US20120111220A1 - Lead-free bullet for use in a wide range of impact velocities - Google Patents

Lead-free bullet for use in a wide range of impact velocities Download PDF

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US20120111220A1
US20120111220A1 US12/100,495 US10049508A US2012111220A1 US 20120111220 A1 US20120111220 A1 US 20120111220A1 US 10049508 A US10049508 A US 10049508A US 2012111220 A1 US2012111220 A1 US 2012111220A1
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bullet
cross
sectional dimension
cavity
approximately
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US8186277B1 (en
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Gary D. King
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Nosler Inc
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Nosler Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/34Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect expanding before or on impact, i.e. of dumdum or mushroom type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/72Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
    • F42B12/74Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body

Definitions

  • This invention relates to a lead-free bullet with a blind cavity that enables outward expansion of the bullet upon impact with a target over a wide range of impact velocities.
  • Lead has been used as a material in bullets for years, and many lead bullets have a nose portion with a hollow point or hollow cavity that enables the bullet to mushroom or petal upon impact with a target. Such mushrooming disperses most or all of the bullet's kinetic energy to the target. Lead has been widely used because it has a high density, good ductility, and low cost. However, there have been assertions that lead bullets present an issue of significant environmental contamination. There have also been claims that scavenger animals, such as the California condor, may have been subjected to lead poisoning from consuming animals shot with lead projectiles.
  • U.S. Pat. No. 4,685,397 discloses a completely lead-free bullet preferably made of tombac that has a cylindrical cavity in the nose and a cap.
  • lead-free bullets generally do not have consistent performance characteristics over a wide range of velocities and uses because the materials do not have the same properties as lead. More specifically, if the opening at the nose of the bullet is too large, or if the cylindrical cavity is too deep, then the bullet may mushroom to the extent that the petals fragment from the bullet upon impact. This can reduce the efficacy of the bullet. Conversely, if the opening at the nose of the bullet is too small, then the bullet may not petal adequately upon impacting a target at low velocity. This also reduces the efficacy of the bullet.
  • FIG. 1 is an enlarged side view of a bullet in accordance with an embodiment of the invention.
  • FIG. 2A is an enlarged cross-sectional side view of an embodiment of a body of a bullet taken along line 2 - 2 of FIG. 1 .
  • FIG. 2B is an enlarged cross-sectional side view taken along line 2 - 2 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 3 is a cross-sectional top view taken along line 3 - 3 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 4 is a cross-sectional top view taken along line 4 - 4 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 5 is a cross-sectional top view taken along line 5 - 5 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIGS. 6A-6E are cross-sectional side views of various stages of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 7 is a cross-sectional side view of a bullet at a stage of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 8 is a top view of a bullet at the stage of a method for manufacturing a bullet illustrated in FIG. 7 .
  • FIG. 9 is a cross-sectional side view of a bullet at a stage of a method for manufacturing a bullet in accordance with another embodiment of the invention.
  • FIG. 10 is a top view of a bullet at the stage of a method for manufacturing a bullet illustrated in FIG. 9 .
  • FIG. 11 is an enlarged isometric view of a bullet at a stage of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 12 is a cross-sectional view of a bullet in accordance with another embodiment.
  • FIGS. 1-12 Several embodiments in accordance with the invention are set forth in FIGS. 1-12 and the following text to provide a thorough understanding of particular embodiments of the invention. Moreover, several other embodiments of the invention can have different configurations, components or procedures than those described in this section. A person skilled in the art will understand, therefore, that the invention may have additional embodiments, or that the invention may be practiced without several details of the embodiments shown in FIGS. 1-12 .
  • the bullet has a lead-free body that has a tail section and a nose section with an ogived outer surface and a forward terminus.
  • the body also has an opening at the terminus and a cavity in the nose section.
  • the cavity extends rearward from the opening to an intermediate section of the body.
  • the cavity includes a forward sidewall having at least a generally frusto-conical shape that converges rearward from the opening to a transition area and a rear sidewall extending rearward from the transition area at a different angle than the forward sidewall.
  • the bullet has a lead-free body that has a tail section, a nose section with an ogived outer surface and a forward terminus, an opening at the terminus, and a cavity in the nose section.
  • the cavity includes a forward sidewall extending rearward from the opening, skives in the forward sidewall, and a rear sidewall extending rearward relative to the forward sidewall.
  • the forward sidewall and the rear sidewall of the body of a 30 caliber, 180 grain bullet are configured to form petals that remain with the body upon impact in animal tissue at impact velocities of approximately 1,800 feet per second to approximately 3,200 feet per second.
  • impact velocities may be different.
  • the bullet has a lead-free body that has a tail section and a nose section with an ogived outer surface and a forward terminus.
  • the body also has an opening at the forward terminus and a cavity in the nose section.
  • the cavity extends rearward from the opening to an intermediate section of the body.
  • the cavity includes a forward sidewall having at least a generally frusto-conical shape that converges rearward from the opening to a transition area, and a rear sidewall extending rearward from the transition area at a different angle than the forward sidewall.
  • the body has a maximum cross-sectional dimension and the opening has a first cross-sectional dimension. The ratio of the first cross-sectional dimension to the maximum cross-sectional dimension is from approximately 0.30 to approximately 0.40.
  • the body also has a length and the ratio of the transition area location rearward of the forward terminus to the body length is from approximately 0.20 to approximately 0.25.
  • the cavity has a second cross-sectional dimension at the transition area and the ratio of the second cross-sectional dimension to the maximum cross-sectional dimension is from approximately 0.15 to approximately 0.25.
  • One embodiment of such a method comprises forming a cavity at a first end portion of a slug of lead-free material such that the cavity has an opening and a forward sidewall that has a surface converging rearward from the opening at a first angle.
  • This embodiment of the method also includes forming a rear sidewall in the cavity that extends rearward at a second angle different than the first angle, and contouring a nose portion to have an ogived outer surface and a forward terminus.
  • the cavity extends rearward from the opening to a generally hemispherical end, the forward sidewall of the cavity converges rearward from the opening to a transition area, and the rear sidewall extends rearward at a different angle than the forward sidewall from the transition area to the generally hemispherical end.
  • FIG. 1 is an enlarged side view of a bullet 100 in accordance with an embodiment of the invention.
  • the bullet 100 includes a lead-free body 105 having a tail section 115 and a nose section 120 , and the bullet 100 can further include a tip 110 at the nose section 120 .
  • the lead-free body 105 can be a continuous piece of material composed of unalloyed copper or a copper alloyed with another metal.
  • a copper-zinc alloy may reduce depositions of copper on the interior surface of a gun barrel (i.e., “fouling”) that could otherwise reduce the accuracy of the bullet.
  • One suitable copper-zinc alloy that can be used for the lead-free body 105 is a copper 210 alloy.
  • the lead-free body 105 can also be composed of other materials, such as tungsten.
  • the tip 110 can be composed of a polymeric substance.
  • the tip 110 is colored differently according to the caliber of the bullet 100 .
  • a 30-caliber bullet can have a tip with a green hue, and other calibers can have tips of different colors.
  • a user can thus easily determine the caliber of a bullet by the color of the tip 110 .
  • the color of the tip 110 can be uniform across several calibers in other embodiments.
