US2409307A - Projectile - Google Patents
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- US2409307A US2409307A US449280A US44928042A US2409307A US 2409307 A US2409307 A US 2409307A US 449280 A US449280 A US 449280A US 44928042 A US44928042 A US 44928042A US 2409307 A US2409307 A US 2409307A
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- United States
- Prior art keywords
- bullet
- iron
- lead
- projectile
- metal
- Prior art date
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 65
- 229910052751 metal Inorganic materials 0.000 description 36
- 239000002184 metal Substances 0.000 description 36
- 229910052742 iron Inorganic materials 0.000 description 24
- 239000011148 porous material Substances 0.000 description 10
- 238000005470 impregnation Methods 0.000 description 9
- 229910000831 Steel Inorganic materials 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 239000000463 material Substances 0.000 description 7
- 238000000034 method Methods 0.000 description 7
- 239000000843 powder Substances 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 5
- 239000007787 solid Substances 0.000 description 5
- 239000004484 Briquette Substances 0.000 description 4
- 229910000978 Pb alloy Inorganic materials 0.000 description 4
- 239000007769 metal material Substances 0.000 description 4
- 238000005245 sintering Methods 0.000 description 4
- 229910001369 Brass Inorganic materials 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- 239000010951 brass Substances 0.000 description 3
- 239000002360 explosive Substances 0.000 description 3
- 229910001385 heavy metal Inorganic materials 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 238000009736 wetting Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- 238000006066 Comins reaction Methods 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000004320 controlled atmosphere Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000011344 liquid material Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/74—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/12028—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, etc.]
- Y10T428/12063—Nonparticulate metal component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/1216—Continuous interengaged phases of plural metals, or oriented fiber containing
Definitions
- This invention relates to porous metal and is particularly concerned with porous metal projectiles and the like.
- Anobject of the invention is to provide a projectile part such as a bullet or bullet core which is made from molded and sintered metal powder that has been impregnated with another material to raise the apparent density thereof.
- a still further object of the invention is to provide a porous iron projectile part which has the pores thereof substantially filled with a metal, such as lead or lead alloy, which has a greater density than iron whereby the apparent density of the entire part is appreciably increased.
- Another object of the invention is to provide a projectile part made from porous metal which has ballistic performance comparable to a solid metal.
- a further object of the invention is to provide a method for controlling the apparent density of porous metal parts by impregnation of said parts with another metal whereby the apparent density may be controlled by controlling the porosity of the porous metal part thereby controlling its absorbing capacity toward the impregnant,
- a still further object is to provide a bullet and method for making same wherein the bullet has a relatively soft exterior surface and a relatively harder interior surface whereby the exterior surface thereof will not injure the rifling in the gun and the harder interior will act an as armor piercing portion.
- Another object of the invention is to provide a bullet made from iron powder which is preferably impregnated with a soft metal, such as lead, and which has a nose portion thereon of a hard metal which in some cases is a solid metal bonded to the remainder of the bullet.
- FIG. 1 is a sectional view of a cartridge
- Fig. 2 is a fragmentary enlarged sectional view of an incendiary and/r explosive cartridge
- Fig. 3 is a diagrammatic sectional view taken on line 3-3 of Fig. 1 showing on a greatly enlarged scale the metallurgical structure of the bullet;
- Fig. 4 is a view of the bullet made from iron powder impregnated with lead or the like which includes a jacket thereover made from brass or other easily formable metal;
- Fig. 5 is a fragmentary view of a nose portion of the bullet wherein the piercing nose of the bullet comprises a solid metal or extremely hard metal portion keyed and bonded to the remainder of the bullet which is made from iron powder.
- Projectile parts in general such as bullets, bullet cores and the like are usually made from steel or lead.
- the steel bullet has great strength as oocasioned by the physical characteristics of the steel, and lead bullets due to their great weight have a tremendous inertia force.
- machine gun bullets and rifle bullets for army purposes have been made from steel parts made on a screw machine.
- porous metal bullets made from metal powders were contemplated, such bullets being formed from iron powder, for example, pressed to shape and sintered 'under suitable conditions of time, temperature and atmosphere to form a porous bullet having an apparent density somewhat less than iron.
- the apparent density of the average porous iron bullet is usually above .6 of the density of iron.
- Porous metal bullets are suiilciently strong for use in machine guns and rifles but ballistically are not as suitable as solid metal bullets or projectile parts due to their lower density.
- Projectile parts of this character are highly desirable from every standpoint since they'have the necessary strength due to the strong framework of porous iron and likewise they have greater weight, due to the high density of lead. For this reason, a lead impregnated porous iron bullet is more desirable in use than either a lead bullet or a steel bullet since it combines the most desirable features of both of these prior typesof projectiles.
- a bullet from other metal powders, if desired, for example, bronze powders, nickel and copper powder, iron and copper powder and the like may be used in accordance with themanufacturers desires.- These pl-11f lets may then be impregnated with a heavy metal, preferably lead. In some cases, however, impregnation with other materials may be desirable; this is especially true Where the apparent density of the bullet material does not necessarily have to be as great as the density of conventional metals and where it is desirable to close the pores of the bullet. In this instance, the bullets may be impregnated with thermosetting resins, non-metallic materials in the molten state, etc., such variations coming within the scope or our invention.
