US2401483A - Projectile and method of making the same - Google Patents

Projectile and method of making the same Download PDF

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US2401483A
US2401483A US348674A US34867440A US2401483A US 2401483 A US2401483 A US 2401483A US 348674 A US348674 A US 348674A US 34867440 A US34867440 A US 34867440A US 2401483 A US2401483 A US 2401483A
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metal
segments
alloys
shell
projectile
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US348674A
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Franz R Hensel
Earl I Larsen
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Duracell Inc USA
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PR Mallory and Co Inc
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    • 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
    • F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
    • 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
    • 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
    • Y10T428/12229—Intermediate article [e.g., blank, etc.]
    • Y10T428/12236—Panel having nonrectangular perimeter
    • Y10T428/12243—Disk
    • 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
    • Y10T428/12292—Workpiece with longitudinal passageway or stopweld material [e.g., for tubular stock, etc.]
    • 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
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771—Transition metal-base component
    • Y10T428/12861—Group VIII or IB metal-base component
    • Y10T428/12951—Fe-base component

Definitions

  • This invention relates to projectiles and the manufacture thereof.
  • An object of the invention is to improve projectiles.
  • Another object is to improve the methods used in projectile manufacture.
  • Figure 3 is a side view of a' complete projectile
  • Figure 4 is a side view of a shell body of modified construction
  • Figure 5 to 8 inclusive are diagrammatic illustrations of steps in the manufacture of a section of a shell body
  • Figure 9 shows one method of uniting sections I into a unitary shell structure
  • Figures 10 and- 11 illustrate steps in another method of assembling a shell:
  • the shell body is made from metal powders, pressed into shape and sintered.
  • Another fea ture of the invention resides in the use of segments of predetermined size and shape, a plurality of which are assembled to produce a comlete shell body.
  • FIG. 1 illustrates one form of shell element or segment formed from pressed and sintered metal powders. This mixed powders into a die or mold of the shape desired, then applying the necessary pressure by meansof a plunger in a suitable press, and subsequently sintering the pressed body in a neutral or reducing atmosphere.
  • Iron-group metal or steel powders or powder mixtures having such composition are suitable.
  • alloys may be made by melting and be subsequently reduced to a fine powder by crushing, ball milling or other methods of disintegration. In some cases, where forming pressures have been usedwhich leave the segment 20 somewhat porous after sintering, the segment may subsequently. be impregnated with a lower melting,
  • point metal such as lead or lead alloys, copper or its alloys, such as brass and bronze, or zinc, tin or cadmium base alloys, by immersing the segment in a molten bath of such metal or by impregnating it by any other convenient method.
  • Low melting eutectics or compounds of binary and ternary alloy systems may also be used for impregnating. This fills the voids in the sintered segment and increases its density. Also, where a lubricant such as lead is used for impregnating, it aids in producing a low friction outer surface on the shell body.
  • a high density metal such as .as tungsten or an alloy thereof may be substituted partly or wholly for the iron or iron alloy.
  • the sintered tungsten (or other high density metal) body may be impregnated with lead or like lowmelting metal or alloy.
  • a coining or repressing operation may be added to theabove processes after sintering. Where an impregnating step is used the coining step,
  • the segments 20 are assembled as illustrated in Figure 2 to form the shell wall 2
  • the joints 22 between segments 20 are sealed and the segments bonded together by metal fusion. This may be accomplished in several difierent ways, such as:
  • the sintered segments may be assembled as shown in a suitable holder or press and then the entire assembly impregnated by immersion in molten lead or other low melting metal, withdrawing the impregnated assembly, wiping the outer surfaces clean and smooth, and allowing to cool and solidify.
  • the impregnated or unimpregnated seg ments may be brazed together by introducing a small quantity of brazing material in the joints and firing the assembly in a furnace. Copper or silver base alloys may be used as brazes as well as high manganese alloys such as copper manganese or nickel manganese alloys. Eutectlcs of iron group metals with phosphorus or sulfur, and other metals or alloys having lower melting points than the sintered body may also be used. Where impregnated segments are used the impregnant itself will form a fusion bond between segments when heated in the furnace.
  • the physical properties of the joints are determined by selecting the proper chemical composition. Thus where a brittle Joint is desired a brittle brazing material is used. Also by regulating the porosity of the segments and selecting certain compositions of brazing metal the brazing metal will be almost wholly absorbed by the segments leaving a weaker bond.
  • brazing metal maybe introduced in the joints and the assembly heated to efiect both sintering of the metal of the segments and together.
