US2393648A - Projectile - Google Patents
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- Publication number
- US2393648A US2393648A US431708A US43170842A US2393648A US 2393648 A US2393648 A US 2393648A US 431708 A US431708 A US 431708A US 43170842 A US43170842 A US 43170842A US 2393648 A US2393648 A US 2393648A
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- United States
- Prior art keywords
- projectile
- hardness
- metal
- powdered
- nose
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002184 metal Substances 0.000 description 15
- 229910052751 metal Inorganic materials 0.000 description 15
- 239000000203 mixture Substances 0.000 description 14
- 239000000463 material Substances 0.000 description 10
- 238000000034 method Methods 0.000 description 9
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 6
- 230000035515 penetration Effects 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 239000012254 powdered material Substances 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000007779 soft material Substances 0.000 description 2
- 101710125089 Bindin Proteins 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000003610 charcoal Substances 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000012256 powdered iron Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
Definitions
- This invention relates to a projectile and more particularly to an improved form of armor piercing projectile and method of making the same.
- Figures 1, 2, and 3 are longitudinal sectional views of a projectile formed according to my invention and representing the products of the three principal steps of the method.
- Figures 4, 5, 6, 7 and 8 are longitudinal sectional views of a projectile produced according to modifications of the method.
- Figure 9 is a similar view of a modified form of projectile produced by a similar method.
- a die I having a shape complementary to that of the desired projectile and provided with a pair of cooperating punches 2 and 3.
- Mixtures of powdered alloys or of the relatively pure constituents of the alloys are added to the die in such a manner that they are arranged in layers or strata along planes perpendicular to the long axis of the bullet.
- the metal powders used are chosen for the characteristics which are to be desired in the projectile.
- the tip zone 4 may be of material on the order of a hard mineral carbide with a suitable binder metal, While the head zone 5 is of a material which on alloying will produce a characteristically hard steel, and the base zone 6 is of a material which will produce a less hard but characteristically tough steel.
- the powdered mixtures are then subjected to pressure, preferably from each end simultaneously, to obtain a body having sufiicient strength and cohesiveness to resist ordinary handling. To promote adhesion at this stage it may be necessary to add a bindin constituent to the original mixtures.
- the formed bullet may then be removed from the mold and subjected to a sintering process the details of which are determined in'a known manner by the materials being treated. Normally sintering will be done by radiated heat in closed boxes with sufiicient charcoal to combine with the oxygen of the air and form a reducin atmosphere.
- the finished bullet shown in Fig. 3 will be physically homogeneous and the physical properties of the various strata will be in accordance with the properties of the materials used therein; At the interfaces between the various strata there will be considerable difiusion and interalloying between the layers thus avoiding any abrupt changes in characteristics which might weaken the structure.
- each unit of the powdered composition has been introduced separately to the die and separately compressed.
- the shapes of the punch faces used in compressing each unit of the charges..may;be' variedias tions will be found in the fact that a composite structure may thus be produced in which each of the alloy compositions retains its own identity andits. own physical characteristics although asdesired to produce interfacial junctionsofiany desired section, those shown being merely illustrative of some of the possible variations.
- the modified form of projectile shown-inFig. 9 is of a type which would be particularly useful as an unjacketed-projectile and is provided with a soft nose ll] of powdered iron or other relatively soft material which on 'impact', serves to assist in penetration by lessening the tendency to rico cartend by supporting and lubricating the body during penetration.
- a soft nose ll of powdered iron or other relatively soft material which on 'impact', serves to assist in penetration by lessening the tendency to rico cartend by supporting and lubricating the body during penetration.
- These functions are fulfilled in conventional. construction bymeans of a jacket and point filler or by soft capswelded, brazed, soldered, or mechanically secured to the projectile body.
- Such a'projectile might be provided with a rotating band or other conventional rifling engaging, means.
- a projectile body may be thus formed in any desired shape suitable for use directly or as a core for the conventional jacketed projectiles.
- titles of powdered materials may be charged into thedies results in elimination of wastage of materials.
- In the typical projectile cores used at present ahigh percentage of metal is lost in turning the body in automatic screw machines from 'bar. stock.
- Such elimination of wastage results in increased economy of critical metals and the method is also economical in that a pressure molding operation replaces precision, machining from bar steel.