  • FIGS. 2A-2B are enlarged cross-sectional side views taken along line 2 - 2 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • Like reference numbers refer to like components in FIGS. 1 and 2 A- 2 B, and thus the description of such components will not be repeated with reference to the bullet 100 in FIGS. 2A-2B .
  • the nose section 120 has an ogived outer surface 205 and a forward terminus 210 .
  • the body 105 has a maximum cross-sectional dimension 255 toward the tail section 115 and an opening 215 with a first cross-sectional dimension 245 at the forward terminus 210 .
  • the body 105 also has a cavity 220 in the nose section 120 that extends rearward from the opening 215 to an intermediate section of the body 105 .
  • the cavity 220 includes a forward sidewall 225 that converges rearward from the opening 215 to a first transition area 230 having a second cross-sectional dimension 240 .
  • the forward sidewall 225 in the embodiment shown in FIGS. 2A and 2B has at least a generally frusto-conical shape.
  • the embodiment of the forward sidewall 225 shown in FIGS. 2A and 2B has a slightly convex frusto-conical shape relative to the central longitudinal axis A-A of the body 105 .
  • the forward sidewall 225 can have a straight frusto-conical shape or a concave frusto-conical shape relative to the central longitudinal A-A.
  • the cavity 220 can further include one or more skives 250 extending longitudinally along the forward sidewall 225 .
  • the skives 250 can be longitudinal grooves at selected radial intervals around the inner circumference of the forward sidewall 225 .
  • the cavity 220 further includes a rear sidewall 235 that extends rearward from the first transition area 230 at a different angle relative to the forward sidewall 225 .
  • the rear sidewall 235 can diverge rearwardly to a second transition area 260 having a third cross-sectional dimension 280 and then converge to form a generally hemispherical cavity end 265 having a fourth cross-sectional dimension 275 .
  • Several embodiments of the cavity 220 shown in FIGS. 2A and 2B have an hourglass-shape.
  • the rear sidewall 235 has a straight cylindrical surface from the first transition area 230 to near the cavity end 265 that is parallel to a central longitudinal axis of the body 105 .
  • the shape and size of the combination of the cavity 220 , opening 215 and outer surface 205 enable the bullet 100 to adequately expand upon impact without breaking apart over a much wider range of velocities and target types than previous lead-free bullets.
  • This unique aspect of several embodiments of the bullet 100 can be described, at least in part, by ratios between various dimensions of the body 105 and cavity 220 .
  • the ratio of the first cross-sectional dimension 245 to the maximum cross-sectional dimension 255 is from approximately 0.30 to approximately 0.40.
  • the ratio of the second cross-sectional dimension 240 to the maximum cross-sectional dimension 255 is from approximately 0.15 to approximately 0.25.
  • the ratio of the third cross-sectional dimension 280 to the maximum cross-sectional dimension 255 is from approximately 0.20 to approximately 0.30.
  • the ratio of the fourth cross-sectional dimension 275 to the maximum cross-sectional dimension 255 can be from approximately 0.10 to approximately 0.20. The foregoing ratios are merely several examples and are not limiting unless expressly listed.
  • the body 105 further has a length 270 .
  • the first transition area 230 is located rearward of the forward terminus 210 by approximately 20-25% of the body length 270 .
  • the ratio of the second transition area 260 location rearward of the forward terminus 210 to the body length 270 can be from approximately 0.30 to approximately 0.35, and the ratio of the generally hemispherical cavity end 265 location rearward of the forward terminus 210 to the body length 270 can range from approximately 0.45 to approximately 0.50.
  • the ratios related to the length of the body are also merely examples and are not limiting unless expressly listed.
  • FIG. 2B illustrates the bullet 100 of FIGS. 1 and 2A including the tip 110 .
  • a rear portion of the tip 110 is in the cavity 220 and a forward portion of the tip 110 projects forward from the forward terminus 210 of the body 105 .
  • the rear portion of the tip 110 accordingly abuts at least a portion of the forward sidewall 225 and extends rearward in the cavity 220 .
  • FIGS. 3-5 are cross-sectional views of the bullet 100 taken along lines 3 - 3 , 4 - 4 and 5 - 5 of FIG. 1 , respectively, and like reference numbers refer to like components in FIGS. 1-5 .
  • the body 105 has a wall thickness T 1 at the line 3 - 3 shown in FIG. 1 .
  • the relatively large opening 215 ( FIG. 2A ) and the relatively thin wall thickness T 1 enable the bullet to initiate petaling along the skives 250 ( FIG. 2A ) at lower velocities and/or in softer targets than conventionally shaped lead-free bullets.
  • the body 105 also has progressively larger wall thicknesses T 2 ( FIG. 4 ) and T 3 ( FIG. 5 ) toward the tail.
  • the larger wall thickness at lines 4 - 4 and 5 - 5 prevent, or at least inhibit, the petals from separating from the body 105 at high velocity impacts. Additionally, it can be seen from contrasting FIGS. 3 and 4 that the forward sidewall 225 converges from the opening (not shown) to the first transition area (not shown) because the tip 110 in FIG. 4 has a smaller cross-section than the tip 110 in FIG. 3 .
  • the opening 215 and forward sidewall 225 are configured to initiate petal formation when the bullet 100 impacts a target. More specifically, the large opening 215 and small wall thickness T 1 enable the body 105 to readily tear at the skives 250 and cause the petals to unfold.
  • the tip 110 can further enable mushrooming because the impact force drives the tip 110 into the cavity 220 .
  • One advantage of several embodiments of the bullet 100 is that the configuration of the opening 215 , the forward sidewall 225 of the cavity 220 , and outer surface of the nose section 120 operate together with the type of material of the body such that the bullet 100 can petal at impact velocities of approximately 1,800 feet per second.
  • Another advantage of several embodiments of the bullet 100 is that it can petal upon impact without undue fragmentation at much higher impact velocities.
  • the increasing thickness of the forward sidewall 225 toward the transition zone and the relatively larger thickness of the rear sidewall 235 increase the strength of the petals toward the tail such that the bullet can mushroom at high-velocity impacts of approximately 3,200 feet per second without fragmenting the petals.
  • Such a configuration can also prevent the bullet 100 from mushrooming prematurely in flight before impacting the desired target.
  • FIGS. 6A-6E are cross-sectional side views of stages of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • a slug of lead-free material is pressed into a die cavity (not shown) to form a generally cylindrical slug 600 having a first end portion 602 with a face 620 and a second end portion 610 .
  • FIG. 6B illustrates a stage at which an axial force (not shown) has been applied to the face 620 of the first end portion 602 to form the second end portion 610 into a tail portion 615 .
  • FIG. 6C illustrates a subsequent stage at which a punch (not shown) presses against the face 620 to further form the tail portion 615 and shape the slug 600 in another die cavity (not shown).
  • the punch forms a generally annular ring portion 625 and a recess 630 at the first end portion 602 .
  • the punch of the stage shown in FIG. 6C may form a planar surface at the first end portion 602 without a ring portion or a recess.
  • the slug 600 has been formed into a body 601 having a first end portion 605 into which a first punch (not shown) has been driven to form a cavity 640 that includes a forward sidewall 635 extending rearward from the opening 630 .
  • a first punch not shown
  • FIG. 6E illustrates the process after a second punch (not shown) has been applied to the first end portion 605 to further extend the cavity 640 to include a rear sidewall 645 .
  • the first and second punches can have conical shapes at different angles such that the forward sidewall 635 tapers at a first angle and the rear sidewall 645 tapers at a second angle different than the first angle.