  • the pressed segments may be assembled and immersed in impregnating metal, heated to sintering temperature forthe pressed metal powder, effecting sintering and impregna- I tion in one step.
  • Figure 3 shows a completed. projectile comprising a nose, shell body 2 I, rifiing ring 24 and drawn brass cartridge 25.
  • the nose 23 is generally formed of harder i and tougher metal or metal composition having armor piercing qualities. It may be made of cast or forged metal or of pressedand sintered alloy powders and brazed to the shell body 2
  • brazing of the segments Rifiing ring 24 is required to be sufllciently soft to act as a. bearing guide engaging the riflings of the gun to rotate the shell when it is fired.
  • This may suitably be formed of copper or a copper alloy and may be attached to the shell body by brazing, shrinking, screwing or appliedby electro,
  • Figure 4 illustrates ashell body especially suitable'for smaller projectiles, made from pressed metal powders.
  • the nose 26 of armor'piercing ,inetal- may be cast or forged metal although pressed and sintered metal powders such as hard metal carbide compositions are sometimes suitable.
  • the nose is brazed or otherwise bonded to the shell body 21 formed from pressed and sin-' reduced to fit into the cartridge.
  • A. cavity 30 may 'be provided therein to hold explosives.
  • the shell if not too large or complicated in design may be made complete in a single molding operation.
  • the powders may be molded directly against the nose 26 (which may be roughened or provided with projections to mechanically interlock with the molded powder).
  • the entire body may then be sintered to eflect bonding of 'all parts, and subsequently impregnated with lower'melting point metal, such as lead.
  • Figures 5 to 8 inclusive illustrate the steps in a process of making ring-like sections 3
  • the metal powders 32 are charged into a circular die 33
  • are welded together by resistance welding in the welding ma-.
  • chine 38 shown diagrammatically in Figure 9.
  • a, ring 39 which has no welding projection is placed on the lower electrode 40 of the machine and a ring 3
  • is brought down to clamp the two rings between them and-after sufficient pressure has been applied electric current is applied through conductors 42. Since ridge 36 has the smallest cross section and hence highest resistance in the circuit it is fused by the electric current, spreading out and welding the rings together.
  • are added, one at a time, in like manner, the rings being-aligned and guided by guide ring 43 supported by the machine. In fact the whole operation of feeding, aligning and welding may be almost wholly automatic.
  • a. series of separate welding rings of reduced cross section may be used interspersed with a series of flat rings 39, the welding proceeding in the same manner.
  • Figures 10 and 11 illustrate an automatic appa- I ratus and method for assembly and furnace brazing of shell bodies.
  • Pressed powder rings 39 (having notches 31- if desired) are stacked in hopper 44 of the assembling machine of Figure 10 and thin rings 45 of brazing metal in hopper 46.
  • a pair of automatic pusher arms 41 and 48 shove one of the rings 39 and 46 alternately into a third hopper 49 to form a stack of alternate rings 39 and 45.
  • the truck on which the stack is formed is released and rolls into furnace 5
  • Nose pieces 52 may be added on top of each stack in the assembling machine all of one composition or different segments may,
  • the resistance welded, sinter bonded, brazed, impregnated or otherwise bonded projectile may be given a coining, broaching, pressing or shaping operation to bring the projectile to within the desired degree of accuracy.
  • a shell body which comprises forming a plurality of individual sections, a, plurality of said sections comprising compact bonded masses of metal powders, assembling said sections in contiguous relation and immersing the assembly in a body of molten metal of lower melting point than the metals of said sections, to impregnate said metal powder sections withsaid molten metal and bond said sections together.
  • a shell body formed at least in part of a compact mass of ferrous metal powders interspersed with an impregnating metal of lower melting point than said powders and selected from the group consisting of lead and alloys thereof, babbitt, copper alloys, silver alloys, zinc base alloys, tin base alloys and cadmium base alloys.

Description

PROJECTILE AND METHOD OF MAKING THE SAME Filed July 51, 1940 INVENTQRS 7314112 B Hansel svfi'arl I Zarsen/ ATTORNEY Patented June 4, 1946 I PROJECTILE AND METHOD OF IWAKING THE SAME Franz It. Hansel and Earl 1 Larsen,'lndianapolis,
Ind., assignors. to P. R. Mallory & '00., Inc., Indianapolis, Ind, a corporation of Delaware Application July 31, 1940, Serial No. 348,674
- 1 This invention relates to projectiles and the manufacture thereof.