- the sintered iron is generally sufficiently soft so as not to injure the rifling of the guns.
- the rifiing can cut in the leaded iron surface of the bullet and give a twist to the bullet during the passage of the bullet through the bore of the gun.
- carbon may be incorporated in the iron powder and the bullet may be decarburized at the surface thereof to form a relatively softer surface while the remainder of the bullet remains carburized and hard. This may be accomplished while sintering by using an atmosphere with suflicient water vapor present to decarburize the surface but controlledso as to prevent oxidation of the iron.
- FIG. 5 Another embodiment of the invention is shown in Fig. 5 wherein a solid nose portion 42 including a. key' l3 is placed in the die and iron powder is thenbriquetted thereon to form the remainder of the bullet as at 44. The assembly is next sintered for causing the iron powder to form a strong porous structur which is.bonded to the noseportion 42. The iron portion of the bullet may then be impregnated with lead or other metal as desired.
- the nose portionAZ in this embodiment may be a hardened steel or may be formed in some cases from metal, powders. such as tungsten carbide.
- the briquetting operation may be simultaneous for both portions of the .bulletor may be carried out in. two steps, as desired, the simultaneous operation being preferred.
- .A bullet made in this manner may be sintered in a single operation since the temperatures involved are similar for both types of metal powders.
- the impregnation of porous parts may b carried out by conventional methods such as immersing th part in a liquid or molten material, and then removing it therefrom.
- metallic material i utilized it may be heated until molten or if non-metallics are used, such as resins, they may be either heated to a molten state or dissolved in a solvent.
- the 'soIvent must be evaporated, either by air drying or heating.
- FIG. 1 shows two specific: embodiments of the invention wherein a cartridge-20 is shown-in Fig. 1 including a bullet. or projectile part 22*held in a shell 24.
- the bullet 22 is made under the teachings of this invention.
- Fig. 2 is an enlarged view of an incendiary and/or explosive cartridge 26 which includes a shell 28 and a bullet. 30, which has a bullet core 32 therein which includes a bore 34 that may be filled with an incendiary or explosive charge.
- Fig. 3 is a diagrammatic crosssectional view of this material in these bullet parts wherein the dark areas 38" indicate iron and the lighter areas 38 indicate the impregnated material.
- Iron powder preferably made from reduced oxide or'comminuted iron particles and having a mesh size smaller than 100, is briquetted to the desired shape at pressures ranging from 20,000 to 70,000 pounds per square inch and preferably at 45,000 pounds persquare inch.
- the part when removed from the briquetting die is self-sustain ingand of the size and shape desired.
- This part is then sintered under non-oxidizing conditions at a temperature of between 2,000 and 2,050 F., for a period of about a half hour whereupon it is cooled under a non-oxidizing condition.
- the part is next immersed in molten lead maintained at a temperature above the melting point of lead and preferably at 1,700 F. where it remains for a period of about ten .minutes.
- the part is then removed and allowed to cool; upon cooling the lead contracts slightly so that there, is little if any excess lead on the external surface of the bullet.
- a part made in this manner will have an apparent density in the order of 7.8, which is the density of
- a sizing step may be resorted to after the sintering steps if the parts are ,not exactsize. However, this is unnecessary in most instances and depends upon control conditions Since it is apparent that by varying the briquetting pressure and sintering temperatures andv the like that slight variations in the finished size of the sintered briquette may be obtained.
- a wetting metal to the lead.
- One of such metals is tin in quantities up to 10%. In this instance, the
- Alloys of lead may also be used where appreciable quantities of tin. antimony and the like are present or these other metals may be used in the substantially pure state.
- a projectile made from sintered briquetted iron powder which is coated over with and has the pores substantially filled with a metal softer than and heavier than iron and impregnated therein, whereby the said projectile has a relatively soft surface thereover and an apparent density greater than a sintered iron briquette.
- a projectile made from sintered briquetted iron powder having an apparent density in excess of 60% of the density of iron, said projectile being coated over with and having the pores substantially filled with lead which is impregnated therein, whereby said projectile has a soft surface thereover.
- a projegtile made from sintered briquetted iron powder and having an apparent density in excess of 60% of the density of iron, said projectile being coated over with and having the pores substantially filled with a lead alloy which is impregnated therein, whereby the said projectile has a soft surface thereover.
- a projectile made of two portions, including a nose portion formed from a relatively hard metallic material and a body portion formed from sinter d briquetted iron powder, said body portion being metallurgically bonded to said nose portion, said body portion of the projectile being coated over with and having the pores filled with a lead base alloy for producing a relatively soft surface thereover and for increasing the weight of the projectile.
- a projectile made of two portions, including a nose portion formed from a relatively hard metallic material and a body portion formed from sintered briquetted iron powder, said body portion being metallurgically bonded to said nose portion, said body portion of the projectile being coated over with and having the pores filled with lead for producing a relatively soft surface thereover and for increasing the weight of the projectile.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Oct. 15, 1946- E. s. PATCH ET AL PROJEC'IILE Filed July 1, 1942 6. 2 3. 0 N H E M m 7 S L B m WE m I m r 5.