  • the cavity 640 can accordingly have a transition zone 650 .
  • the second punch can also have a spherical tip to form a semi-spherical end 660 .
  • FIG. 7 is a side view and FIG. 8 is a top view of a bullet at a subsequent stage of an embodiment of a method.
  • the ring portion 625 of FIG. 6E has been removed from the first end portion 605 , but the nose section of the bullet has not yet been formed.
  • the first end portion 605 has a portion 710 that will be formed into the nose section's forward terminus.
  • FIGS. 7 and 8 together further illustrate the conical surfaces of the forward sidewall 635 and rear sidewall 645 .
  • FIG. 9 is a side view and FIG. 10 is a top view of a bullet at a subsequent stage of an embodiment of the method for manufacturing a bullet.
  • Like reference numbers refer to like components in FIGS. 7-10 .
  • a third punch (not shown) has been pressed into the cavity 640 to form longitudinal skives 905 in the forward sidewall 635 by driving the edges of a pyramidal punch (not shown) that has three or more triangular faces into the forward sidewall 635 .
  • the number of faces that a pyramidal punch has determines the number of skives.
  • a four-sided pyramidal punch has four edges that form four skives.
  • the skives 905 may be formed by engraving or etching the forward sidewall 635 .
  • the skives 905 reduce the structural integrity at specific sites around the body 601 to further enable the bullet to mushroom upon impacting a target.
  • One advantage of forming the skives 905 with a pyramidal punch is that extensive working of the body 601 is not required, and thus the risk of any fragmentation of the bullet that may occur is lessened vis-à-vis other techniques.
  • FIG. 11 is an enlarged isometric view of a subsequent stage of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • the body 601 has been contoured to form a nose section 1120 .
  • the nose section 1120 can be formed by inserting the body 601 into an ogive die cavity (not shown) and applying an axial force (not shown) to the bottom face of the tail section 615 .
  • the nose section 1120 has an ogived outer surface 1125 , a forward terminus 1130 , and an opening 630 at the terminus 1130 .
  • the cavity 640 includes the forward sidewall 635 that converges rearward from the opening 630 and the rear sidewall 645 extending toward the tail at a different angle than the forward sidewall 635 .
  • FIG. 12 is a cross-sectional view of a bullet in accordance with another embodiment, and like reference numbers refer to like components in FIGS. 1-2B and 12 .
  • at least a portion of the rear sidewall 1235 has a cylindrical surface rearward from the transition area 230 .
  • the cylindrical surface for example, can extend from the transition zone to the beginning of the generally hemispherical cavity end 1265 .
  • the cross-sectional dimension 240 at the transition area 230 is the same as the cross-sectional dimension 240 at the generally hemispherical cavity end 1265 .

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  • Chemical & Material Sciences (AREA)
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Abstract

A bullet comprising a lead-free body having a tail section and a nose section. The nose section has an ogived outer surface and a forward terminus. The body further has an opening at the terminus, and a cavity in the nose section. The cavity extends rearward from the opening to an intermediate section of the body. The cavity includes a forward sidewall having at least a generally frusto-conical shape that converges rearward from the opening to a transition area. The cavity further includes a rear sidewall extending rearward from the transition area at a different angle than the forward sidewall.

Description

    CROSS-REFERENCE TO RELATED APPLICATION(S)
  • This application claims the benefit of U.S. Provisional Patent Application No. 60/923,078 filed Apr. 11, 2007, entitled “LEAD-FREE BULLET FOR USE IN A WIDE RANGE OF IMPACT VELOCITIES,” which is incorporated herein by reference in its entirety.
  • TECHNICAL FIELD
  • This invention relates to a lead-free bullet with a blind cavity that enables outward expansion of the bullet upon impact with a target over a wide range of impact velocities.
  • BACKGROUND
  • Lead has been used as a material in bullets for years, and many lead bullets have a nose portion with a hollow point or hollow cavity that enables the bullet to mushroom or petal upon impact with a target. Such mushrooming disperses most or all of the bullet's kinetic energy to the target. Lead has been widely used because it has a high density, good ductility, and low cost. However, there have been assertions that lead bullets present an issue of significant environmental contamination. There have also been claims that scavenger animals, such as the California condor, may have been subjected to lead poisoning from consuming animals shot with lead projectiles.
  • Bullet manufacturers have attempted to solve these purported problems in various ways. One such solution is to encase a lead core with a non-lead metal. For example, U.S. Pat. No. 5,127,332 discloses a hunting bullet with an encapsulated lead core that purports to minimize contamination of animal tissue. However, certain jurisdictions have entirely banned the use of bullets with any lead for hunting certain game.
  • Another solution is a completely lead-free bullet. U.S. Pat. No. 4,685,397, for example, discloses a completely lead-free bullet preferably made of tombac that has a cylindrical cavity in the nose and a cap. However, such lead-free bullets generally do not have consistent performance characteristics over a wide range of velocities and uses because the materials do not have the same properties as lead. More specifically, if the opening at the nose of the bullet is too large, or if the cylindrical cavity is too deep, then the bullet may mushroom to the extent that the petals fragment from the bullet upon impact. This can reduce the efficacy of the bullet. Conversely, if the opening at the nose of the bullet is too small, then the bullet may not petal adequately upon impacting a target at low velocity. This also reduces the efficacy of the bullet.
  • Accordingly, a lead-free bullet that has consistent performance characteristics over a wide range of velocities and uses would have significant utility.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is an enlarged side view of a bullet in accordance with an embodiment of the invention.
  • FIG. 2A is an enlarged cross-sectional side view of an embodiment of a body of a bullet taken along line 2-2 of FIG. 1.
  • FIG. 2B is an enlarged cross-sectional side view taken along line 2-2 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 3 is a cross-sectional top view taken along line 3-3 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 4 is a cross-sectional top view taken along line 4-4 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIG. 5 is a cross-sectional top view taken along line 5-5 of FIG. 1 of a bullet in accordance with an embodiment of the invention.
  • FIGS. 6A-6E are cross-sectional side views of various stages of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 7 is a cross-sectional side view of a bullet at a stage of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 8 is a top view of a bullet at the stage of a method for manufacturing a bullet illustrated in FIG. 7.
  • FIG. 9 is a cross-sectional side view of a bullet at a stage of a method for manufacturing a bullet in accordance with another embodiment of the invention.
  • FIG. 10 is a top view of a bullet at the stage of a method for manufacturing a bullet illustrated in FIG. 9.
  • FIG. 11 is an enlarged isometric view of a bullet at a stage of a method for manufacturing a bullet in accordance with an embodiment of the invention.
  • FIG. 12 is a cross-sectional view of a bullet in accordance with another embodiment.
  • DETAILED DESCRIPTION A. Overview
  • The present disclosure describes a lead-free bullet with an opening that can enable the bullet to be used over a wide range of velocities and applications. Several embodiments in accordance with the invention are set forth in FIGS. 1-12 and the following text to provide a thorough understanding of particular embodiments of the invention. Moreover, several other embodiments of the invention can have different configurations, components or procedures than those described in this section. A person skilled in the art will understand, therefore, that the invention may have additional embodiments, or that the invention may be practiced without several details of the embodiments shown in FIGS. 1-12.
