WO2001018453A1 - A projectile of sintered metal powder - Google Patents
A projectile of sintered metal powder Download PDFInfo
- Publication number
- WO2001018453A1 WO2001018453A1 PCT/SE2000/001565 SE0001565W WO0118453A1 WO 2001018453 A1 WO2001018453 A1 WO 2001018453A1 SE 0001565 W SE0001565 W SE 0001565W WO 0118453 A1 WO0118453 A1 WO 0118453A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- projectile
- rifling
- metal powder
- bore
- porosity
- Prior art date
Links
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
- Y10T428/12021—All metal or with adjacent metals having metal particles having composition or density gradient or differential porosity
-
- 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.]
- Y10T428/12042—Porous component
Definitions
- the present invention relates to a projectile of the kind defined in the preamble of Claim 1.
- the material is considered environmentally friendlv. has a relatively high density, a high toughness and a relatively low hardness, therewith enabling the copper projectile to be provided with a hollow tip, so that it can be used for hunting purposes and therewith expand upon impact.
- the sintered metal powder body of the projectile has a porosity such as to enable the body to be compressed radially with relatively slight resistance during passage of the projectile through the barrel of the weapon if the interference/tolerances require such compression, so that potentially dangerous radial interference between the bore of the barrel and the projectile can be reduced or avoided by the ensuing reduction or elimination of said porosity. Because this radial compaction of a projectile having such porosity can be effected with a lower force than if the projectile should comprise the same material but with full density, it is possible to restrict friction of the projectile through the bore of the barrel and therewith also the gas pressure in the weapon.
- the sintered projectile body may have a porosity in the order of 10%. or generally between 5 and 25%.
- the projectile may conveniently comprise 90-95% by weight copper and 5-10% by weight zinc and/or tin, preferably about 95% by weight copper and 5% by weight zinc/tin This minimises coating of the walls of the bore
- This porosity can be readily achieved by producing the projectile with the aid of a conventional sinte ⁇ ng technique, wherewith a powder is compacted to form a body of desired shape and of desired dimensions and also with the desired porosity, and thereafter sinte ⁇ ng the compacted powder body to desired mechanical strength, for instance to an extent such that the projectile mate ⁇ al will have essentially full toughness. It is possible also in this way to obtain the advantage whereby the projectile will not normally splinter upon impact. This enables the projectile to be formed to "cushion-up" upon impact, therewith enabling the projectile to be used for hunting purposes with a fully satisfactory result.
- the projectiles can be easily collected from, e.g., the sand used in the construction of a practice fi ⁇ ng range and reused when they are still substantially in one piece after st ⁇ king the embankment on the fi ⁇ ng range.
- the invention also includes projectiles that splinter either completely or partially upon impact with a target surface, which may be desirable m respect of, e.g., practice ammunition so that penetration of the projectile can be reduced.
- a major volumet ⁇ c part of the projectile may be produced from a metal powder, e.g , iron or steel, which results in lower costs.
- the inventive projectile can be further developed within the scope of the invention
- the projectile may be given a core of some other mate ⁇ al, for instance hardmetal, or a heavy mate ⁇ al, such as tungsten, in order to give the projectile a relatively high density and/or certain determined ballistic properties
- the projectile core can be formed from a mate ⁇ al of full density
- the core can be formed from a powder different to its pe ⁇ pheral parts, wherewith the core powder may optionally be compacted, for instance in an axially exposed cavity in that part of the projectile that forms said outer parts
- the powder composition of the projectile may be va ⁇ ed along the longitudinal axis thereof
- the projectile has an outer layer of porous mate ⁇ al, for instance tin or a tin alloy, that can be compacted radially essentially by eliminating or reducing said porosity as the projectile passes through the bore of the barrel, even in the case of troublesome tolerance overlap, so as to enable the projectile body to be made from a material which in a solid design would cause damage to the bore wall, for instance due to hardness, or would be liable to promote a hazardous gas pressure in the weapon.
- the material may also be chosen so as not to coat the lands of the rifling in the barrel, or only to a very small extent.
- the inventive porosity of the projectile also enables the use of powder material which in addition to including a relatively large proportion of relatively soft basic material (copper, copper alloy) also contains a minor proportion of hard particles which can be pressed back into the porous, relatively soft material layer upon temporary contact with the wall of the bore.
- the porosity of the projectile may be in the region of 5-25%, preferably about 10%.
- the porosity of the projectile shall be sufficiently high to enable the projectile to be compacted radially with small resistance, particularly its radially outer parts upon interference between the projectile and the wall of the barrel.