Patented Oct. 15, 1946 raomc'rmn Earl S. Patch, Dayton, Ohio, and Wiley T. Moore,
Washington, D. C., assignors to General Motors Corporation, Detroit, Mich., a corporation of Delaware Application July 1, 1942, Serial No. 449,280
5 Claims. (Cl. 102- 925) This invention relates to porous metal and is particularly concerned with porous metal projectiles and the like.
Anobject of the invention is to provide a projectile part such as a bullet or bullet core which is made from molded and sintered metal powder that has been impregnated with another material to raise the apparent density thereof.
In carrying out the above object, it is a further object of the invention to impregnate the pores of said porous metal part with a heavy metal for increasing the apparent density of the part.
A still further object of the invention is to provide a porous iron projectile part which has the pores thereof substantially filled with a metal, such as lead or lead alloy, which has a greater density than iron whereby the apparent density of the entire part is appreciably increased.
Another object of the invention is to provide a projectile part made from porous metal which has ballistic performance comparable to a solid metal.
A further object of the invention is to providea method for controlling the apparent density of porous metal parts by impregnation of said parts with another metal whereby the apparent density may be controlled by controlling the porosity of the porous metal part thereby controlling its absorbing capacity toward the impregnant,
A still further object is to provide a bullet and method for making same wherein the bullet has a relatively soft exterior surface and a relatively harder interior surface whereby the exterior surface thereof will not injure the rifling in the gun and the harder interior will act an as armor piercing portion.
Another object of the invention is to provide a bullet made from iron powder which is preferably impregnated with a soft metal, such as lead, and which has a nose portion thereon of a hard metal which in some cases is a solid metal bonded to the remainder of the bullet.
Further objects and advantages of the present invention will be apparent from the following description, reference being had to the accompanying drawings wherein a preferred embodiment of the present invention is clearly shown.
In the drawing Fig. 1 is a sectional view of a cartridge;
Fig. 2 is a fragmentary enlarged sectional view of an incendiary and/r explosive cartridge;
Fig. 3 is a diagrammatic sectional view taken on line 3-3 of Fig. 1 showing on a greatly enlarged scale the metallurgical structure of the bullet;
Fig. 4 is a view of the bullet made from iron powder impregnated with lead or the like which includes a jacket thereover made from brass or other easily formable metal; and
Fig. 5 is a fragmentary view of a nose portion of the bullet wherein the piercing nose of the bullet comprises a solid metal or extremely hard metal portion keyed and bonded to the remainder of the bullet which is made from iron powder.
Projectile parts in general, such as bullets, bullet cores and the like are usually made from steel or lead. Each of these materials has its advantages. The steel bullet has great strength as oocasioned by the physical characteristics of the steel, and lead bullets due to their great weight have a tremendous inertia force. Heretofore, machine gun bullets and rifle bullets for army purposes have been made from steel parts made on a screw machine. In view of war-time conditions it is desirable to relieve the load on screw machines and, therefore, porous metal bullets made from metal powders were contemplated, such bullets being formed from iron powder, for example, pressed to shape and sintered 'under suitable conditions of time, temperature and atmosphere to form a porous bullet having an apparent density somewhat less than iron. For example. the apparent density of the average porous iron bullet is usually above .6 of the density of iron.
Porous metal bullets are suiilciently strong for use in machine guns and rifles but ballistically are not as suitable as solid metal bullets or projectile parts due to their lower density. To improve the ballistic performance of these parts, we impregnate them with another metal preferably lead or lead alloy which substantially fills the pores thereof and yields an apparent density greater than that of porous iron and variable according to control conditions. Projectile parts of this character are highly desirable from every standpoint since they'have the necessary strength due to the strong framework of porous iron and likewise they have greater weight, due to the high density of lead. For this reason, a lead impregnated porous iron bullet is more desirable in use than either a lead bullet or a steel bullet since it combines the most desirable features of both of these prior typesof projectiles.
It is also possible to form a bullet from other metal powders, if desired, for example, bronze powders, nickel and copper powder, iron and copper powder and the like may be used in accordance with themanufacturers desires.- These pl-11f lets may then be impregnated with a heavy metal, preferably lead. In some cases, however, impregnation with other materials may be desirable; this is especially true Where the apparent density of the bullet material does not necessarily have to be as great as the density of conventional metals and where it is desirable to close the pores of the bullet. In this instance, the bullets may be impregnated with thermosetting resins, non-metallic materials in the molten state, etc., such variations coming within the scope or our invention.