  • In one embodiment, the bullet has a lead-free body that has a tail section and a nose section with an ogived outer surface and a forward terminus. The body also has an opening at the terminus and a cavity in the nose section. The cavity extends rearward from the opening to an intermediate section of the body. The cavity includes a forward sidewall having at least a generally frusto-conical shape that converges rearward from the opening to a transition area and a rear sidewall extending rearward from the transition area at a different angle than the forward sidewall.
  • In another embodiment, the bullet has a lead-free body that has a tail section, a nose section with an ogived outer surface and a forward terminus, an opening at the terminus, and a cavity in the nose section. The cavity includes a forward sidewall extending rearward from the opening, skives in the forward sidewall, and a rear sidewall extending rearward relative to the forward sidewall. Upon impact in animal tissue over a broad range of impact velocities, the forward sidewall and the rear sidewall are configured to form petals that remain with the body. For example, the forward sidewall and the rear sidewall of the body of a 30 caliber, 180 grain bullet are configured to form petals that remain with the body upon impact in animal tissue at impact velocities of approximately 1,800 feet per second to approximately 3,200 feet per second. For other bullets with other calibers and/or other grain values, the range of impact velocities may be different.
  • In still another embodiment, the bullet has a lead-free body that has a tail section and a nose section with an ogived outer surface and a forward terminus. The body also has an opening at the forward terminus and a cavity in the nose section. The cavity extends rearward from the opening to an intermediate section of the body. The cavity includes a forward sidewall having at least a generally frusto-conical shape that converges rearward from the opening to a transition area, and a rear sidewall extending rearward from the transition area at a different angle than the forward sidewall. The body has a maximum cross-sectional dimension and the opening has a first cross-sectional dimension. The ratio of the first cross-sectional dimension to the maximum cross-sectional dimension is from approximately 0.30 to approximately 0.40. The body also has a length and the ratio of the transition area location rearward of the forward terminus to the body length is from approximately 0.20 to approximately 0.25. The cavity has a second cross-sectional dimension at the transition area and the ratio of the second cross-sectional dimension to the maximum cross-sectional dimension is from approximately 0.15 to approximately 0.25.
  • Methods of manufacturing a bullet in accordance with embodiments of the invention are also described. One embodiment of such a method, for example, comprises forming a cavity at a first end portion of a slug of lead-free material such that the cavity has an opening and a forward sidewall that has a surface converging rearward from the opening at a first angle. This embodiment of the method also includes forming a rear sidewall in the cavity that extends rearward at a second angle different than the first angle, and contouring a nose portion to have an ogived outer surface and a forward terminus. The cavity extends rearward from the opening to a generally hemispherical end, the forward sidewall of the cavity converges rearward from the opening to a transition area, and the rear sidewall extends rearward at a different angle than the forward sidewall from the transition area to the generally hemispherical end.
  • B. Embodiments of Bullets and Processes of Making Bullets
  • FIG. 1 is an enlarged side view of a bullet 100 in accordance with an embodiment of the invention. The bullet 100 includes a lead-free body 105 having a tail section 115 and a nose section 120, and the bullet 100 can further include a tip 110 at the nose section 120. The lead-free body 105 can be a continuous piece of material composed of unalloyed copper or a copper alloyed with another metal. A copper-zinc alloy, for example, may reduce depositions of copper on the interior surface of a gun barrel (i.e., “fouling”) that could otherwise reduce the accuracy of the bullet. One suitable copper-zinc alloy that can be used for the lead-free body 105 is a copper 210 alloy. The lead-free body 105 can also be composed of other materials, such as tungsten. The tip 110 can be composed of a polymeric substance. In some embodiments, the tip 110 is colored differently according to the caliber of the bullet 100. For example, a 30-caliber bullet can have a tip with a green hue, and other calibers can have tips of different colors. A user can thus easily determine the caliber of a bullet by the color of the tip 110. The color of the tip 110, however, can be uniform across several calibers in other embodiments.
  • FIGS. 2A-2B are enlarged cross-sectional side views taken along line 2-2 of FIG. 1 of a bullet in accordance with an embodiment of the invention. Like reference numbers refer to like components in FIGS. 1 and 2A-2B, and thus the description of such components will not be repeated with reference to the bullet 100 in FIGS. 2A-2B. Referring to FIG. 2A, the nose section 120 has an ogived outer surface 205 and a forward terminus 210. The body 105 has a maximum cross-sectional dimension 255 toward the tail section 115 and an opening 215 with a first cross-sectional dimension 245 at the forward terminus 210. The body 105 also has a cavity 220 in the nose section 120 that extends rearward from the opening 215 to an intermediate section of the body 105. The cavity 220 includes a forward sidewall 225 that converges rearward from the opening 215 to a first transition area 230 having a second cross-sectional dimension 240. The forward sidewall 225 in the embodiment shown in FIGS. 2A and 2B has at least a generally frusto-conical shape. For example, the embodiment of the forward sidewall 225 shown in FIGS. 2A and 2B has a slightly convex frusto-conical shape relative to the central longitudinal axis A-A of the body 105. In other embodiments, the forward sidewall 225 can have a straight frusto-conical shape or a concave frusto-conical shape relative to the central longitudinal A-A. The term “frusto-conical,” accordingly, includes straight, convex and/or concave frusto-conical shapes. The cavity 220 can further include one or more skives 250 extending longitudinally along the forward sidewall 225. The skives 250, for example, can be longitudinal grooves at selected radial intervals around the inner circumference of the forward sidewall 225. The cavity 220 further includes a rear sidewall 235 that extends rearward from the first transition area 230 at a different angle relative to the forward sidewall 225. The rear sidewall 235, for example, can diverge rearwardly to a second transition area 260 having a third cross-sectional dimension 280 and then converge to form a generally hemispherical cavity end 265 having a fourth cross-sectional dimension 275. Several embodiments of the cavity 220 shown in FIGS. 2A and 2B have an hourglass-shape. In another embodiment, the rear sidewall 235 has a straight cylindrical surface from the first transition area 230 to near the cavity end 265 that is parallel to a central longitudinal axis of the body 105.
  • The shape and size of the combination of the cavity 220, opening 215 and outer surface 205 enable the bullet 100 to adequately expand upon impact without breaking apart over a much wider range of velocities and target types than previous lead-free bullets. This unique aspect of several embodiments of the bullet 100 can be described, at least in part, by ratios between various dimensions of the body 105 and cavity 220. In one embodiment, for example, the ratio of the first cross-sectional dimension 245 to the maximum cross-sectional dimension 255 is from approximately 0.30 to approximately 0.40. In another embodiment, the ratio of the second cross-sectional dimension 240 to the maximum cross-sectional dimension 255 is from approximately 0.15 to approximately 0.25. In yet another embodiment, the ratio of the third cross-sectional dimension 280 to the maximum cross-sectional dimension 255 is from approximately 0.20 to approximately 0.30. The ratio of the fourth cross-sectional dimension 275 to the maximum cross-sectional dimension 255 can be from approximately 0.10 to approximately 0.20. The foregoing ratios are merely several examples and are not limiting unless expressly listed.
  • The body 105 further has a length 270. In several embodiments, the first transition area 230 is located rearward of the forward terminus 210 by approximately 20-25% of the body length 270. Additionally, the ratio of the second transition area 260 location rearward of the forward terminus 210 to the body length 270 can be from approximately 0.30 to approximately 0.35, and the ratio of the generally hemispherical cavity end 265 location rearward of the forward terminus 210 to the body length 270 can range from approximately 0.45 to approximately 0.50. The ratios related to the length of the body are also merely examples and are not limiting unless expressly listed.
