Hunting projectile

• US 10,222,187 B2
• Filed: 07/11/2017
• Issued: 03/05/2019
• Est. Priority Date: 07/11/2016
• Status: Active Grant

• Current Assignee: Federal Cartridge Company (Vista Outdoor Inc.)
• Original Assignee: Vista Outdoor Operations LLC (Vista Outdoor Inc.)
• Inventors: Laska, David M., Peterson, Bryan P.
• Primary Examiner(s): Semick, Joshua T
• Application Number:
  US15/646,832
• Publication Number:
  US 20180010896A1
• Time in Patent Office: 602 Days
• CPC Class Codes: F42B 12/34 expanding before or on impact, i.e. of dumdum or mushroom type
• CPC Class Codes: F42B 33/00 Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor F42B5/188 takes precedence; manufacturing processes for hollow charges F42B1/036; manufacture of blasting cartridge initiators F42B3/195
• CPC Class Codes: F42B 33/001 Devices or processes for assembling ammunition, cartridges or cartridge elements from parts
• CPC Class Codes: F42B 5/02 Cartridges, i.e. cases with charge and missile

Abstract

A projectile comprises a projectile body including a tail portion, a barrel engaging portion, a nose portion, a grooved portion, and a tip portion disposed along a central longitudinal axis of the projectile body. The tail portion has a rearward facing surface defining an plane. The tail portion extends forwardly along the central longitudinal axis of the projectile body between the rearward facing surface and the barrel engaging portion of the projectile body. The central longitudinal axis being orthogonal to the plane defined by the rearward facing surface.

Claims

1. A projectile comprising:

a homogeneous projectile body including a tail portion, a barrel engaging portion, a nose portion, a grooved portion, and a tip portion disposed along a central longitudinal axis of the projectile body;

the tail portion having a rearward facing surface defining an XY plane, the tail portion extending forwardly along the central longitudinal axis of the projectile body between the rearward facing surface and the barrel engaging portion, the central longitudinal axis being orthogonal to the XY plane, the tail portion having a tail radius extending between the central longitudinal axis and an outer surface of the tail portion, the tail radius increasing as the tail portion extends forwardly along the central longitudinal axis;

the barrel engaging portion of the projectile body extending forwardly along the central longitudinal axis between the tail portion and the nose portion, the barrel engaging portion having a barrel engaging radius extending between the central longitudinal axis and an outer surface of the barrel engaging portion, the barrel engaging radius remaining substantially constant as the barrel engaging portion extends forwardly along the central longitudinal axis so that the barrel engaging portion has a shape generally corresponding to the shape of a cylinder;

the nose portion of the projectile body extending forwardly along the central longitudinal axis between the barrel engaging portion and the grooved portion, the nose portion having a nose radius extending between the central longitudinal axis and an outer surface of the nose portion, the nose radius decreasing as the nose portion extends forwardly along the central longitudinal axis so that the nose portion has a shape generally corresponding to the shape of an ogive, the nose portion having an interior surface and a nose wall extending between the interior and exterior surfaces thereof;

the grooved portion of the projectile body extending forwardly along the central longitudinal axis between the nose portion and the tip portion;

the tip portion of the projectile body extending forwardly along the central longitudinal axis between the grooved portion and a forward facing edge of the tip portion, the forward facing edge defining an opening in the tip portion, the opening fluidly communicating with an interior cavity extending from the opening to a cavity end point within the nose portion, a forward portion of the interior cavity being defined by an interior surface of the tip portion, the tip portion having an exterior surface that is convex when viewed in a longitudinal cross-section of the projectile body, the tip portion having a tip wall extending between the interior and exterior surfaces thereof;

the grooved portion of the projectile body having first and second groove defining surfaces, the first and second groove-defining surfaces displaced from the forward facing edge of the tip portion and defining an internal annular groove, the first groove defining surface meeting the interior surface of the tip portion at a forward edge of the annular groove, the second groove defining surface meeting an interior surface of the nose portion at a rearward edge of the annular groove, the first and second groove defining surfaces intersecting and defining an apex of the annular groove, the first and second groove defining surfaces defining an included angle of the annular groove, the included angle having a magnitude of less than 90 degrees;

the nose wall having a minimum thickness at the rearward edge of the annular groove, the tip wall having a maximum thickness at the forward edge of the annular groove, the minimum thickness of the nose wall being greater than the maximum thickness of the tip wall.