An object of the invention is to improve projectiles.
Another object is to improve the methods used in projectile manufacture.
Other objects of the invention will be-apparent from the following description and accompanying drawing taken in connection with the ap- 3 Claims. (cl. 102--92.5)
l is made by charging a metal powder or pre Figure 3 is a side view of a' complete projectile;
Figure 4 is a side view of a shell body of modified construction;
Figure 5 to 8 inclusive are diagrammatic illustrations of steps in the manufacture of a section of a shell body;
Figure 9 shows one method of uniting sections I into a unitary shell structure; and
Figures 10 and- 11 illustrate steps in another method of assembling a shell:
According toone aspect of the present invention the shell body is made from metal powders, pressed into shape and sintered. Another fea ture of the invention resides in the use of segments of predetermined size and shape, a plurality of which are assembled to produce a comlete shell body.
While a preferred'embodiment of the invention is described herein, it is-contemplated that considerable variation may be made in the method of procedure and the construction of parts without departing from the spirit of the invention. In the following description and in the claims, parts will b identified by specific names for convenience, but they are intended to be as generic in their application to similar parts as the art will permit.
Heretofore projectiles have been made from forgings and castings. The. number of available compositions for forgingsare limited by the requirement that the steel used must be capable of I hot and cold working Moreover, withboth forgings and castings a considerable amount of machine work, expensive in'both time and materials, is necessary. We contemplate the manufacture of shell bodie for projectilesfrom powdered metal, especially powdered iron on iron alloys or iron group metals, namely nickel and cobalt and their alloys. .This
may be used to produce a novel shell element which can'be assembled in a novel automatic manner into a complete shell body.
Referring to the drawing Figure 1 illustrates one form of shell element or segment formed from pressed and sintered metal powders. This mixed powders into a die or mold of the shape desired, then applying the necessary pressure by meansof a plunger in a suitable press, and subsequently sintering the pressed body in a neutral or reducing atmosphere.
. Iron-group metal or steel powders or powder mixtures having such composition are suitable.
Also alloys of iron with such metals as nickel,
cobalt, manganese, chromium, molybdenum, tungsten, vanadium, columbium, tantalum, ti-
tanium, zirconium, copper, aluminum, beryllium 2 and such non-metals as carbon, silicon, phosphorus, boron, sulfur, and nitrogen are suitable. The alloys may be made by melting and be subsequently reduced to a fine powder by crushing, ball milling or other methods of disintegration. In some cases, where forming pressures have been usedwhich leave the segment 20 somewhat porous after sintering, the segment may subsequently. be impregnated with a lower melting,
point metal, such as lead or lead alloys, copper or its alloys, such as brass and bronze, or zinc, tin or cadmium base alloys, by immersing the segment in a molten bath of such metal or by impregnating it by any other convenient method.
Low melting eutectics or compounds of binary and ternary alloy systems may also be used for impregnating. This fills the voids in the sintered segment and increases its density. Also, where a lubricant such as lead is used for impregnating, it aids in producing a low friction outer surface on the shell body. Q
Where still higher densities are desired itis contemplated that a high density metal such .as tungsten or an alloy thereof may be substituted partly or wholly for the iron or iron alloy. The sintered tungsten (or other high density metal) body may be impregnated with lead or like lowmelting metal or alloy. A coining or repressing operation may be added to theabove processes after sintering. Where an impregnating step is used the coining step,
or an added coining step, may be applied after impregnation.
The segments 20 are assembled as illustrated in Figure 2 to form the shell wall 2| defining within it a chamber for the bursting charge of explosive and shrapnel. The joints 22 between segments 20 are sealed and the segments bonded together by metal fusion. This may be accomplished in several difierent ways, such as:
(1) Instead of impregnating the individual segments with low melting point metal, the sintered segments may be assembled as shown in a suitable holder or press and then the entire assembly impregnated by immersion in molten lead or other low melting metal, withdrawing the impregnated assembly, wiping the outer surfaces clean and smooth, and allowing to cool and solidify.
(2) The impregnated or unimpregnated seg ments may be brazed together by introducing a small quantity of brazing material in the joints and firing the assembly in a furnace. Copper or silver base alloys may be used as brazes as well as high manganese alloys such as copper manganese or nickel manganese alloys. Eutectlcs of iron group metals with phosphorus or sulfur, and other metals or alloys having lower melting points than the sintered body may also be used. Where impregnated segments are used the impregnant itself will form a fusion bond between segments when heated in the furnace.