In the bullet material discussed herein the sintered iron is generally sufficiently soft so as not to injure the rifling of the guns. In other words, the rifiing can cut in the leaded iron surface of the bullet and give a twist to the bullet during the passage of the bullet through the bore of the gun. In some cases where a particularly hard bulletis desired carbon may be incorporated in the iron powder and the bullet may be decarburized at the surface thereof to form a relatively softer surface while the remainder of the bullet remains carburized and hard. This may be accomplished while sintering by using an atmosphere with suflicient water vapor present to decarburize the surface but controlledso as to prevent oxidation of the iron. This is in differentiation of th usual type of steel bullet which is jacketed with a soft metal such as brass to improve the action of rifling and also to prevent injury to the rifling at the bore of the gun. However, it is understood that in bullets made from iron powder which are preferably impregnated with a heavy metal, such as lead, and wherein the entire bullet is carburized' and tempered to a high degree of hardness, a jacket 40 may be provided as shown in Fig; 4, which completely covers the iron. In this case the iron powder is briquetted to a size slightly smaller than desired so that the covering of brass or other metal thereover brings the outer diameter of the bullet to that necessary for any particular gun bore.
' Another embodiment of the invention is shown in Fig. 5 wherein a solid nose portion 42 including a. key' l3 is placed in the die and iron powder is thenbriquetted thereon to form the remainder of the bullet as at 44. The assembly is next sintered for causing the iron powder to form a strong porous structur which is.bonded to the noseportion 42. The iron portion of the bullet may then be impregnated with lead or other metal as desired. v I
The nose portionAZ in this embodiment may be a hardened steel or may be formed in some cases from metal, powders. such as tungsten carbide.
mined amount of this powder to form the nose portion and then the remainder of the die is filled with a softer iron powder containing substantiallyno carbon. In this instance the briquetting operation may be simultaneous for both portions of the .bulletor may be carried out in. two steps, as desired, the simultaneous operation being preferred. .A bullet made in this manner may be sintered in a single operation since the temperatures involved are similar for both types of metal powders.
Methods for forming porous metal parts are disclosed in a number of patents and such methods form no part of the present invention. Reference may be made to the Lenel Patents Nos. 2,226,520 or 2,191,936, both of which disclose methods of making porous iron articles.
The impregnation of porous parts may b carried out by conventional methods such as immersing th part in a liquid or molten material, and then removing it therefrom. In this case, if metallic material i utilized it may be heated until molten or if non-metallics are used, such as resins, they may be either heated to a molten state or dissolved in a solvent. In this case, after impregnation the 'soIvent must be evaporated, either by air drying or heating. Also where finely porous materials are,to be impregnated, it is often desirable to evacuate the part prior to impregnation, thus expediting the impregnation thereof. We have found in most cases and in accordance with the example to be given hereinafter thatevacuation is unnecessary. However, where impregnation is found to be difiicult, it is to be understood that such a step may be carried out Within the scope of my invention. Another impregnating method which may be utilized is shown in Kurtz, Patent No. 2,192,792, wherein iron articles are simultaneously sintered and impregnated with lead.
The drawing showstwo specific: embodiments of the invention wherein a cartridge-20 is shown-in Fig. 1 including a bullet. or projectile part 22*held in a shell 24. The bullet 22 is made under the teachings of this invention. Fig. 2 is an enlarged view of an incendiary and/or explosive cartridge 26 which includes a shell 28 and a bullet. 30, which has a bullet core 32 therein which includes a bore 34 that may be filled with an incendiary or explosive charge. Fig. 3 is a diagrammatic crosssectional view of this material in these bullet parts wherein the dark areas 38" indicate iron and the lighter areas 38 indicate the impregnated material.
A specific example in the formation'of a pr'oiec tile part given for illustrative purpose only is as follows:
Iron powder, preferably made from reduced oxide or'comminuted iron particles and having a mesh size smaller than 100, is briquetted to the desired shape at pressures ranging from 20,000 to 70,000 pounds per square inch and preferably at 45,000 pounds persquare inch. The part when removed from the briquetting die is self-sustain ingand of the size and shape desired. This part is then sintered under non-oxidizing conditions at a temperature of between 2,000 and 2,050 F., for a period of about a half hour whereupon it is cooled under a non-oxidizing condition. The part is next immersed in molten lead maintained at a temperature above the melting point of lead and preferably at 1,700 F. where it remains for a period of about ten .minutes. The part is then removed and allowed to cool; upon cooling the lead contracts slightly so that there, is little if any excess lead on the external surface of the bullet. A part made in this manner will have an apparent density in the order of 7.8, which is the density of steel.
A sizing step may be resorted to after the sintering steps if the parts are ,not exactsize. However, this is unnecessary in most instances and depends upon control conditions Since it is apparent that by varying the briquetting pressure and sintering temperatures andv the like that slight variations in the finished size of the sintered briquette may be obtained.
We have found that by varying the briquetting pressure and/or particle size, it is possible to control the apparent density of the finished part. In this manner it is possible to obtain apparent density of parts in accordance with predetermined specifications. Thus, by changing the briquetting pressure, it is possible to increase or decrease the porosity of the part and thereby increase or decrease the quantity of lead absorption thereof, thus changing the apparent density of the part. Similarly by changing the particle size and/or briquetting pressure similar results are obtainable. In this manner we have found that it is possible to closely control the apparent density of the part so that specified apparent density may be easily obtained. Thus, it is possible to form projectile parts having apparent densities greater than the density of steel, if desired. This is a very important part of our invention since by suitable control methods the projectile parts having desired apparent densities may be obtained whereby the ballistic periormance of the parts may be changed according to the use thereof.
