Advanced aerodynamic projectile and method of making same

Abstract

A projectile is improved aerodynamically by cutting grooves having parabolic transitions between the depth of the groove and the bearing surface. An ejectable tip is attached to the leading edge of the projectile to facilitate greater ballistic coefficient during flight and improved expansion upon impact at a soft target.

Claims

1. A projectile comprising: a projectile body comprising a nose portion, a tail portion, a base, a bearing surface, and a groove cut into the bearing surface, wherein the portion of the projectile between the bearing surface and the groove comprises a curved first transition portion, wherein the curved first transition portion is convex from the bearing surface to the groove relative to a longitudinal axis defined by the center of the nose portion and the center of the base, wherein the curved first transition portion is tangential to the bearing surface, and wherein the curved first transition portion is defined by the von Karman equation.

2. The projectile of claim 1, wherein the projectile body is manufactured from a material containing at least one of copper, tin, tungsten, aluminum, iron, or gilding metal.

3. The projectile of claim 1, further comprising: a hollow meplat having a nose rim surrounding an opening; a nose wall extending from the nose rim toward the base of the projectile; a seating channel; and a tip operable to be seated in the seating channel, the tip comprising a shank, a seating face, a tip nose, and a tip meplat, wherein the tip shank is configured to fit inside the seating channel, and wherein the tip is configured to eject from the hollow meplat after impact with a soft target.

4. The projectile of claim 3, wherein after impact, the seating face of the tip is configured to transfer force from the impact to the nose rim, and wherein the nose wall is configured to deform sufficiently under the transferred force to disrupt the seating of the tip shank in the seating channel.

5. The projectile of claim 4, further comprising a fracture groove in the interior of the hollow meplat, wherein the fracture groove is configured to assist fracturing of the nose wall to facilitate expansion of the projectile.

6. The projectile of claim 4, wherein the tip is aluminum and the projectile body is one of copper or a copper alloy.

7. The projectile of claim 3, the tip further comprising a beveled transition having a maximum diameter less than the seating surface, wherein the beveled portion reduces from the seating face to the shank, and where in the shank is operable to be seated in the seating channel, and the seating face is operable to be disposed against the nose rim when the shank is seated in the seating channel.

8. The projectile of claim 3, wherein the tip is manufactured from a material with greater hardness than the material of the projectile body.

9. The projectile of claim 3, wherein the tip is comprised of a metal having a greater hardness than the material of the projectile body.

10. The projectile of claim 1, further comprising a curved second transition portion between the bearing surface and the groove.

11. The projectile of claim 10, wherein the curved second transition portion is defined by the von Karman equation.

12. The projectile of claim 1, wherein the nose portion has an ogive shape.

13. The projectile of claim 12, wherein the tail portion has a parabolic cross-section from the bearing surface to the base.

14. The projectile of claim 1, wherein the nose portion, tip, and base are manufactured with at least a portion of an ogive shape.

15. The projectile of claim 14, wherein the at least a portion of an ogive shape is defined by the von Karman equation.

16. The projectile of claim 1, wherein the projectile comprises at least one additional groove cut into the bearing surface, wherein each additional groove has a curved first transition portion and a curved second transition portion.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a representation of a completed projectile in accordance with an embodiment of the invention;

(2) FIG. 1A is a cutaway view of the projectile shown in FIG. 1;

(3) FIG. 1B is an expanded view of the transitions between the bearing surface and the grooves in accordance with an embodiment of the invention;

(4) FIG. 2 is a representation of the tip portion of the projectile shown in FIGS. 1 & 2;

(5) FIG. 3 is a perspective view of the projectile shown in FIGS. 1 & 2 without the tip portion; and

(6) FIG. 4 is an enlarged view of the bearing surface, grooves, and transition portions of the projectile of FIGS. 1 & 1A.

DETAILED DESCRIPTION OF THE INVENTION

(7) In accordance with embodiments of the invention, a machined stock of copper, copper alloy, or other suitable materials for use as rifle projectiles, are manufactured to reduce drag and increase the ballistic coefficient of the projectile. Additionally, the projectiles are designed to achieve greater muzzle velocity through reduced bearing surface and reduce fouling in a steel or chrome-lined barrel.