- 1.'A- homogeneous projectilebody comprising heat treated. stratified mixtures of compressed powdered metallic products, the noseof'said body being relatively soft, the portion of said body adjacent the nose being of great hardness, and the remainder of said body being decrementally hard and incrementally tough and formed from a plural number of compositions, one of which is a heat treated ferrous metal of a high hardness and another of which is a heat treated ferrous metal of great toughness.
- a homogeneous projectile body comprising a sintered composite structure of mixtures of compressed metallic powders, the nose of said body comprising a relatively soft material, an armor piercing portion comprising a mixture of a hard metal carbide and a binder metal in rear of said nose, and: a base portion comprising a material varying decrementally in hardness and incrementally in toughness from said armor piercing portion, said base portion being formed from .a plural number of compositions, one of which-is a heat treated ferrous metal of high hardness and another of which is a heat treated ferrous metal of great'toughness.
- a homogeneous projectile body comprising a nose portion of a; relatively soft metal, a hard armor piercing portion of amixture of metallic carbide and a binder metal behindsaid nose, and a-metallicbase portion varying decrementally in hardness and incrementally in toughness from said-armor piercing-portion, said metallic base portion being formed" from a plural number of compositions, one of which is'a heat treated ferrous metal of a high hardness and another of which is a heat treated ferrous metal of great toughness the portions of said projectile body being interfacially allowed with each other.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Powder Metallurgy (AREA)
Description
Jan. 29, 1946.
C. A. MARTIN PROJECTILE Filed Feb. 20, 1942 m 9 y M Patented Jan. 29, 1946 UNITED it STATES PATENT OFFICE 2,393,648 PROJEGTILE Carl A. Martin, Negaunee, Mich.
7 Application February 20, 1942, Serial No. 431,708 7 (01. 102-52) (Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) 3 Claims.
The invention described herein may be manufactured and used by or for the Government for governmental purposes. without the payment to me of any royalty thereon.
This invention relates to a projectile and more particularly to an improved form of armor piercing projectile and method of making the same.
Modern armor plates which have proven to have the greatest protective qualities are, as is well known, provided with an extremely hard face by any one of several processes. Examination of projectiles after impact with such facehardened plates seems to show that the resistance to penetration of such plates is due to the fact that on impact there is a tendency for the head of the projectile to be shattered or upset by the blow of impact, in the happening of either event losing its power of penetration. However, if the shape of the projectile can be maintained and the body thereof kept intact until the hardened surface of the plate has been destroyed, there will generally be no difliculty in penetrating the underlying layers of softer material.
Prior attempts to reach this end in practice have involved the provision of a projectile having a head portion of such great hardness as to shatter the face of the plate. Attempts have been made by the provision of soft nose caps in advance of the hardened head and by controlled local heat treatment of the body to further increase penetration. However, eiforts to control the zone hardness of armor piercing projectiles of small caliber have not been successful as the small size of these projectiles precludes any effective variation in the heat treatment which is applied to the various zones of the projectile.
It is therefore an object of this invention to produce an armor piercing projectile or core therefor which, even in the small and medium calibers, will have optimum physical characteristics in respect to hardness and strength of each increment.
It is a further object to provide a method of producing such projectiles which will relieve critical shortages of strategic materials and which will release machine tools, such as the automatic screw machines, for other essential employment.
It is a further object to improve the economy and efiiciency with which such projectiles may be produced.
The exact nature of the invention as well as other objects and advantages thereof will clearly appear from a description of a preferred embodiment as shown in the accompanying drawing in which:
Figures 1, 2, and 3 are longitudinal sectional views of a projectile formed according to my invention and representing the products of the three principal steps of the method.
Figures 4, 5, 6, 7 and 8 are longitudinal sectional views of a projectile produced according to modifications of the method.
Figure 9 is a similar view of a modified form of projectile produced by a similar method.