In some cases it is desirable to add a wetting metal to the lead. One of such metals is tin in quantities up to 10%. In this instance, the
tin tends to make lead Wet the surface of the I iron more readily. Thus, lead as mentioned in the appended claims is understood to include small quantities of wetting metals if desired.
Alloys of lead may also be used where appreciable quantities of tin. antimony and the like are present or these other metals may be used in the substantially pure state. Similarly, to facilitate the wetting action of the impregnant and impregnation of the sintered iron briquette, it may be desirable in some instances to fiux the part either with a liquid flux or by means of a reducing atmosphere at an elevated temperature for cleaning the surface of the article of oxides. in this respect it should be understood that the briquette may go into the impregnating oath immediately after sintering and prior to exposure to atmospheric air. In this instance the article may be cooled down to a suitable temperature in controlled atmosphere prior to impregnation. It is manifest that instead of lead or alloys thereof that other metals may be used as impregnants. For example, copper or copper alloys are quite suitable for use as impregnants for iron parts. In fact the only limiting factor in an impregnating metal is the melting point. Obviously, this figure must be less than the melting point of the projectile part.
While the embodiments of the present invention as herein disclosed, constitute preferred forms, it is to be understood that other forms might be adopted, all comin within the scope of theclaims which follow.
What is claimed is as follows:
1. A projectile, made from sintered briquetted iron powder which is coated over with and has the pores substantially filled with a metal softer than and heavier than iron and impregnated therein, whereby the said projectile has a relatively soft surface thereover and an apparent density greater than a sintered iron briquette.
2. A projectile, made from sintered briquetted iron powder having an apparent density in excess of 60% of the density of iron, said projectile being coated over with and having the pores substantially filled with lead which is impregnated therein, whereby said projectile has a soft surface thereover.
3. A projegtile, made from sintered briquetted iron powder and having an apparent density in excess of 60% of the density of iron, said projectile being coated over with and having the pores substantially filled with a lead alloy which is impregnated therein, whereby the said projectile has a soft surface thereover.
4. A projectile, made of two portions, including a nose portion formed from a relatively hard metallic material and a body portion formed from sinter d briquetted iron powder, said body portion being metallurgically bonded to said nose portion, said body portion of the projectile being coated over with and having the pores filled with a lead base alloy for producing a relatively soft surface thereover and for increasing the weight of the projectile.
5. A projectile, made of two portions, including a nose portion formed from a relatively hard metallic material and a body portion formed from sintered briquetted iron powder, said body portion being metallurgically bonded to said nose portion, said body portion of the projectile being coated over with and having the pores filled with lead for producing a relatively soft surface thereover and for increasing the weight of the projectile.
EARL S. PATCH. WILEY T. MOORE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US449280A US2409307A (en) | 1942-07-01 | 1942-07-01 | Projectile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US449280A US2409307A (en) | 1942-07-01 | 1942-07-01 | Projectile |
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US2409307A true US2409307A (en) | 1946-10-15 |
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US449280A Expired - Lifetime US2409307A (en) | 1942-07-01 | 1942-07-01 | Projectile |
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Cited By (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2669930A (en) * | 1946-01-05 | 1954-02-23 | Remington Arms Co Inc | Sabot projectile |
US2741827A (en) * | 1950-12-22 | 1956-04-17 | August H Schilling | Process for the manufacture of piston rings by powder metallurgy and articles obtained thereby |
US2801590A (en) * | 1951-06-14 | 1957-08-06 | Claire C Balke | Pyrophoric element |