(8) FIGS. 1 & 1A show an embodiment of the present invention. Projectile 10 shows a tip 20, a nose 30, grooves 40, bearing surfaces 50, tail portion 60, and base 70. Although not necessary, in a preferred embodiment, the projectile is machined of a uniform material, such as copper or copper alloy. The nose portion 30 includes a meplat 32 and a nose transition 34 where the nose meets the bearing surface. The shape of nose 30 is typically an ogive, which reduces the coefficient of drag of the projectile 10 and increases the ballistic coefficient. Because of the supersonic, and sometimes hypersonic, velocities of projectiles made in accordance with the present invention, the ogive is manufactured with a shape determined by applying the Von Karman equation. Typically, the bearing surface 50 is sized for the caliber of rifle designed for the projectile. For example, a .30 caliber rifle would fire a projectile with a diameter at the bearing surface 50 of 0.308 or 7.62 mm. The tail portion 60 is typically a boat tail design, and in the preferred embodiment, tail portion 60 also has tail transition 62 where the rearward-most bearing surface 50 ends and the tail begins to taper at tail surface 64 the shape of an ogive, or portion thereof, to the base 70. In certain embodiments, tail portion 60 need not be boat tail, parabolic, or ogive in shape, but reducing the diameter of the tail portion 60 from a tail transition 62 to base 70 has been shown to increase the ballistic coefficient of projectile 10. Base 70 may be flat, concave, or convex.

(9) As shown in FIGS. 1 and 1A, and in greater detail in FIG. 4, the bearing surface 50 has at least one groove 40 cut into it. Grooves 40 reduce the bearing surface in contact with the rifling of a barrel. Reducing the bearing surface has advantages. For example, in the case of a swaged lead jacketed bullet, the softer lead core allows the core to be deformed more easily under pressure from the lans of the rifle barrel, which reduces the amount of jacket material deposited in the interior of the barrel. However, with a projectile manufactured with a uniform material, such as copper, the projectile resists deformation, resulting in the lans cutting more copper when the projectile travels down the barrel. This additional projectile material increases barrel fouling, and can impede the projectile's travel through the barrel, potentially increasing pressure and friction and reducing muzzle velocity.

(10) Grooves 40, however, both reduce the area of bearing surfaces 50, and provide a volume between the barrel and the projectile 10 that allows for the deposit of projectile material cut by the lans of the barrel as the projectile 10 travels down the barrel before exiting the muzzle.

(11) In a preferred embodiment, the grooves 40 are cut into the bearing surface 50 such that the overall diameter at the groove is only slightly less than the bearing surface diameter. During testing, the inventors found that for a .308 caliber projectile, for example, the depth of grooves 40 is optimally 0.006 inches, such that the diameter of the projectile 10 at a groove 40 is 0.012 less than the 0.308 diameter of the bearing surface. As stated previously in the background of the invention, however, the grooves 40 have typically been cut into the bearing surface 50 at a right angle, or normal, to the bearing surface 50, resulting in a sharp edge between the bearing surface 50 and the base of groove 40. Lead transition 42 and trail transition 44 are present between the bearing surface 50 closes to the nose 30 and tail portion 60, respectively. In order to reduce the amount of turbulence created at the transitions 42 and 44, each transition 42 and 44 has a parabolic shape. Testing to date has shown that a parabolic profile of transitions 42 and 44 in accordance with the Von Karman ogive (LD-Haack) has the greatest reduction of turbulence, and thus the greatest increase in the ballistic coefficient of a projectile 10. The parabolic or ogive shape of the transitions 42 and 44 allow the projectile 10 to pass through air with a much-reduced drag coefficient. Additionally, as many cartridges are crimped, by depressing the case mouth into a groove or cannelure of the projectile, the tapered nature of the transition 44 allows for a tighter crimp to secure the projectile 10 within a cartridge casing (not shown). The length of the transition 42 and 44 may be increased and/or decreased based on a given overall length of a projectile 10, the caliber of a projectile 10, or the number of grooves 40 desired or necessary for optimum aerodynamics. During testing, it has been shown that a 1:1:1 ratio of transition width:groove width:transition width is effective. For example, for a .308 caliber projectile 10 with two grooves 40, a groove width of 0.040, and the width of transitions 42 and 44 of 0.040 performs well, reducing the overall bearing surface to approximately 0.3 from over 0.5. This reduction of bearing surface allows for reduced friction within the barrel while still providing adequate bearing surface to maintain sufficient pressure and stabilization. For larger calibers with greater overall length, such as .338 caliber, widths of grooves 40 and transitions 42 and 44 may be used. Likewise smaller widths may be used for smaller caliber projectiles.