  • FIG. 2B illustrates the bullet 100 of FIGS. 1 and 2A including the tip 110. In this embodiment, a rear portion of the tip 110 is in the cavity 220 and a forward portion of the tip 110 projects forward from the forward terminus 210 of the body 105. The rear portion of the tip 110 accordingly abuts at least a portion of the forward sidewall 225 and extends rearward in the cavity 220.
  • FIGS. 3-5 are cross-sectional views of the bullet 100 taken along lines 3-3, 4-4 and 5-5 of FIG. 1, respectively, and like reference numbers refer to like components in FIGS. 1-5. The body 105 has a wall thickness T1 at the line 3-3 shown in FIG. 1. The relatively large opening 215 (FIG. 2A) and the relatively thin wall thickness T1 enable the bullet to initiate petaling along the skives 250 (FIG. 2A) at lower velocities and/or in softer targets than conventionally shaped lead-free bullets. The body 105 also has progressively larger wall thicknesses T2 (FIG. 4) and T3 (FIG. 5) toward the tail. The larger wall thickness at lines 4-4 and 5-5 prevent, or at least inhibit, the petals from separating from the body 105 at high velocity impacts. Additionally, it can be seen from contrasting FIGS. 3 and 4 that the forward sidewall 225 converges from the opening (not shown) to the first transition area (not shown) because the tip 110 in FIG. 4 has a smaller cross-section than the tip 110 in FIG. 3.
  • Several embodiments of the bullet provide adequate outward radial expansion at impact (i.e., petaling or mushrooming) without undue fragmentation (i.e., without completely separating the petals from the body). Referring again to FIGS. 2A and 2B, the opening 215 and forward sidewall 225 are configured to initiate petal formation when the bullet 100 impacts a target. More specifically, the large opening 215 and small wall thickness T1 enable the body 105 to readily tear at the skives 250 and cause the petals to unfold. The tip 110 can further enable mushrooming because the impact force drives the tip 110 into the cavity 220. One advantage of several embodiments of the bullet 100 is that the configuration of the opening 215, the forward sidewall 225 of the cavity 220, and outer surface of the nose section 120 operate together with the type of material of the body such that the bullet 100 can petal at impact velocities of approximately 1,800 feet per second. Another advantage of several embodiments of the bullet 100 is that it can petal upon impact without undue fragmentation at much higher impact velocities. For example, the increasing thickness of the forward sidewall 225 toward the transition zone and the relatively larger thickness of the rear sidewall 235 increase the strength of the petals toward the tail such that the bullet can mushroom at high-velocity impacts of approximately 3,200 feet per second without fragmenting the petals. Such a configuration can also prevent the bullet 100 from mushrooming prematurely in flight before impacting the desired target.
  • FIGS. 6A-6E are cross-sectional side views of stages of a method for manufacturing a bullet in accordance with an embodiment of the invention. In FIG. 6A, a slug of lead-free material is pressed into a die cavity (not shown) to form a generally cylindrical slug 600 having a first end portion 602 with a face 620 and a second end portion 610. FIG. 6B illustrates a stage at which an axial force (not shown) has been applied to the face 620 of the first end portion 602 to form the second end portion 610 into a tail portion 615. FIG. 6C illustrates a subsequent stage at which a punch (not shown) presses against the face 620 to further form the tail portion 615 and shape the slug 600 in another die cavity (not shown). In the embodiment shown in FIG. 6C, the punch forms a generally annular ring portion 625 and a recess 630 at the first end portion 602. In other embodiments, however, the punch of the stage shown in FIG. 6C may form a planar surface at the first end portion 602 without a ring portion or a recess. In FIG. 6D, the slug 600 has been formed into a body 601 having a first end portion 605 into which a first punch (not shown) has been driven to form a cavity 640 that includes a forward sidewall 635 extending rearward from the opening 630. As the first punch forms the cavity 640 in FIG. 6D, it finalizes the tail portion 615 in another die cavity (not shown). FIG. 6E illustrates the process after a second punch (not shown) has been applied to the first end portion 605 to further extend the cavity 640 to include a rear sidewall 645. The first and second punches can have conical shapes at different angles such that the forward sidewall 635 tapers at a first angle and the rear sidewall 645 tapers at a second angle different than the first angle. The cavity 640 can accordingly have a transition zone 650. The second punch can also have a spherical tip to form a semi-spherical end 660.
  • FIG. 7 is a side view and FIG. 8 is a top view of a bullet at a subsequent stage of an embodiment of a method. In FIG. 7, the ring portion 625 of FIG. 6E has been removed from the first end portion 605, but the nose section of the bullet has not yet been formed. The first end portion 605 has a portion 710 that will be formed into the nose section's forward terminus. FIGS. 7 and 8 together further illustrate the conical surfaces of the forward sidewall 635 and rear sidewall 645.
  • FIG. 9 is a side view and FIG. 10 is a top view of a bullet at a subsequent stage of an embodiment of the method for manufacturing a bullet. Like reference numbers refer to like components in FIGS. 7-10. In FIG. 9, a third punch (not shown) has been pressed into the cavity 640 to form longitudinal skives 905 in the forward sidewall 635 by driving the edges of a pyramidal punch (not shown) that has three or more triangular faces into the forward sidewall 635. The number of faces that a pyramidal punch has determines the number of skives. For example, a four-sided pyramidal punch has four edges that form four skives. In other embodiments, the skives 905 may be formed by engraving or etching the forward sidewall 635. The skives 905 reduce the structural integrity at specific sites around the body 601 to further enable the bullet to mushroom upon impacting a target. One advantage of forming the skives 905 with a pyramidal punch is that extensive working of the body 601 is not required, and thus the risk of any fragmentation of the bullet that may occur is lessened vis-à-vis other techniques.
  • FIG. 11 is an enlarged isometric view of a subsequent stage of a method for manufacturing a bullet in accordance with an embodiment of the invention. At this stage, the body 601 has been contoured to form a nose section 1120. The nose section 1120 can be formed by inserting the body 601 into an ogive die cavity (not shown) and applying an axial force (not shown) to the bottom face of the tail section 615. At the completion of this stage, the nose section 1120 has an ogived outer surface 1125, a forward terminus 1130, and an opening 630 at the terminus 1130. The cavity 640 includes the forward sidewall 635 that converges rearward from the opening 630 and the rear sidewall 645 extending toward the tail at a different angle than the forward sidewall 635.
  • FIG. 12 is a cross-sectional view of a bullet in accordance with another embodiment, and like reference numbers refer to like components in FIGS. 1-2B and 12. In FIG. 12, at least a portion of the rear sidewall 1235 has a cylindrical surface rearward from the transition area 230. The cylindrical surface, for example, can extend from the transition zone to the beginning of the generally hemispherical cavity end 1265. The cross-sectional dimension 240 at the transition area 230 is the same as the cross-sectional dimension 240 at the generally hemispherical cavity end 1265.
  • From the foregoing, it will be appreciated that specific embodiments of the invention have been described herein for purposes of illustration, but that various modifications may be made without deviating from the spirit and scope of the invention. For example, the elements of one embodiment can be combined with other embodiments in addition to or in lieu of the elements of other embodiments. Accordingly, the invention is not limited except as by the appended claims.