US2805624A (en) * | 1952-03-11 | 1957-09-10 | Olin Mathieson | Metallurgical process |
US2819961A (en) * | 1952-12-20 | 1958-01-14 | Int Standard Electric Corp | Process for connecting a tantalum electrode pin to an electrode body |
US2950523A (en) * | 1955-06-02 | 1960-08-30 | John A Bitterli | Cutting tool and method of making |
US2985571A (en) * | 1956-11-09 | 1961-05-23 | North American Aviation Inc | Lead-uranium oxide nuclear fuel element |
US2995090A (en) * | 1954-07-02 | 1961-08-08 | Remington Arms Co Inc | Gallery bullet |
US3026806A (en) * | 1957-03-22 | 1962-03-27 | Russell Mfg Co | Ballistic missile nose cone |
US3107418A (en) * | 1958-09-23 | 1963-10-22 | Mc Graw Edison Co | Refractory metal contacts and methods of manufacture |
US3157137A (en) * | 1963-04-01 | 1964-11-17 | Olin Mathieson | Expanding point bullet |
US3250661A (en) * | 1958-02-18 | 1966-05-10 | Avco Mfg Corp | Reinforced material and method of making the same |
US3301300A (en) * | 1964-03-16 | 1967-01-31 | Natter Bernd | Traction studs for vehicle tires |
US3495957A (en) * | 1965-03-15 | 1970-02-17 | Mitsubishi Metal Corp | Lead-impregnated,iron-base,sinteredalloy materials for current-collecting slider shoes |
US3812565A (en) * | 1971-12-27 | 1974-05-28 | Nissan Motor | SINTERED FE{13 CR{13 C{13 {8 MO{13 V{13 Ni{9 {11 ALLOYS IMPREGNATED WITH Pb OR Rb-BASE ALLOYS |
DE2322728A1 (en) * | 1973-05-05 | 1977-03-10 | Diehl Fa | SPLITTER CASE FOR BULLETS, BATTLE HEADS, THROWING AMMUNITION, etc. |
US4603637A (en) * | 1984-10-31 | 1986-08-05 | The United States Of America As Represented By The Secretary Of The Air Force | Variable density frangible projectile |
WO1993016349A1 (en) * | 1992-02-07 | 1993-08-19 | Snc Industrial Technologies Inc. | Frangible practice ammunition |
EP0626557A1 (en) * | 1993-05-27 | 1994-11-30 | Royal Ordnance plc | Practice projectile made of sintered metal powder |
US5399187A (en) * | 1993-09-23 | 1995-03-21 | Olin Corporation | Lead-free bullett |
WO1996041113A1 (en) * | 1995-06-07 | 1996-12-19 | Lockheed Martin Energy Systems, Inc. | Projectiles having controllable density and mass distribution |
WO1998002266A1 (en) * | 1996-07-11 | 1998-01-22 | Scm Metal Products, Inc. | Lead free-franglible bullets and process for making same________ |
US5728968A (en) * | 1989-08-24 | 1998-03-17 | Primex Technologies, Inc. | Armor penetrating projectile |
WO1999008063A1 (en) * | 1997-08-08 | 1999-02-18 | Remington Arms Company, Inc. | Frangible powdered iron projectiles |
WO2000002689A2 (en) * | 1998-04-22 | 2000-01-20 | Sinterfire, Inc. | Frangible metal bullets, ammunition and method of making such articles |
US6149705A (en) * | 1994-07-06 | 2000-11-21 | Ut-Battelle, Llc | Non-lead, environmentally safe projectiles and method of making same |
US6158351A (en) * | 1993-09-23 | 2000-12-12 | Olin Corporation | Ferromagnetic bullet |
US6174494B1 (en) | 1993-07-06 | 2001-01-16 | Lockheed Martin Energy Systems, Inc. | Non-lead, environmentally safe projectiles and explosives containers |
US6536352B1 (en) | 1996-07-11 | 2003-03-25 | Delta Frangible Ammunition, Llc | Lead-free frangible bullets and process for making same |
US6640724B1 (en) | 1999-08-04 | 2003-11-04 | Olin Corporation | Slug for industrial ballistic tool |
US6892647B1 (en) | 1997-08-08 | 2005-05-17 | Ra Brands, L.L.C. | Lead free powdered metal projectiles |
US20050223882A1 (en) * | 2004-02-10 | 2005-10-13 | Yaich Daniel S | Cannelured frangible cartridge and method of canneluring a frangible projectible |
US20060281842A1 (en) * | 2004-03-03 | 2006-12-14 | Hoppe Karl M | Malleable composites and methods of making and using the same |
US7399334B1 (en) | 2004-05-10 | 2008-07-15 | Spherical Precision, Inc. | High density nontoxic projectiles and other articles, and methods for making the same |
US8122832B1 (en) | 2006-05-11 | 2012-02-28 | Spherical Precision, Inc. | Projectiles for shotgun shells and the like, and methods of manufacturing the same |
US8393273B2 (en) | 2009-01-14 | 2013-03-12 | Nosler, Inc. | Bullets, including lead-free bullets, and associated methods |
US20150144019A1 (en) * | 2012-05-18 | 2015-05-28 | Nammo Vanasverken Ab | Lead-free ammunition for small-bore weapons |
US20170219325A1 (en) * | 2016-01-15 | 2017-08-03 | Continuous Metal Technology, Inc. | Non-Jacketed Expandable Bullet and Method of Manufacturing a Non-Jacketed Expandable Bullet |
US20170336186A1 (en) * | 2016-01-15 | 2017-11-23 | Continuous Metal Technology, Inc. | Non-Jacketed Bullet and Method of Manufacturing a Non-Jacketed Bullet |