- the porosity of the projectile shall be so small that the decrease in density of the projectile due to the porosity will be as small as possible.
- the projectile has a solid, completely rigid core with a porous outer layer that contacts the wall of the bore directly and engages the rifling of the barrel, in which case the thickness of the porous outer covering of the projectile will preferably be such that the radial compaction of the projectile required to avoid the generation of hazardous gas pressures can be achieved by elimination of said porosity.
- the projectile can be produced from a unitary powder alloy that is compacted to form the projectile body, which is then sintered and preferably pressed to the desired calibration.
- the projectile may be desirable in some instances to form the projectile from two or more pre-manufactured complementary projectile parts which are joined and connected, preferably by pressing and suitably in conjunction with a calibration pressing process.
- These parts may have different compositions/ alloying, such as to provide the projectile with a bore co-acting outer covering that has the aforementioned advantageous properties, namely a relatively high density, a radial compressiveness that is reduced by said porosity, a material selection that results in minimum coating of steel bore surfaces.
- the remaining parts of the projectile that do not thus co-act with the rifling of the bore can be selected to impart other desired properties to the projectile.
- said other body parts may be comprised of tungsten or tungsten alloys when a high density is desired.
- iron powder can be used, which also has a relatively high density.
- Bismuth and tin are also conceivable materials that result in a relatively low load on the environment.
- the manufacturing process is the same as that applied conventionally in the manufacture of metal objects by metal powder sintering techniques, wherewith the powder is conventionally compacted in a cold state to a desired body shape, whereafter said body is sintered at a temperature chosen to promote desired mechanical strength properties.
- the sintered body can be subjected to a calibration pressing process to give the body a more precise outer shape.
- the inventive projectile is conveniently produced from a powder that consists mainly of a copper alloy, for instance 95% by weight copper and 5% by weight zinc. Such an alloy has been found particularly favourable with respect to minimum coating of the bore surfaces.
- the powder may also include minor proportions of another powder that impa ⁇ s other properties to the projectile, for instance a higher density. Even though such hard particles imply, per se, a scratching or scoring risk or the risk of elevated bore wear, the invention affords the advantage that the porosity of the body enables the hard particles to be pressed down more easily into the more resilient parts of the sintered body.
- the inventive projectile may, for instance, be produced in calibre of up to 0.5 inch in diameter (heavy machine gun) or 20 mm in diameter (automatic canon), wherein the choice of material and porosity may also be used to limit the firing range of the weapon, which may be beneficial in conjunction with firing practice.
- Fig. 1 is an axial section view of an inventive projectile.
- the projectile shown in Fig. 1 includes a primary body 1 whose outer cylindrical surface is intended to enable the projectile to engage the helical rifling in the bore of a gun.
- the illustrated projectile includes a primary body 1 that has a central, preferably co-axial and rotationally-symmetrical recess 2 in one end thereof, preferably its front end.
- a core 3 is fastened stably in the recess 2 and conveniently has a recess-complementary shape.
- the body 1 is comprised of an alloy of Cu (90-95% by weight) and Zn (the remainder), and has a porosity of 10%.
- the core 3 does not contact the rifling of the bore and may be comprised of material that fulfils desired requirements, for instance low cost, brittleness, density, manufacturing costs, and environmentally friendliness and the like.
- the core 3 of the illustrated embodiment may be formed by a sintered metal powder body, for instance a body comprised of iron powder.
- the core 3 and the body 1 can include particles of a foreign material, for instance heavy particles that serve to increase the density of the body/core.
- Fig. 1 shows by way of example a so-called W.C. bullet, calibre 38, that has a diameter of 9.07 mm for correct co-action with the rifling of a corresponding bore in respect of a 38 calibre firearm.
- the recess 2 in said body defines a wall thickness of about 2 mm for the front part of the body 1.
- the depth of the recess is about 10 mm.
- the total length of the body 1 is about 14 mm.
- the core 3 may alternatively have a porosity of 10% by volume for example.
- the core 3 may be formed by cold compaction of a metal powder in a mould. The compacted, moulded core may then be sintered to obtain desired mechanical strength properties.
- the body 1 is produced from a powder comprised of the aforesaid alloy, this powder being cold compacted in a mould and the compacted powder body then sintered to impart desired properties thereto.
- the body has a porosity of about 10%.
- the core is then inserted into the recess in said body and the body and core then subjected to a calibration pressing process that imparts well-determined outer cross-sectional dimensions to the resultant projectile on the one hand, and secures the core in the body recess 2 on the other hand.