Claims (29)

1. A bullet comprising a lead-free body having a tail section, a nose section having an ogived outer surface and a forward terminus, an opening at the forward terminus, the opening having a first-cross sectional dimension, and a cavity in the nose section extending rearward from the opening to an intermediate section of the body, wherein the cavity includes a forward sidewall that has at least a generally frusto-conical shape extending from the opening to a second cross-sectional dimension, the forward sidewall converging rearward from the first cross-sectional dimension to the second cross-sectional dimension, and a rear sidewall contiguous with the forward sidewall and extending directly from the second cross-sectional dimension to a third cross-sectional dimension, the rear sidewall diverging rearward from the second cross-sectional dimension to the third cross-sectional dimension.
2. The bullet of claim 1 wherein the body includes longitudinal skives in the forward sidewall.
3. (canceled)
4. The bullet of claim 1 wherein at least a portion of the rear sidewall converges to form a generally hemispherical end of the cavity.
5. The bullet of claim 1 wherein the lead-free body includes copper.
6. The bullet of claim 1 wherein the lead-free body includes a copper-zinc alloy.
7. The bullet of claim 1 wherein the lead-free body includes copper 210 alloy.
8. The bullet of claim 1 wherein the opening at the terminus is generally circular.
9. The bullet of claim 1, further comprising a separate polymeric tip in the opening projecting forward from the terminus.
10. The bullet of claim 1 wherein at least a portion of the cavity has an hourglass-shape.
11. A bullet comprising a lead-free body having a tail section, a nose section having an ogived outer surface and a forward terminus, an opening at the forward terminus, and a cavity in the nose section including a forward sidewall extending rearward convergently from the opening toward a transition area, the body having a first wall thickness at the transition area, skives in the forward sidewall, a rear sidewall contiguous with the forward sidewall and diverging rearward from the transition area, and a cavity end, the body having a second wall thickness at the cavity end, the second wall thickness greater than the first wall thickness, wherein the forward sidewall and the rear sidewall are configured to form petals upon impact in animal tissue that remain with the body at impact velocities of approximately 1,800 ft/sec to approximately 3,200 ft/sec.
12. (canceled)
13. The bullet of claim 11 wherein the transition area is a first transition area, the rear sidewall extends rearward divergently from the first transition area to a second transition area, and at least a portion of the rear sidewall extends rearward convergently to form a generally hemispherical end of the cavity.
14. The bullet of claim 12 wherein at least a portion of the rear sidewall is cylindrical rearward from the transition area.
15. The bullet of claim 11 wherein the lead-free body includes copper.
16. The bullet of claim 11 wherein the lead-free body includes a copper-zinc alloy.
17. The bullet of claim 11 wherein the lead-free body includes copper 210 alloy.
18. The bullet of claim 11, further comprising a tip in the opening projecting forward from the terminus.
19. The bullet of claim 11 wherein at least a portion of the cavity has an hourglass-shape.
20. A bullet comprising a lead-free body having a tail section, a nose section having an ogived outer surface and a forward terminus, an opening at the forward terminus, the opening having a first-cross sectional dimension, and a cavity in the nose section extending rearward from the opening to an intermediate section of the body, wherein:
the cavity includes a forward sidewall having at least a generally frusto-conical shape extending from the opening to a second cross-sectional dimension, the forward sidewall converging rearward from the first cross-sectional dimension to the second cross-sectional dimension, and a rear sidewall extending directly from the second cross-sectional dimension to a third cross-sectional dimension, the rear sidewall diverging rearward from the second cross-sectional dimension to the third cross-sectional dimension;
the body has a maximum cross-sectional dimension, and the ratio of the first cross-sectional dimension to the maximum cross-sectional dimension is approximately 0.30 to approximately 0.40;
the body has a length and the ratio of the distance of the second cross-sectional dimension rearward of the forward terminus to the body length is approximately 0.20 to approximately 0.25; and
the ratio of the second cross-sectional dimension to the maximum cross-sectional dimension is approximately 0.15 to approximately 0.25.
21. The bullet of claim 20 wherein:
the rear sidewall converges from the second transition area to form a generally hemispherical end of the cavity; and
the ratio of the distance of the third cross-sectional dimension rearward of the forward terminus to the body length is approximately 0.30 to approximately 0.35, and the ratio of the distance of the generally hemispherical end location rearward of the forward terminus to the body length is approximately 0.45 to approximately 0.50.
22. The bullet of claim 21 wherein:
the ratio of the third cross-sectional dimension to the maximum cross-sectional dimension is approximately 0.20 to approximately 0.30; and
the generally hemispherical end of the cavity has a fourth cross-sectional dimension and the ratio of the fourth cross-sectional dimension to the maximum cross-sectional dimension is approximately 0.10 to approximately 0.20.
23. The bullet of claim 20 wherein the body includes copper.
24. The bullet of claim 20 wherein the body includes a copper-zinc alloy.
25. The bullet of claim 20 wherein the body includes copper 210 alloy.
26. The bullet of claim 20 further comprising a tip in the opening that extends forwardly from the terminus.
27-36. (canceled)
37. The bullet of claim 1 wherein the body further comprises a cavity end having a fourth cross-sectional dimension, and wherein the body has a first wall thickness at the second cross-sectional dimension and a second wall thickness at the fourth cross-sectional dimension, the second wall thickness greater than the first wall thickness.
38. The bullet of claim 11 wherein the transition area is a first transition area, and wherein the rear sidewall diverges rearward from the first transition area to a second transition area and converges rearward from the second transition area to the cavity end.