2. The projectile of claim 1 wherein the included angle is between 60 degrees and 90 degrees.

3. The projectile of claim 1 wherein the projectile body is formed of copper.

4. The projectile of claim 3 wherein the projectile has a barrel engaging radius of between 0.07 inches and 0.25 inches.

5. The projectile of claim 1 wherein the interior surface of the tip portion is concave when viewed in a longitudinal cross-section of the projectile body.

6. The projectile of claim 1 wherein the interior surface of the tip portion is convex when viewed in a longitudinal cross-section of the projectile body.

7. The projectile of claim 1 wherein the thickness of the tip wall at the forward edge of the annular groove is between 0.010 inches and 0.038 inches.

8. The projectile of claim 7 wherein the thickness of the tip wall at the forward edge of the annular groove is between 0.012 inches and 0.028 inches.

9. The projectile of claim 1 wherein the thickness of the nose wall at the rearward edge of the annular groove is between 0.015 inches and 0.050 inches.

10. The projectile of claim 9 wherein the thickness of the nose wall at the rearward edge of the annular groove is between 0.016 inches and 0.036 inches.

11. The projectile of claim 1 wherein the annular groove is generally V-shaped when viewed in a longitudinal cross-section of the projectile.

12. The projectile of claim 1 wherein the interior cavity extends rearward from the opening along the central longitudinal axis by a distance more than 35% of an overall length of the projectile body.

13. The projectile of claim 12 wherein the interior cavity extends rearward from the opening along the central longitudinal axis by a distance more than 45% of an overall length of the projectile body.

14. The projectile of claim 1 wherein the annular groove has a depth extending laterally outward from the rearward edge of the annular groove that is greater than 33% of the minimum thickness of the nose wall.

15. The projectile of claim 1 wherein the annular groove has a depth extending laterally outward from the forward edge of the annular groove that is greater than 33% of the maximum thickness of the tip wall.

16. A centerfire rifle cartridge comprising a casing with a primer, propellant in the casing, and a hollow point bullet in the casing, the hollow point bullet being homogeneous and comprising copper, the bullet having a forward end with a lip defining a mouth and an interior sidewall defining a cavity extending rearwardly from the lip, the interior sidewall having a forward sidewall portion extending from the forward lip and converging to a neck portion of the sidewall and defining a first funnel portion, the interior sidewall at a mid-sidewall portion contiguous with and rearward of the neck portion, the mid-sidewall portion diverging to an increased diameter portion, the interior sidewall converging from the increased diameter portion to a rearward-most terminus of the cavity, the forward sidewall portion at the first funnel portion having an internal circumferential notch intermediate the mouth of the cavity and the neck portion, the internal circumferential notch defined by a two groove surfaces, the groove surfaces spaced rearwardly from the mouth.

17. The projectile of claim 16 wherein the annular groove is generally V-shaped when viewed in a longitudinal cross-section of the projectile.

18. The projectile of claim 16 wherein the interior cavity extends rearward from the opening along the central longitudinal axis by a distance more than 35% of an overall length of the projectile body.

19. The projectile of claim 16 wherein the projectile has a barrel engaging radius of between 0.07 inches and 0.25 inches.

20. The projectile of claim 16 wherein the annular groove is generally V-shaped when viewed in a longitudinal cross-section of the projectile, the interior cavity extends rearward from the opening along the central longitudinal axis by a distance more than 35% of an overall length of the projectile body, and the projectile has a barrel engaging radius of between 0.07 inches and 0.25 inches.