Referring to the drawing by characters of ref erence there is shown in Fig. 1 a die I having a shape complementary to that of the desired projectile and provided with a pair of cooperating punches 2 and 3. Mixtures of powdered alloys or of the relatively pure constituents of the alloys are added to the die in such a manner that they are arranged in layers or strata along planes perpendicular to the long axis of the bullet. The metal powders used are chosen for the characteristics which are to be desired in the projectile. For example the tip zone 4 may be of material on the order of a hard mineral carbide with a suitable binder metal, While the head zone 5 is of a material which on alloying will produce a characteristically hard steel, and the base zone 6 is of a material which will produce a less hard but characteristically tough steel. As indicated in Fig. 2 the powdered mixtures are then subjected to pressure, preferably from each end simultaneously, to obtain a body having sufiicient strength and cohesiveness to resist ordinary handling. To promote adhesion at this stage it may be necessary to add a bindin constituent to the original mixtures.
The formed bullet may then be removed from the mold and subjected to a sintering process the details of which are determined in'a known manner by the materials being treated. Normally sintering will be done by radiated heat in closed boxes with sufiicient charcoal to combine with the oxygen of the air and form a reducin atmosphere. The finished bullet shown in Fig. 3 will be physically homogeneous and the physical properties of the various strata will be in accordance with the properties of the materials used therein; At the interfaces between the various strata there will be considerable difiusion and interalloying between the layers thus avoiding any abrupt changes in characteristics which might weaken the structure.
The modifications shown in Figures 4 to 7 inclusive correspond to the step shown in Fig. 2, previously described. ,7 The modifications consist in variations in the method of charging the die for the molding operation. In the form shown in Fig. 4 the addition of the mixture comprising zone 4 was gradually stopped and at the same time the delivery of the powdered mixture comprising zone 5 was gradually increased. A similar procedure resulted in a similar blending or gradual transition between zones 5 and 6. By choice of the rates of addition of the powdered material it is possible to producea smooth variation in composition so that hardness may. be made to vary decrementally from the tip while the toughness of the metal varies incrementally.
' ..-may be desirable.
In the forms shown in Figs. 5 to 7 each unit of the powdered composition has been introduced separately to the die and separately compressed. The shapes of the punch faces used in compressing each unit of the charges..may;be' variedias tions will be found in the fact that a composite structure may thus be produced in which each of the alloy compositions retains its own identity andits. own physical characteristics although asdesired to produce interfacial junctionsofiany desired section, those shown being merely illustrative of some of the possible variations. In
this way it is possible to carry a'core. oftougher? the application of final pressure to form the pro- I jectile body ready for sintering.
The modified form of projectile shown-inFig. 9 is of a type which would be particularly useful as an unjacketed-projectile and is provided with a soft nose ll] of powdered iron or other relatively soft material which on 'impact', serves to assist in penetration by lessening the tendency to ricochetand by supporting and lubricating the body during penetration. These functions are fulfilled in conventional. construction bymeans of a jacket and point filler or by soft capswelded, brazed, soldered, or mechanically secured to the projectile body. Such a'projectile might be provided with a rotating band or other conventional rifling engaging, means.
It will be obvious that a projectile body may be thus formed in any desired shape suitable for use directly or as a core for the conventional jacketed projectiles. titles of powdered materials" may be charged into thedies results in elimination of wastage of materials. In the typical projectile cores used at present ahigh percentage of metal is lost in turning the body in automatic screw machines from 'bar. stock. Such elimination of wastage results in increased economy of critical metals and the method is also economical in that a pressure molding operation replaces precision, machining from bar steel.
It .is generally contemplated that the harder The fact that exact quan-.
sociated in a homogeneous body with materials of greatly differing characteristics.
vI-claim:
1.'A- homogeneous projectilebody comprising heat treated. stratified mixtures of compressed powdered metallic products, the noseof'said body being relatively soft, the portion of said body adjacent the nose being of great hardness, and the remainder of said body being decrementally hard and incrementally tough and formed from a plural number of compositions, one of which is a heat treated ferrous metal of a high hardness and another of which is a heat treated ferrous metal of great toughness.
2.. A homogeneous projectile body comprising a sintered composite structure of mixtures of compressed metallic powders, the nose of said body comprising a relatively soft material, an armor piercing portion comprising a mixture of a hard metal carbide and a binder metal in rear of said nose, and: a base portion comprising a material varying decrementally in hardness and incrementally in toughness from said armor piercing portion, said base portion being formed from .a plural number of compositions, one of which-is a heat treated ferrous metal of high hardness and another of which is a heat treated ferrous metal of great'toughness.
