comprise a width of between about 1.0 mm (0.04″) and about 2.5 mm (0.10″) and the lowermost surface of each root 802 may have a depth equal to the width. In yet another embodiment, the width of each root 802 may be between about 1.2 and about 2.5 times greater than the width of the crest 804.
The helical groove 402 may progress along the length of the first section 102 by any suitable or desired degree. For example, in one embodiment, the helical groove may comprise a pitch of between about 2.39 mm (0.94″) and about 2.67 mm (0.105″). In another embodiment, the pitch of the helical groove 402 may be determined according to a desired number of roots 802 and crests 804 for a given length of the helical groove 402 along the first section 102. For example, if the helical groove 402 comprises a length of about 23 mm and the desired number of roots 802 and crests 804 is 9, then the pitch of the helical groove 402 may be set accordingly to meet that requirement. Increasing or decreasing the pitch results in a greater or lesser number of roots 802 and crests 804 which may be used to increase or decrease the ease at which the gas piston 400 is able to slide within the operating cylinder during use.
A curved root 802 may allow the helical groove 402 to be cleaned of debris easier than a root 802 having sharply angled corners. The curving nature of the roots 802 may also allow carbon build up during use to provide a smoother sliding action within the piston cylinder (not shown) after a round is fired compared to the prior art gas piston 100.
An unexpected result of the combination of the helical groove 402 and a curved root 802 is improved accuracy of the firearm during use. For example, when the disclosed gas piston 400 having a crest 804 with a width of about 1 mm (0.04″) and a root with a width of about 1.5 mm (0.06″) is used in a M14 rifle, accuracy of the firearm was improved by up to 56% compared to the standard prior art gas piston 100.
The particular implementations shown and described are illustrative of the technology and its best mode and are not intended to otherwise limit the scope of the present technology in any way. Indeed, for the sake of brevity, conventional manufacturing, connection, preparation, and other functional aspects of the system may not be described in detail. Furthermore, the connecting lines shown in the various figures are intended to represent exemplary functional relationships and/or steps between the various elements. Many alternative or additional functional relationships or physical connections may be present in a practical system.
In the foregoing specification, the technology has been described with reference to specific exemplary embodiments. Various modifications and changes may be made, however, without departing from the scope of the present technology as set forth in the claims. The specification and figures are illustrative, rather than restrictive, and modifications are intended to be included within the scope of the present technology. Accordingly, the scope of the technology should be determined by the claims and their legal equivalents rather than by merely the examples described.
For example, the steps recited in any method or process claims may be executed in any order and are not limited to the specific order presented in the claims. Additionally, the components and/or elements recited in any apparatus claims may be assembled or otherwise operationally configured in a variety of permutations and are accordingly not limited to the specific configuration recited in the claims. Benefits, other advantages and solutions to problems have been described above with regard to particular embodiments; however, any benefit, advantage, solution to problem or any element that may cause any particular benefit, advantage or solution to occur or to become more pronounced are not to be construed as critical, required or essential features or components of any or all the claims.
As used herein, the terms “comprise,” “comprises,” “comprising,” “having,” “including,” “includes,” or any variation thereof, are intended to reference a non-exclusive inclusion, such that a process, method, article, composition or apparatus that comprises a list of elements does not include only those elements recited, but may also include other elements not expressly listed or inherent to such process, method, article, composition or apparatus. Other combinations and/or modifications of the above-described structures, arrangements, applications, proportions, elements, materials or components used in the practice of the present technology, in addition to those not specifically recited, may be varied or otherwise particularly adapted to specific environments, manufacturing specifications, design parameters or other operating requirements without departing from the general principles of the same. Any terms of degree such as “substantially,” “about,” and “approximate” as used herein mean a reasonable amount of deviation of the modified term such that the end result is not significantly changed. For example, these terms can be construed as including a deviation of at least ±5% of the modified term if this deviation would not negate the meaning of the word it modifies.
This application claims the benefit of U.S. Provisional Patent Application No. 63/306,183, filed on Feb. 3, 2022, and incorporates the disclosure of this application by reference.
| Number | Date | Country | |
|---|---|---|---|
| 63306183 | Feb 2022 | US |