(12) As shown in FIGS. 1, 1A, and 2, projectile 10 also includes tip 20. Tip 20 may be of any suitable metal or polymer, but in the preferred embodiment, is it machined from aluminum. As shown in FIGS. 2 and 3, tip 20 includes a tip nose 202, a tip point 204 or 204A, seating surface 206, bevel 208, and shank 210.

(13) As shown in FIG. 3, projectile 10 has a hollow meplat at 32. At meplat 32, the projectile 10 includes a nose rim 302, and a seating cavity 304, a seating channel 306, fracture grooves 308, and an expansion channel 310 disposed therein. The configuration of the cavity disposed within hollow meplat 32 works in concert with tip 20 as shown in the cutaway depiction of FIG. 1A. Tip 20 may have a flat meplat at tip point 204, or may have a pointed tip point 204A. Shank 210 is configured to be inserted and secured in seating channel 306. Bevel 208 is designed to be inserted within seating cavity 304, and has a diameter less than the diameter of the seating face 206 at bevel 208's widest point. Seating face 206 is configured to rest against nose rim 302 when the tip shank 210 is inserted into the seating channel 306. In one embodiment, tip shank 210 and seating channel 306 are configured such that tip shank 210 is held in seating channel 306 by friction, though a suitable adhesive may be applied to prevent tip 20 from being prematurely ejected from hollow meplat 32.

(14) Tip 20 provides additional ballistic performance to projectile 10 by increasing the ballistic coefficient and decreasing drag during flight. Upon impact of the tip 20 with a relatively soft or fluid target, like a game animal, the impact drives tip 20 into the nose rim 32. Nose wall 312 in the vicinity of nose rim 302 is of sufficient thinness that the force of the seating face 206 of tip 20 being driven backward causes the nose wall 312 to deform. This deformation allows fluid into the hollow meplat 32 which disrupts the frictional seat of tip shank 210 in seating channel 306. Because tip 20 is preferable manufactured from a material harder than the copper or copper alloy of the rest of projectile 10, the tip 20 is ejected from the projectile 10 as it travels through a fluid target. The ejection of tip 20 may create a secondary wound channel in an animal further increasing the lethality and humaneness of a game harvest. The primary benefit, however, is that once the tip 20 is ejected from hollow meplat 32, it allows fluid to enter the seating channel and expansion channel of projectile 10. While some prior art references claim that ballistic tips such as tip 20 may aid in expansion by driving back into the projectile, the inventors' testing has shown that projectiles manufactured in accordance with the present invention provide more reliable expansion at lower velocities when tip 20 is ejected from hollow meplat 32, allowing fluid to drive expansion. Fracture grooves 308 create shear points in the hollow meplat 32, such that when fluid enters the hollow meplat, the nose wall 312 fractures at the nose groove 308. After fracture, the projectile 10 peels back to create a larger frontal surface area and thus, a greater diameter wound channel. In one embodiment, six fracture grooves 308 are formed in the interior of hollow meplat 308, though one of ordinary skill in the art will recognize that any number of grooves may be used. Additionally, expansion channel 310 is deeper than seating channel 306. During expansion, the petals created by the expansion of projectile 10 are configured peel back to the end of expansion channel 310. At lower impact velocities, expansion may not proceed all the way to the base of expansion channel 310, while at higher velocities, expansion may proceed beyond the end of expansion channel 310, as should be apparent to one of ordinary skill in the art.

(15) In practice, projectile 10 may be made from solid bar stock copper or copper alloy. The nose 30, bearing surface 50, and tail portion are typically machined by a lathe, waterjet, or CNC machine, but may also be machined using hand tools. In addition to copper, any suitable alloy may be used, such as tin, gilding metal, brass, and even mild steel, subject to law and the rules covering projectiles. In practice, the range of suitable alloys is limited only by the hardness of the barrel of the rifle used to fire the projectile, and the need for the projectile 10 to be fired reliably 26 in a firearm. Tip 20 may be machined from any suitable material, and is limited only in that tip 20 is preferably made of a harder material than the body of projectile 10 so that upon impact, it is capable of deforming the hollow meplat 32 sufficiently to create instability to eject the tip 20 upon impact, or shortly thereafter. Materials such as titanium, tungsten, steel, iron, Kevlar, and nylon may be used, subject to the limitations described herein. Additional changes and or modifications of materials, dimensions, and methods may be used in accordance with the present invention, and within the skill of one of ordinary skill in the art.