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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140318405A1 (en) * 2011-08-08 2014-10-30 Ruag Ammotec Gmbh Structuring of the ogive surface of a projectile
WO2015118173A1 (en) * 2014-02-10 2015-08-13 Ruag Ammotec Gmbh Pb-free deforming/partially fragmenting projectile with a defined mushrooming and fragmenting behavior
US20160025469A1 (en) * 2013-03-08 2016-01-28 Vesa NURMINEN Bullet and method for expanding a bullet
WO2016025838A3 (en) * 2014-08-14 2016-04-14 OATH Corporation Fracturing and materials based impact reactive projectiles
US9354027B2 (en) * 2013-10-24 2016-05-31 G2 Research Inc. Fragmenting projectile
US9797696B2 (en) 2014-08-14 2017-10-24 OATH Corporation Conic taper tip fracturing projectiles
US20180106581A1 (en) * 2016-10-13 2018-04-19 G2 Research Inc. Predictably Fragmenting Projectiles Having Internally-Arranged Geometric Features
WO2018090025A1 (en) * 2016-11-14 2018-05-17 Agazim Eric Frangible bullet tip with fluted sides
US10101137B2 (en) * 2017-01-12 2018-10-16 Sig Sauer, Inc. Heat-mitigating nose insert for a projectile and a projectile containing the same
US10119797B2 (en) * 2017-02-27 2018-11-06 Sig Sauer, Inc. Cap-based heat-mitigating nose insert for a projectile and a projectile containing the same
US10312065B2 (en) 2016-07-20 2019-06-04 Applied Materials, Inc. Physical vapor deposition (PVD) plasma energy control per dynamic magnetron control
WO2019126830A1 (en) * 2017-12-22 2019-06-27 Olin Corporation Bullets and methods of making bullets
US10352669B2 (en) * 2016-09-30 2019-07-16 Badlands Precision LLC Advanced aerodynamic projectile and method of making same
US10495427B2 (en) * 2018-04-11 2019-12-03 Hornady Manufacturing Company Subsonic expanding bullet
US20200094319A1 (en) * 2018-09-26 2020-03-26 Environ-Metal, Inc. Die assemblies for forming a firearm projectile, methods of utilizing the die assemblies, and firearm projectiles
US10690464B2 (en) 2017-04-28 2020-06-23 Vista Outdoor Operations Llc Cartridge with combined effects projectile
CN111595208A (en) * 2020-06-24 2020-08-28 湖南天合终极防务科技实业有限公司 High-precision bullet
WO2020249788A1 (en) * 2019-06-13 2020-12-17 Ruag Ammotec Gmbh Projectile, in particular deformation and/or partial fragmentation projectile, and method for producing a projectile
WO2021170899A1 (en) * 2020-02-28 2021-09-02 Sako Oy Bullet
US11313657B1 (en) 2016-11-14 2022-04-26 Erik Agazim Multi-piece projectile with an insert formed via a powder metallurgy process
US11428517B2 (en) 2019-09-20 2022-08-30 Npee L.C. Projectile with insert
WO2023161400A1 (en) * 2022-02-25 2023-08-31 Swissp Defence Ag Intermediate, tool and method for producing a deformation projectile with defined terminal ballistics

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD733836S1 (en) 2011-07-26 2015-07-07 Ra Brands, L.L.C. Firearm bullet
USD735289S1 (en) 2011-07-26 2015-07-28 R.A. Brands, L.L.C. Firearm bullet
USD734419S1 (en) 2011-07-26 2015-07-14 Ra Brands, L.L.C. Firearm bullet
US8950333B2 (en) 2011-07-26 2015-02-10 Ra Brands, L.L.C. Multi-component bullet with core retention feature and method of manufacturing the bullet
USD733837S1 (en) 2011-07-26 2015-07-07 Ra Brands, L.L.C. Firearm bullet
USD733252S1 (en) 2011-07-26 2015-06-30 Ra Brands, L.L.C. Firearm bullet and portion of firearm cartridge
USD733834S1 (en) 2011-07-26 2015-07-07 Ra Brands, L.L.C. Firearm bullet
USD733835S1 (en) 2011-07-26 2015-07-07 Ra Brands, L.L.C. Firearm bullet
US9534876B2 (en) 2013-05-28 2017-01-03 Ra Brands, L.L.C. Projectile and mold to cast projectile
US8893621B1 (en) 2013-12-07 2014-11-25 Rolando Escobar Projectile
EP3628960A1 (en) 2014-04-30 2020-04-01 G9 Holdings, LLC Projectile with enhanced ballistics
DE102014224715B4 (en) * 2014-10-29 2019-07-11 Metallwerk Elisenhütte GmbH Unterschallpatrone with a projectile as well as projectile for such a
US10041773B2 (en) 2015-10-14 2018-08-07 Vista Outdoor Operations Llc Projectiles with insert-molded polymer tips
US10001355B2 (en) 2015-10-21 2018-06-19 Vista Outdoor Operations Llc Reduced drag projectiles
US10684108B2 (en) 2015-10-21 2020-06-16 Vista Outdoor Operations Llc Reduced drag projectiles
US10036619B2 (en) * 2016-01-11 2018-07-31 Lehigh Defense, LLC Armor-piercing cavitation projectile
US10222187B2 (en) * 2016-07-11 2019-03-05 Vista Outdoor Operations Llc Hunting projectile
WO2018136338A2 (en) 2017-01-12 2018-07-26 Vista Outdoor Operations Llc Projectile with tip for fluid based expansion at lower velocities
US10823539B1 (en) * 2017-11-14 2020-11-03 Sme Engineering (Pty) Ltd Expanding subsonic bullet
US10969209B2 (en) * 2018-02-14 2021-04-06 Olin Corporation Segmenting pistol bullet
WO2019236704A1 (en) 2018-06-05 2019-12-12 Norris Wayne Projectile having adaptive expansion characteristics
US11408717B2 (en) 2020-04-29 2022-08-09 Barnes Bullets, Llc Low drag, high density core projectile

Family Cites Families (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1493614A (en) * 1920-09-01 1924-05-13 Remington Arms Co Inc Mushroom bullet
US4044685A (en) 1971-06-18 1977-08-30 Hirtenberger Patronen-, Zundhutchen- Und Metallwarenfabrik Aktiengesellschaft Jacketless hunting bullet with roll-back cutting flags
US3972286A (en) 1972-03-23 1976-08-03 Canon Jack Y Bullet
EP0015574B1 (en) * 1979-03-10 1983-09-14 Hans-Ludwig Schirneker Projectile, e.g. for hunting, and method of manufacturing same
US4385545A (en) 1981-09-08 1983-05-31 Duer Morris J Reloading device for metallic firearm cartridges
US4385546A (en) 1981-10-13 1983-05-31 Lee Richard J Cartridge reloading dies
US4829904A (en) 1983-06-22 1989-05-16 Branscomb Corporation N. V. Ammunition round
AU578029B2 (en) 1983-06-22 1988-10-13 Branscomb Corporation N.V. Ammunition round
DE3510343A1 (en) 1985-03-22 1986-09-25 Hans-Ludwig 4773 Möhnesee Schirneker LEAD-FREE HUNTING BULLET
US4619203A (en) 1985-04-26 1986-10-28 Olin Corporation Armor piercing small caliber projectile
US4811666A (en) 1988-01-04 1989-03-14 Lutfy Eric A Solid projectiles
US4777883A (en) 1988-01-19 1988-10-18 Chovich Milija M Bullet
US4856160A (en) 1988-02-16 1989-08-15 Olin Corporation Bullet with reverse taper interlock jacket and method of manufacturing the bullet
BE1001874A3 (en) 1988-12-05 1990-04-03 Nationale Herstal Fn Sa Fab Powerful shot.