3. A homogeneous projectile body comprising a nose portion of a; relatively soft metal, a hard armor piercing portion of amixture of metallic carbide and a binder metal behindsaid nose, and a-metallicbase portion varying decrementally in hardness and incrementally in toughness from said-armor piercing-portion, said metallic base portion being formed" from a plural number of compositions, one of which is'a heat treated ferrous metal of a high hardness and another of which is a heat treated ferrous metal of great toughness the portions of said projectile body being interfacially allowed with each other.
CARL -A. MARTIN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US431708A US2393648A (en) | 1942-02-20 | 1942-02-20 | Projectile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US431708A US2393648A (en) | 1942-02-20 | 1942-02-20 | Projectile |
Publications (1)
Publication Number | Publication Date |
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US2393648A true US2393648A (en) | 1946-01-29 |
Family
ID=23713094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US431708A Expired - Lifetime US2393648A (en) | 1942-02-20 | 1942-02-20 | Projectile |
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US (1) | US2393648A (en) |
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2669930A (en) * | 1946-01-05 | 1954-02-23 | Remington Arms Co Inc | Sabot projectile |
US3203349A (en) * | 1962-09-18 | 1965-08-31 | Kohlswa Jernverks Ab | Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile |
EP0073385A1 (en) * | 1981-08-31 | 1983-03-09 | GTE Products Corporation | Multiple component penetrator projectile |
EP0111712A1 (en) * | 1982-11-18 | 1984-06-27 | Rheinmetall GmbH | Sub-calibre penetrator with a high length-to-diameter ratio |
EP0143775A2 (en) * | 1983-11-23 | 1985-06-05 | VOEST-ALPINE Aktiengesellschaft | Sub-calibre penetrator and method of making the same |
US4836108A (en) * | 1981-08-31 | 1989-06-06 | Gte Products Corporation | Material for multiple component penetrators and penetrators employing same |
US4869175A (en) * | 1985-01-25 | 1989-09-26 | Mcdougal John A | Impact structures |
US5069138A (en) * | 1989-01-02 | 1991-12-03 | Lars Ekbom | Armor-piercing projectile with spiculating core |
US5847313A (en) * | 1997-01-30 | 1998-12-08 | Cove Corporation | Projectile for ammunition cartridge |
US5877437A (en) * | 1992-04-29 | 1999-03-02 | Oltrogge; Victor C. | High density projectile |
US5936191A (en) * | 1996-05-14 | 1999-08-10 | Rheinmetall Industrie Ag | Subcaliber kinetic energy projectile |
WO2000055569A2 (en) | 1999-03-08 | 2000-09-21 | Beal Harold F | A multi-part projectile and method of making |
US6149705A (en) * | 1994-07-06 | 2000-11-21 | Ut-Battelle, Llc | Non-lead, environmentally safe projectiles and method of making same |
US6174494B1 (en) | 1993-07-06 | 2001-01-16 | Lockheed Martin Energy Systems, Inc. | Non-lead, environmentally safe projectiles and explosives containers |
WO2001055666A1 (en) * | 2000-01-26 | 2001-08-02 | Beal Harold F | Powder-based disc for gun ammunition |
WO2001069165A2 (en) * | 2000-03-08 | 2001-09-20 | Beal Harold F | A multi-part projectile and method of making |
WO2002090869A2 (en) * | 2001-04-30 | 2002-11-14 | Beal Harold F | Solid outer skin powder-base disc for projectiles |
WO2003002928A2 (en) * | 2001-05-15 | 2003-01-09 | Beal Harold F | Cap for an ammunition projectile and method |
US6551376B1 (en) | 1997-03-14 | 2003-04-22 | Doris Nebel Beal Inter Vivos Patent Trust | Method for developing and sustaining uniform distribution of a plurality of metal powders of different densities in a mixture of such metal powders |