WO2017171692A3 (en) * | 2015-05-28 | 2018-02-15 | Olive Tree Financial Group, L.L.C. | Projectile |
US10222183B2 (en) | 2015-03-02 | 2019-03-05 | Timothy G. Smith | Lead-free rimfire projectile |
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 |
US11674781B2 (en) * | 2014-09-29 | 2023-06-13 | TPI Powder Metallurgy, Inc. | Lead free frangible iron bullets |
-
1942
- 1942-07-01 US US449280A patent/US2409307A/en not_active Expired - Lifetime
Cited By (68)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2669930A (en) * | 1946-01-05 | 1954-02-23 | Remington Arms Co Inc | Sabot projectile |
US2741827A (en) * | 1950-12-22 | 1956-04-17 | August H Schilling | Process for the manufacture of piston rings by powder metallurgy and articles obtained thereby |
US2801590A (en) * | 1951-06-14 | 1957-08-06 | Claire C Balke | Pyrophoric element |
US2805624A (en) * | 1952-03-11 | 1957-09-10 | Olin Mathieson | Metallurgical process |
US2819961A (en) * | 1952-12-20 | 1958-01-14 | Int Standard Electric Corp | Process for connecting a tantalum electrode pin to an electrode body |
US2995090A (en) * | 1954-07-02 | 1961-08-08 | Remington Arms Co Inc | Gallery bullet |
US2950523A (en) * | 1955-06-02 | 1960-08-30 | John A Bitterli | Cutting tool and method of making |
US2985571A (en) * | 1956-11-09 | 1961-05-23 | North American Aviation Inc | Lead-uranium oxide nuclear fuel element |
US3026806A (en) * | 1957-03-22 | 1962-03-27 | Russell Mfg Co | Ballistic missile nose cone |
US3250661A (en) * | 1958-02-18 | 1966-05-10 | Avco Mfg Corp | Reinforced material and method of making the same |
US3107418A (en) * | 1958-09-23 | 1963-10-22 | Mc Graw Edison Co | Refractory metal contacts and methods of manufacture |
US3157137A (en) * | 1963-04-01 | 1964-11-17 | Olin Mathieson | Expanding point bullet |
US3301300A (en) * | 1964-03-16 | 1967-01-31 | Natter Bernd | Traction studs for vehicle tires |
US3495957A (en) * | 1965-03-15 | 1970-02-17 | Mitsubishi Metal Corp | Lead-impregnated,iron-base,sinteredalloy materials for current-collecting slider shoes |
US3812565A (en) * | 1971-12-27 | 1974-05-28 | Nissan Motor | SINTERED FE{13 CR{13 C{13 {8 MO{13 V{13 Ni{9 {11 ALLOYS IMPREGNATED WITH Pb OR Rb-BASE ALLOYS |
DE2322728A1 (en) * | 1973-05-05 | 1977-03-10 | Diehl Fa | SPLITTER CASE FOR BULLETS, BATTLE HEADS, THROWING AMMUNITION, etc. |
US4603637A (en) * | 1984-10-31 | 1986-08-05 | The United States Of America As Represented By The Secretary Of The Air Force | Variable density frangible projectile |
US5728968A (en) * | 1989-08-24 | 1998-03-17 | Primex Technologies, Inc. | Armor penetrating projectile |
WO1993016349A1 (en) * | 1992-02-07 | 1993-08-19 | Snc Industrial Technologies Inc. | Frangible practice ammunition |
EP0626557A1 (en) * | 1993-05-27 | 1994-11-30 | Royal Ordnance plc | Practice projectile made of sintered metal powder |
US6174494B1 (en) | 1993-07-06 | 2001-01-16 | Lockheed Martin Energy Systems, Inc. | Non-lead, environmentally safe projectiles and explosives containers |
US5399187A (en) * | 1993-09-23 | 1995-03-21 | Olin Corporation | Lead-free bullett |
US5814759A (en) * | 1993-09-23 | 1998-09-29 | Olin Corporation | Lead-free shot |
WO1995008653A1 (en) * | 1993-09-23 | 1995-03-30 | Olin Corporation | Lead-free bullet |
US6158351A (en) * | 1993-09-23 | 2000-12-12 | Olin Corporation | Ferromagnetic bullet |
US6149705A (en) * | 1994-07-06 | 2000-11-21 | Ut-Battelle, Llc | Non-lead, environmentally safe projectiles and method of making same |
WO1996041113A1 (en) * | 1995-06-07 | 1996-12-19 | Lockheed Martin Energy Systems, Inc. | Projectiles having controllable density and mass distribution |
US6536352B1 (en) | 1996-07-11 | 2003-03-25 | Delta Frangible Ammunition, Llc | Lead-free frangible bullets and process for making same |
US6074454A (en) * | 1996-07-11 | 2000-06-13 | Delta Frangible Ammunition, Llc | Lead-free frangible bullets and process for making same |
WO1998002266A1 (en) * | 1996-07-11 | 1998-01-22 | Scm Metal Products, Inc. | Lead free-franglible bullets and process for making same________ |
US6892647B1 (en) | 1997-08-08 | 2005-05-17 | Ra Brands, L.L.C. | Lead free powdered metal projectiles |
US5917143A (en) * | 1997-08-08 | 1999-06-29 | Remington Arms Company, Inc. | Frangible powdered iron projectiles |
WO1999008063A1 (en) * | 1997-08-08 | 1999-02-18 | Remington Arms Company, Inc. | Frangible powdered iron projectiles |
US6691623B1 (en) * | 1997-08-08 | 2004-02-17 | Ra Brands, Llc | Frangible powdered iron projectiles |