- the core can be diversified so that it can be deformed by the rifling in the bore of the barrel with the deformation resulting in a fragile or brittle core.
- the diameter of the recess in the body 1 is made slightly larger than the diameter of the core, so that the core can be easily inserted into the recess prior to the calibration pressing process, if this process is able to deform the body 1 into securing contact with the core.
- an inventive projectile (not shown) which is assumed to be the most common, a powder comprised of Cu-Zn alloy (95 and 5% by weight) is compacted in a mould to form a pressed body that is later sintered.
- the moulding and sintering conditions are chosen so that the sintered body will be somewhat overdimensioned in respect to desired final dimensions.
- the sintered projectile body is calibration pressed to impart a desired outer dimension, i.e. to eliminate shape deviations resulting from the sintering process.
- the powder and the working operations are chosen to give the projectile a final porosity of about 10%, at least in its outer layer.
- the projectile is given standard calibre dimensions, so that its outer layer will engage with the helical rifling in the barrel, and therewith impart the correct rotation and guidance to the projectile.
- a projectile of .30 calibre (diameter about 7.6 mm) produced in accordance with the invention on the basis of powder comprising Cu-Zn alloy (95% by weight Cu, 5% by weight Zn) was manufactured by compacting a powder mass at a pressure of 6000 bar, to form a shaped body having a porosity of about 10%.
- the shape of the body conformed essentially with the desired shape of the projectile, and was sintered at a temperature of 1000-1050°C under a shielding gas for 33 minutes (30-40 min.). After cooling, the projectile was calibration pressed at 6000 bar to its final shape, said projectile then having a porosity of 10%.
- the hardness of the projectile was measured as being 80% of the hardness of a solid projectile comprised of said alloy.
- At least the porous sintered outer layer of the projectile may include a significant proportion of a metal, such as copper for instance, that preferably has a lubricating function against the bore wall, for instance a steel wall.
- This metal (copper) proportion will correspond at least to 10% by weight and preferably 20% by weight.
- a projectile intended, for example, for practice tiring on a firing range may. for instance. comprise in at least its outer cylindrical layer a porous, sintered powder mixture that consists of a further 20% by weight copper granules and 80% by weight granules of another substance, for instance a metal or a metal alloy such as steel, whose granules or grains are covered with copper.
- At least the porous, sintered outer cylindrical layer of the projectile may consist of tin bronze that preferably contains at least 80% by weight copper and the remainder essentially tin, preferably about 90% by weight copper and the remainder tin.
Landscapes
- 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)
- Carbon And Carbon Compounds (AREA)
- Jellies, Jams, And Syrups (AREA)
- Solid-Sorbent Or Filter-Aiding Compositions (AREA)
- Materials For Medical Uses (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU66034/00A AU6603400A (en) | 1999-09-03 | 2000-08-10 | A projectile of sintered metal powder |
US10/069,509 US6776818B1 (en) | 1999-09-03 | 2000-08-10 | Projectile of sintered metal powder |
DK00953614T DK1210551T3 (en) | 1999-09-03 | 2000-08-10 | Sintered metal powder projectile |
DE60021093T DE60021093T2 (en) | 1999-09-03 | 2000-08-10 | SHOP PRODUCED FROM SINTERED POWDER |
AT00953614T ATE298870T1 (en) | 1999-09-03 | 2000-08-10 | BULLET MADE FROM SINTERED POWDER |
EP00953614A EP1210551B1 (en) | 1999-09-03 | 2000-08-10 | A projectile of sintered metal powder |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9903111A SE517797C2 (en) | 1999-09-03 | 1999-09-03 | Projectile of sintered metal powder |
SE9903111-4 | 1999-09-03 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2001018453A1 true WO2001018453A1 (en) | 2001-03-15 |
WO2001018453A8 WO2001018453A8 (en) | 2001-07-12 |
Family