US6581523B2 (en) * | 2000-01-26 | 2003-06-24 | Doris Nebel Beal Intervivos Patent Trust | Powder-based disc having solid outer skin for use in a multi-component ammunition projectile |
US6607692B2 (en) | 1997-01-30 | 2003-08-19 | Doris Nebel Beal Intervivos Patent Trust | Method of manufacture of a powder-based firearm ammunition projectile employing electrostatic charge |
WO2003073036A2 (en) * | 2002-02-26 | 2003-09-04 | Doris Nebel Beal Inter Vivos Patent Trust | Ammunition projectile including tapered powder-based core |
WO2003029746A3 (en) * | 2001-05-29 | 2004-04-15 | Olin Corp | Dual core ammunition |
US6845719B1 (en) * | 2003-06-05 | 2005-01-25 | Lockheed Martin Corporation | Erosion resistant projectile |
US20060196383A1 (en) * | 2003-09-27 | 2006-09-07 | Parker William P | Target assignment projectile |
US20070131132A1 (en) * | 2001-05-15 | 2007-06-14 | Doris Nebel Beal, Inter Vivos Patent Trust | Power-based core for ammunition projective |
US20100212535A1 (en) * | 2007-07-11 | 2010-08-26 | Beal Harold F | Traceable Frangible Projectile |
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 |
-
1942
- 1942-02-20 US US431708A patent/US2393648A/en not_active Expired - Lifetime
Cited By (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2669930A (en) * | 1946-01-05 | 1954-02-23 | Remington Arms Co Inc | Sabot projectile |
US3203349A (en) * | 1962-09-18 | 1965-08-31 | Kohlswa Jernverks Ab | Projectile or the like, preferably for armor-piercing weapons, and a method of manufacturing such a projectile |
EP0073385A1 (en) * | 1981-08-31 | 1983-03-09 | GTE Products Corporation | Multiple component penetrator projectile |
US4836108A (en) * | 1981-08-31 | 1989-06-06 | Gte Products Corporation | Material for multiple component penetrators and penetrators employing same |
EP0111712A1 (en) * | 1982-11-18 | 1984-06-27 | Rheinmetall GmbH | Sub-calibre penetrator with a high length-to-diameter ratio |
US4872409A (en) * | 1982-11-18 | 1989-10-10 | Rheinmetall Gmbh | Kinetic-energy projectile having a large length to diameter ratio |
EP0143775A2 (en) * | 1983-11-23 | 1985-06-05 | VOEST-ALPINE Aktiengesellschaft | Sub-calibre penetrator and method of making the same |
EP0143775A3 (en) * | 1983-11-23 | 1986-06-25 | Voest-Alpine Aktiengesellschaft | Sub-calibre penetrator and method of making the same |
US4665828A (en) * | 1983-11-23 | 1987-05-19 | Voest-Alpine Aktiengesellschaft | Penetrator for a driving-cage projectile and the process of manufacturing the same |
US4869175A (en) * | 1985-01-25 | 1989-09-26 | Mcdougal John A | Impact structures |
US5069138A (en) * | 1989-01-02 | 1991-12-03 | Lars Ekbom | Armor-piercing projectile with spiculating core |
US5877437A (en) * | 1992-04-29 | 1999-03-02 | Oltrogge; Victor C. | High density projectile |
US6174494B1 (en) | 1993-07-06 | 2001-01-16 | Lockheed Martin Energy Systems, Inc. | Non-lead, environmentally safe projectiles and explosives containers |
US6149705A (en) * | 1994-07-06 | 2000-11-21 | Ut-Battelle, Llc | Non-lead, environmentally safe projectiles and method of making same |
US5936191A (en) * | 1996-05-14 | 1999-08-10 | Rheinmetall Industrie Ag | Subcaliber kinetic energy projectile |
US6035501A (en) * | 1996-05-14 | 2000-03-14 | Rheinmetall W & M Gmbh | Method of making a subcaliber kinetic energy projectile |
US5847313A (en) * | 1997-01-30 | 1998-12-08 | Cove Corporation | Projectile for ammunition cartridge |
US6626114B2 (en) | 1997-01-30 | 2003-09-30 | Doris Nebel Beal Intervivos Patent Trust | Projectile having a disc and multiple cores |
US6607692B2 (en) | 1997-01-30 | 2003-08-19 | Doris Nebel Beal Intervivos Patent Trust | Method of manufacture of a powder-based firearm ammunition projectile employing electrostatic charge |
