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.308 Subsonic Bullet

a subsonic bullet and bullet technology, applied in the field of subsonic bullets, can solve the problems of prior art not divulging the dimensions of subsonic bullets and the drag force of projectiles, and achieve the effect of reducing drag and optimizing flight stability

Inactive Publication Date: 2018-11-22
MCWILLIAM SR CHARLES EDMOND +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The patent is about a new subsonic bullet design that reduces drag and increases flight stability to improve accuracy. The subsonic bullet has a unique shape with a curved nose, cylindrical center, and cone-like tail that reduces turbulent airflow. It also has a copper shell filled with a low-density material in the nose and tail, which moves the center of mass as far forward as possible for further stability during flight. Additionally, the subsonic bullet is longer than supersonic bullets to increase mass and minimize voids in the powder load for better flight speeds and reduced chance of misfires.

Problems solved by technology

Meanwhile the drag force on the projectile affects its impact energy.
As noted above, the prior art does not disclose subsonic bullet dimensions, which provide for optimal flight stability and reduction of drag.

Method used

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  • .308 Subsonic Bullet
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Examples

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Embodiment Construction

[0027]Referring to the accompanying figures, a supersonic bullet 11 of the prior art is depicted in FIG. 1, and comprises a conical into parabolic nose 1 and tapered to flat tail 2, connected by a cylindrical portion with a diameter such that it fits snugly into a casing of appropriate caliber. The aerodynamics of the prior art bullet depicted in FIG. 1 are essential for supersonic flight; the pointed nose is used to reduce air pressure against the nose of the bullet with flight speeds in excess of the speed of sound. When used in subsonic applications; however, the pointed nose and flat tail 2 cause pockets of air pressure 16 buildups that increase the drag on the bullet and reduce its impact energy as noted in table 1 above and demonstrated in FIG. 6. In addition, the position of the COM (center of mass) 3 is far enough back in the bullet to cause a loss of stability at low flight speeds; even tumbling which can have a noticeably negative impact on both accuracy and precision when...

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Abstract

The invention here described of novel aerodynamics and construction has been shown to alleviate the problems inherent in subsonic ballistics, such as, but not limited to, tumbling in flight, loss of impact energy, as well as the changes in both accuracy and precision of the firearm shots fired at subsonic speeds. The subsonic bullet herein described has three main aerodynamic components that aid in subsonic flight: 1) a parabolic or hemispherical nose; 2) a cylindrical center length with parallel sides; 3) a cone-like parabolic tail with an optimized tail geometry to slowly converge the laminar flow around the bullet without introducing turbulence. These features serve to reduce air pressure and turbulent airflow around the bullet during flight.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS[0001]This application is a continuation-in-part of U.S. Non-Provisional application Ser. No. 15 / 167,251 filed on May 27, 2016, now pending, which application claims priority from U.S. Provisional Application No. 62 / 188614 filed on Jul. 3, 2015 the disclosures of which are hereby incorporated by reference in their entirety to provide continuity of disclosure.STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT[0002]Not applicable.THE NAMES OF THE PARTIES TO A JOINT RESEARCH AGREEMENT[0003]Not applicable.REFERENCE TO SEQUENCE LISTING, A TABLE, OR A COMPUTER PROGRAM LISTING COMPACT DISC APPENDIX[0004]Not applicable.BACKGROUND OF THE INVENTION[0005]This invention generally relates to firearms and ammunition, and specifically to an article and method of silencing firearm shots and usage of subsonic bullets. This invention specifically relates to an exemplary embodiment of a subsonic .308 bullet, which can be utilized with standard .308 W...

Claims

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Application Information

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IPC IPC(8): F42B10/02F42B12/74F42B12/78F42B30/02
CPCF42B10/02F42B30/02F42B12/78F42B12/74F42B5/025F42B10/44F42B10/46
Inventor MCWILLIAM, SR., CHARLES EDMONDMCWILLIAM, JAMIE GEORGE
Owner MCWILLIAM SR CHARLES EDMOND
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