US6090178A (en) * | 1998-04-22 | 2000-07-18 | Sinterfire, Inc. | Frangible metal bullets, ammunition and method of making such articles |
WO2000002689A2 (en) * | 1998-04-22 | 2000-01-20 | Sinterfire, Inc. | Frangible metal bullets, ammunition and method of making such articles |
US6263798B1 (en) | 1998-04-22 | 2001-07-24 | Sinterfire Inc. | Frangible metal bullets, ammunition and method of making such articles |
WO2000002689A3 (en) * | 1998-04-22 | 2000-03-30 | Sinterfire Inc | Frangible metal bullets, ammunition and method of making such articles |
US20040200340A1 (en) * | 1999-08-04 | 2004-10-14 | Robinson Peter W. | Slug for industrial ballistic tool |
US20110017050A1 (en) * | 1999-08-04 | 2011-01-27 | Robinson Peter W | Slug for industrial ballistic tool |
US7159519B2 (en) | 1999-08-04 | 2007-01-09 | Olin Corporation | Slug for industrial ballistic tool |
US7328658B2 (en) | 1999-08-04 | 2008-02-12 | Olin Corporation | Slug for industrial ballistic tool |
US6640724B1 (en) | 1999-08-04 | 2003-11-04 | Olin Corporation | Slug for industrial ballistic tool |
US7891299B2 (en) | 1999-08-04 | 2011-02-22 | Olin Corporation | Slug for industrial ballistic tool |
US20050223882A1 (en) * | 2004-02-10 | 2005-10-13 | Yaich Daniel S | Cannelured frangible cartridge and method of canneluring a frangible projectible |
US7143679B2 (en) | 2004-02-10 | 2006-12-05 | International Cartridge Corporation | Cannelured frangible cartridge and method of canneluring a frangible projectible |
US20070144395A1 (en) * | 2004-02-10 | 2007-06-28 | International Cartridge Corporation | Cannelured frangible projectile and method of canneluring a frangible projectile |
US7322297B2 (en) | 2004-02-10 | 2008-01-29 | International Cartridge Corporation | Cannelured frangible projectile and method of canneluring a frangible projectile |
US20060281842A1 (en) * | 2004-03-03 | 2006-12-14 | Hoppe Karl M | Malleable composites and methods of making and using the same |
US7157140B1 (en) | 2004-03-03 | 2007-01-02 | Rtp Company | Malleable composites and methods of making and using the same |
US7399334B1 (en) | 2004-05-10 | 2008-07-15 | Spherical Precision, Inc. | High density nontoxic projectiles and other articles, and methods for making the same |
US7422720B1 (en) | 2004-05-10 | 2008-09-09 | Spherical Precision, Inc. | High density nontoxic projectiles and other articles, and methods for making the same |
US8122832B1 (en) | 2006-05-11 | 2012-02-28 | Spherical Precision, Inc. | Projectiles for shotgun shells and the like, and methods of manufacturing the same |
US8393273B2 (en) | 2009-01-14 | 2013-03-12 | Nosler, Inc. | Bullets, including lead-free bullets, and associated methods |
US20150144019A1 (en) * | 2012-05-18 | 2015-05-28 | Nammo Vanasverken Ab | Lead-free ammunition for small-bore weapons |
US11674781B2 (en) * | 2014-09-29 | 2023-06-13 | TPI Powder Metallurgy, Inc. | Lead free frangible iron bullets |
US10222183B2 (en) | 2015-03-02 | 2019-03-05 | Timothy G. Smith | Lead-free rimfire projectile |
WO2017171692A3 (en) * | 2015-05-28 | 2018-02-15 | Olive Tree Financial Group, L.L.C. | Projectile |
US10209045B2 (en) * | 2016-01-15 | 2019-02-19 | Continuous Metal Technology, Inc. | Non-jacketed expandable bullet and method of manufacturing a non-jacketed expandable bullet |
US10107605B2 (en) * | 2016-01-15 | 2018-10-23 | Continuous Metal Technology, Inc. | Non-jacketed bullet and method of manufacturing a non-jacketed bullet |
US20170336186A1 (en) * | 2016-01-15 | 2017-11-23 | Continuous Metal Technology, Inc. | Non-Jacketed Bullet and Method of Manufacturing a Non-Jacketed Bullet |
US10288396B2 (en) | 2016-01-15 | 2019-05-14 | Continuous Metal Technology, Inc. | Non-jacketed bullet and method of manufacturing a non-jacketed bullet |
US20190170489A1 (en) * | 2016-01-15 | 2019-06-06 | Continuous Metal Technology, Inc. | Non-Jacketed Expandable Bullet and Method of Manufacturing a Non-Jacketed Expandable Bullet |
US10591265B2 (en) * | 2016-01-15 | 2020-03-17 | Continuous Metal Technology, Inc. | Non-jacketed expandable bullet and method of manufacturing a non-jacketed expandable bullet |
US20170219325A1 (en) * | 2016-01-15 | 2017-08-03 | Continuous Metal Technology, Inc. | Non-Jacketed Expandable Bullet and Method of Manufacturing a Non-Jacketed Expandable Bullet |
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 |
US11428517B2 (en) | 2019-09-20 | 2022-08-30 | Npee L.C. | Projectile with insert |
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