US6317946B1 (en) * | 1997-01-30 | 2001-11-20 | Harold F. Beal | Method for the manufacture of a multi-part projectile for gun ammunition and product produced thereby |
US6551376B1 (en) | 1997-03-14 | 2003-04-22 | Doris Nebel Beal Inter Vivos Patent Trust | Method for developing and sustaining uniform distribution of a plurality of metal powders of different densities in a mixture of such metal powders |
WO1999010702A3 (en) * | 1997-08-28 | 1999-05-06 | Cove Corp | Projectile for ammunition cartridge |
WO2000055569A2 (en) | 1999-03-08 | 2000-09-21 | Beal Harold F | A multi-part projectile and method of making |
WO2000055569A3 (en) * | 1999-03-08 | 2001-03-08 | Harold F Beal | A multi-part projectile and method of making |
US6371029B1 (en) * | 2000-01-26 | 2002-04-16 | Harold F. Beal | Powder-based disc for gun ammunition having a projectile which includes a frangible powder-based core disposed within a metallic jacket |
US6581523B2 (en) * | 2000-01-26 | 2003-06-24 | Doris Nebel Beal Intervivos Patent Trust | Powder-based disc having solid outer skin for use in a multi-component ammunition projectile |
WO2001055666A1 (en) * | 2000-01-26 | 2001-08-02 | Beal Harold F | Powder-based disc for gun ammunition |
WO2001069165A3 (en) * | 2000-03-08 | 2002-02-28 | Harold F Beal | A multi-part projectile and method of making |
WO2001069165A2 (en) * | 2000-03-08 | 2001-09-20 | Beal Harold F | A multi-part projectile and method of making |
WO2002090869A3 (en) * | 2001-04-30 | 2003-10-09 | Harold F Beal | Solid outer skin powder-base disc for projectiles |
WO2002090869A2 (en) * | 2001-04-30 | 2002-11-14 | Beal Harold F | Solid outer skin powder-base disc for projectiles |
WO2003002928A2 (en) * | 2001-05-15 | 2003-01-09 | Beal Harold F | Cap for an ammunition projectile and method |
WO2003002928A3 (en) * | 2001-05-15 | 2003-06-19 | Harold F Beal | Cap for an ammunition projectile and method |
US6591730B2 (en) * | 2001-05-15 | 2003-07-15 | Doris Nebel Beal Intervivos Patent Trust | Cap for a multi-component ammunition projectile and method |
US7243588B2 (en) | 2001-05-15 | 2007-07-17 | Doris Nebel Beal Inter Vivos Patent Trust | Power-based core for ammunition projective |
US20070131132A1 (en) * | 2001-05-15 | 2007-06-14 | Doris Nebel Beal, Inter Vivos Patent Trust | Power-based core for ammunition projective |
WO2003029746A3 (en) * | 2001-05-29 | 2004-04-15 | Olin Corp | Dual core ammunition |
US20030221580A1 (en) * | 2002-02-26 | 2003-12-04 | Beal Harold F. | Tapered powder-based core for projectile |
US7069834B2 (en) * | 2002-02-26 | 2006-07-04 | Doris Nebel Beal Inter Vivos Patent Trust | Tapered powder-based core for projectile |
WO2003073036A3 (en) * | 2002-02-26 | 2004-02-19 | Doris Nebel Beal Inter Vivos P | Ammunition projectile including tapered powder-based core |
WO2003073036A2 (en) * | 2002-02-26 | 2003-09-04 | Doris Nebel Beal Inter Vivos Patent Trust | Ammunition projectile including tapered powder-based core |
US6845719B1 (en) * | 2003-06-05 | 2005-01-25 | Lockheed Martin Corporation | Erosion resistant projectile |
US20060196383A1 (en) * | 2003-09-27 | 2006-09-07 | Parker William P | Target assignment projectile |
US9638501B2 (en) * | 2003-09-27 | 2017-05-02 | William P. Parker | Target assignment projectile |
US20100212535A1 (en) * | 2007-07-11 | 2010-08-26 | Beal Harold F | Traceable Frangible Projectile |
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 |
WO2020068937A1 (en) * | 2018-09-26 | 2020-04-02 | Environ-Metal, Inc. | Die assemblies for forming a firearm projectile, methods of utilizing the die assemblies, and firearm projectiles |
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 |
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