US5131123A (en) 1989-06-29 1992-07-21 Barnes Bullets, Inc. Methods of manufacturing a bullet
US5259320A (en) 1989-06-29 1993-11-09 Barnes Bullets, Inc. Intermediate article used to form a bullet projectile or component and a finally formed bullet
AU8751191A (en) 1990-08-23 1992-03-17 International Shooter Development Fund, Inc. Match-grade rifle cartridge with improved components
US5097767A (en) 1990-10-22 1992-03-24 James Cirillo Cartridge guide nose
DE69117191T2 (en) 1990-10-31 1996-09-05 John E Brown MAKE IT LEAD-FREE BULLETS AND CARTRIDGES
US5187325A (en) 1991-08-15 1993-02-16 Garvison Geary L Cylindrical bullet
US5127332A (en) 1991-10-07 1992-07-07 Olin Corporation Hunting bullet with reduced environmental lead exposure
US5214238A (en) 1992-03-23 1993-05-25 Christopher Young Sabot for chambering conventional bullets in a shotgun
US5877437A (en) 1992-04-29 1999-03-02 Oltrogge; Victor C. High density projectile
US5317109A (en) 1992-06-19 1994-05-31 Champlain Cable Corporation Conductive polymer cable assembly
US5686693A (en) 1992-06-25 1997-11-11 Jakobsson; Bo Soft steel projectile
US5399187A (en) 1993-09-23 1995-03-21 Olin Corporation Lead-free bullett
US5616642A (en) 1995-04-14 1997-04-01 West; Harley L. Lead-free frangible ammunition
AUPN426595A0 (en) 1995-07-19 1995-10-05 O'dwyer, James Michael Firearms
GB9607022D0 (en) 1996-04-03 1996-06-05 Cesaroni Tech Inc Bullet
US6074454A (en) 1996-07-11 2000-06-13 Delta Frangible Ammunition, Llc Lead-free frangible bullets and process for making same
US6536352B1 (en) 1996-07-11 2003-03-25 Delta Frangible Ammunition, Llc Lead-free frangible bullets and process for making same
US5950064A (en) 1997-01-17 1999-09-07 Olin Corporation Lead-free shot formed by liquid phase bonding
US5811723A (en) 1997-06-05 1998-09-22 Remington Arms Company, Inc. Solid copper hollow point bullet
US6311623B1 (en) 1997-09-02 2001-11-06 Wenzel Zaruba Power-packed arrowhead
US6105506A (en) 1997-09-23 2000-08-22 Antonio C. Gangale Sabot slug for shotgun
US6085661A (en) 1997-10-06 2000-07-11 Olin Corporation Small caliber non-toxic penetrator projectile
US6016754A (en) 1997-12-18 2000-01-25 Olin Corporation Lead-free tin projectile
US6439125B1 (en) 1998-01-27 2002-08-27 Friedkin Companies, Inc. Bullet
DE19818411C2 (en) 1998-04-24 2002-04-18 Rheinmetall W & M Gmbh Swirl-stabilized projectile and method for its production
US6070532A (en) 1998-04-28 2000-06-06 Olin Corporation High accuracy projectile
US5894644A (en) 1998-06-05 1999-04-20 Olin Corporation Lead-free projectiles made by liquid metal infiltration
US6112669A (en) 1998-06-05 2000-09-05 Olin Corporation Projectiles made from tungsten and iron
US6530328B2 (en) 1999-02-24 2003-03-11 Federal Cartridge Company Captive soft-point bullet
US6240849B1 (en) 1999-06-10 2001-06-05 Christopher A. Holler Projectile with expanding members
US6240850B1 (en) 1999-06-14 2001-06-05 Christopher A. Holler Bullets for use in hitting targets at short range
US6244187B1 (en) * 1999-07-01 2001-06-12 Federal Cartridge Company Increased velocity-performance-range bullet
US20020157524A1 (en) 2000-01-28 2002-10-31 Tuftee Edward M. Adaptor assembly for converting a case sizing die assembly to a bullet seating die assembly
DE10010500A1 (en) * 2000-03-07 2001-09-13 Dynamit Nobel Ag Deforming bullet consists of a casing-less body and a hollow chamber extending into the tapered front part of the body centrally to the longitudinal axis of the bullet
US6600126B2 (en) 2000-03-16 2003-07-29 Ruag Components Shell with a shell body and a process for the preparation of radially protruding guiding means on a shell body
US6354890B2 (en) 2000-03-17 2002-03-12 Delphi Technologies, Inc. High current sleeve and post terminals
US20030005846A1 (en) 2001-07-06 2003-01-09 Peter Atwood Crimped-case cartridge
US6837165B2 (en) 2001-11-09 2005-01-04 Olin Corporation Bullet with spherical nose portion
DE10157563A1 (en) 2001-11-23 2003-06-12 Rheinmetall W & M Gmbh Full caliber floor
US6973879B1 (en) 2002-03-16 2005-12-13 Mcelroy Hugh Anthony Monolithic high incapacitation small arms projectile
US7036433B2 (en) 2002-03-20 2006-05-02 Beal Harold F Ammunition projectile having enhanced aerodynamic profile
EP1502074B1 (en) * 2002-04-30 2009-11-18 RUAG Ammotec GmbH Partial fragmentation and deformation bullets having an identical point of impact and proces for the manufacture of such a bullet
US7000547B2 (en) 2002-10-31 2006-02-21 Amick Darryl D Tungsten-containing firearm slug
US7059233B2 (en) 2002-10-31 2006-06-13 Amick Darryl D Tungsten-containing articles and methods for forming the same
DE10257590B4 (en) 2002-12-09 2005-03-24 Wilhelm Brenneke Gmbh & Co. Kg Rifle bullet for hunting purposes
FR2859523B1 (en) * 2003-09-10 2005-12-02 Jean Claude Sauvestre HUNTING BALL WITH REDUCED AERODYNAMIC TRAINING
US7143679B2 (en) 2004-02-10 2006-12-05 International Cartridge Corporation Cannelured frangible cartridge and method of canneluring a frangible projectible
US7150233B1 (en) 2004-04-26 2006-12-19 Olin Corporation Jacketed boat-tail bullet
US20060124022A1 (en) 2004-12-13 2006-06-15 Olin Corporation, A Corporation Of The State Of Virginia Firearm projectile with bonded rear core
US20060278114A1 (en) 2005-05-16 2006-12-14 Hornady Manufacturing Company Shotgun shell with slug
US20070089628A1 (en) 2005-10-20 2007-04-26 Elder Steven M Firearm ammunition having improved flight and impact characteristics

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Publication number Priority date Publication date Assignee Title
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US10312065B2 (en) 2016-07-20 2019-06-04 Applied Materials, Inc. Physical vapor deposition (PVD) plasma energy control per dynamic magnetron control
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US11307005B2 (en) 2016-10-13 2022-04-19 G2 Research Inc. Predictably fragmenting projectiles having internally-arranged geometric features
US11313657B1 (en) 2016-11-14 2022-04-26 Erik Agazim Multi-piece projectile with an insert formed via a powder metallurgy process
US11598617B2 (en) 2016-11-14 2023-03-07 Erik Agazim Multi-piece projectile with an insert formed via a powder metallurgy process
WO2018090025A1 (en) * 2016-11-14 2018-05-17 Agazim Eric Frangible bullet tip with fluted sides
US10101137B2 (en) * 2017-01-12 2018-10-16 Sig Sauer, Inc. Heat-mitigating nose insert for a projectile and a projectile containing the same
US10119797B2 (en) * 2017-02-27 2018-11-06 Sig Sauer, Inc. Cap-based heat-mitigating nose insert for a projectile and a projectile containing the same
US11226182B2 (en) 2017-04-28 2022-01-18 Vista Outdoor Operations Llc Cartridge with combined effects projectile
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US10495427B2 (en) * 2018-04-11 2019-12-03 Hornady Manufacturing Company Subsonic expanding bullet
US10900759B2 (en) * 2018-09-26 2021-01-26 Environ-Metal, Inc. Die assemblies for forming a firearm projectile, methods of utilizing the die assemblies, and firearm projectiles
US20200094319A1 (en) * 2018-09-26 2020-03-26 Environ-Metal, Inc. Die assemblies for forming a firearm projectile, methods of utilizing the die assemblies, and firearm projectiles
WO2020249788A1 (en) * 2019-06-13 2020-12-17 Ruag Ammotec Gmbh Projectile, in particular deformation and/or partial fragmentation projectile, and method for producing a projectile
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US11428517B2 (en) 2019-09-20 2022-08-30 Npee L.C. Projectile with insert
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