ID=20416841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/SE2000/001565 WO2001018453A1 (en) | 1999-09-03 | 2000-08-10 | A projectile of sintered metal powder |
Country Status (9)
Country | Link |
---|---|
US (1) | US6776818B1 (en) |
EP (1) | EP1210551B1 (en) |
AT (1) | ATE298870T1 (en) |
AU (1) | AU6603400A (en) |
DE (1) | DE60021093T2 (en) |
DK (1) | DK1210551T3 (en) |
ES (1) | ES2240143T3 (en) |
SE (1) | SE517797C2 (en) |
WO (1) | WO2001018453A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7690312B2 (en) * | 2004-06-02 | 2010-04-06 | Smith Timothy G | Tungsten-iron projectile |
US8393273B2 (en) | 2009-01-14 | 2013-03-12 | Nosler, Inc. | Bullets, including lead-free bullets, and associated methods |
ES2676313T3 (en) * | 2014-02-10 | 2018-07-18 | Ruag Ammotec Gmbh | Lead-free deformation and partial fragmentation projectile with a defined expansion and fragmentation behavior |
AU2015288295C1 (en) | 2014-04-30 | 2020-02-13 | G9 Holdings, Llc | Projectile with enhanced ballistics |
DE102015110097B4 (en) | 2015-06-23 | 2022-07-14 | Kurt Pritz | Bullet made of tin bronze material |
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 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB647172A (en) * | 1947-08-13 | 1950-12-06 | Hazeltine Corp | Multiple-tuned wave-selector system |
CA2231572A1 (en) * | 1996-07-11 | 1998-01-22 | John T. Abrams | Lead-free frangible bullets and process for making same |
US5877437A (en) * | 1992-04-29 | 1999-03-02 | Oltrogge; Victor C. | High density projectile |
US5950064A (en) * | 1997-01-17 | 1999-09-07 | Olin Corporation | Lead-free shot formed by liquid phase bonding |
WO2000002689A2 (en) * | 1998-04-22 | 2000-01-20 | Sinterfire, Inc. | Frangible metal bullets, ammunition and method of making such articles |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB697172A (en) | 1950-06-17 | 1953-09-16 | Birmingham Small Arms Co Ltd | Improvements in or relating to armour-piercing cores for projectiles |
US5852256A (en) * | 1979-03-16 | 1998-12-22 | The United States Of America As Represented By The Secretary Of The Air Force | Non-focusing active warhead |
CA1327913C (en) * | 1989-02-24 | 1994-03-22 | Yvan Martel | Non-ricocheting projectile and method of making same |
US5198616A (en) * | 1990-09-28 | 1993-03-30 | Bei Electronics, Inc. | Frangible armor piercing incendiary projectile |
GB9310915D0 (en) | 1993-05-27 | 1993-07-14 | Royal Ordance Plc | Improvements in or relating to projectiles |
-
1999
- 1999-09-03 SE SE9903111A patent/SE517797C2/en not_active IP Right Cessation
-
2000
- 2000-08-10 EP EP00953614A patent/EP1210551B1/en not_active Expired - Lifetime
- 2000-08-10 AT AT00953614T patent/ATE298870T1/en not_active IP Right Cessation
- 2000-08-10 WO PCT/SE2000/001565 patent/WO2001018453A1/en active IP Right Grant
- 2000-08-10 ES ES00953614T patent/ES2240143T3/en not_active Expired - Lifetime
- 2000-08-10 AU AU66034/00A patent/AU6603400A/en not_active Abandoned
- 2000-08-10 US US10/069,509 patent/US6776818B1/en not_active Expired - Fee Related
- 2000-08-10 DK DK00953614T patent/DK1210551T3/en active
- 2000-08-10 DE DE60021093T patent/DE60021093T2/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB647172A (en) * | 1947-08-13 | 1950-12-06 | Hazeltine Corp | Multiple-tuned wave-selector system |
US5877437A (en) * | 1992-04-29 | 1999-03-02 | Oltrogge; Victor C. | High density projectile |
CA2231572A1 (en) * | 1996-07-11 | 1998-01-22 | John T. Abrams | 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 |
WO2000002689A2 (en) * | 1998-04-22 | 2000-01-20 | Sinterfire, Inc. | Frangible metal bullets, ammunition and method of making such articles |
Also Published As
Publication number | Publication date |
---|---|
SE517797C2 (en) | 2002-07-16 |
SE9903111D0 (en) | 1999-09-03 |
EP1210551A1 (en) | 2002-06-05 |
AU6603400A (en) | 2001-04-10 |
DE60021093D1 (en) | 2005-08-04 |
ATE298870T1 (en) | 2005-07-15 |
EP1210551B1 (en) | 2005-06-29 |
US6776818B1 (en) | 2004-08-17 |
WO2001018453A8 (en) | 2001-07-12 |
DK1210551T3 (en) | 2005-10-24 |
ES2240143T3 (en) | 2005-10-16 |
DE60021093T2 (en) | 2005-12-08 |
SE9903111L (en) | 2001-03-04 |
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