The physical properties of the joints are determined by selecting the proper chemical composition. Thus where a brittle Joint is desired a brittle brazing material is used. Also by regulating the porosity of the segments and selecting certain compositions of brazing metal the brazing metal will be almost wholly absorbed by the segments leaving a weaker bond.
High ferro-manganese, very low in carbon, with or without other elements such as cobalt, nickel, chromium, tungsten, molybdenum, silicon and titanium, can be used for bonding metals.
(3) It is also possible to combine the sintering with the bonding operation. Thus the brazing metal maybe introduced in the joints and the assembly heated to efiect both sintering of the metal of the segments and together. Or the pressed segments may be assembled and immersed in impregnating metal, heated to sintering temperature forthe pressed metal powder, effecting sintering and impregna- I tion in one step.
Figure 3 shows a completed. projectile comprising a nose, shell body 2 I, rifiing ring 24 and drawn brass cartridge 25. The nose 23 is generally formed of harder i and tougher metal or metal composition having armor piercing qualities. It may be made of cast or forged metal or of pressedand sintered alloy powders and brazed to the shell body 2|.
brazing of the segments Rifiing ring 24 is required to be sufllciently soft to act as a. bearing guide engaging the riflings of the gun to rotate the shell when it is fired. This may suitably be formed of copper or a copper alloy and may be attached to the shell body by brazing, shrinking, screwing or appliedby electro,
ring is electroplated onto the shell plating. Ifthe body the porosity-bf the, P e sed powder segments aflords an excellent mechanically interlocking joint.
Figure 4 illustrates ashell body especially suitable'for smaller projectiles, made from pressed metal powders. The nose 26 of armor'piercing ,inetal-may be cast or forged metal although pressed and sintered metal powders such as hard metal carbide compositions are sometimes suitable. The nose is brazed or otherwise bonded to the shell body 21 formed from pressed and sin-' reduced to fit into the cartridge. A. cavity 30 may 'be provided therein to hold explosives.
The shell if not too large or complicated in design may be made complete in a single molding operation. If desired, the powders may be molded directly against the nose 26 (which may be roughened or provided with projections to mechanically interlock with the molded powder). The entire body may then be sintered to eflect bonding of 'all parts, and subsequently impregnated with lower'melting point metal, such as lead.
Figures 5 to 8 inclusive illustrate the steps in a process of making ring-like sections 3| which can be welded together to form a shell body as shown in Figure 9. According to this process the metal powders 32 are charged into a circular die 33 The desired number of rings 3| are welded together by resistance welding in the welding ma-.
chine 38 shown diagrammatically in Figure 9. First a, ring 39 which has no welding projection is placed on the lower electrode 40 of the machine and a ring 3| is laid, ridge 36 down, on top of' it. Upper electrode 4| is brought down to clamp the two rings between them and-after sufficient pressure has been applied electric current is applied through conductors 42. Since ridge 36 has the smallest cross section and hence highest resistance in the circuit it is fused by the electric current, spreading out and welding the rings together. Further rings 3| are added, one at a time, in like manner, the rings being-aligned and guided by guide ring 43 supported by the machine. In fact the whole operation of feeding, aligning and welding may be almost wholly automatic.
Instead of providing integral welding ridges 36 on rings 3|, a. series of separate welding rings of reduced cross section may be used interspersed with a series of flat rings 39, the welding proceeding in the same manner.
Figures 10 and 11 illustrate an automatic appa- I ratus and method for assembly and furnace brazing of shell bodies. Pressed powder rings 39 (having notches 31- if desired) are stacked in hopper 44 of the assembling machine of Figure 10 and thin rings 45 of brazing metal in hopper 46. A pair of automatic pusher arms 41 and 48 shove one of the rings 39 and 46 alternately into a third hopper 49 to form a stack of alternate rings 39 and 45. When a stack of the desired height is completed the truck on which the stack is formed is released and rolls into furnace 5| of Figure 11 where the rings are brazed together in a unitary assembly. Nose pieces 52 may be added on top of each stack in the assembling machine all of one composition or different segments may,
in some cases be made of difierent composition. The resistance welded, sinter bonded, brazed, impregnated or otherwise bonded projectile may be given a coining, broaching, pressing or shaping operation to bring the projectile to within the desired degree of accuracy.
While the present invention, as to its objects and advantages, has been described herein as carried out in specific embodiments thereof, it is not desired to be limited thereby but it is intended to cover the invention broadly within the spirit and scope of the appended claims.
What is claimed is:
1. The method of making a shell body which comprises forming a plurality of individual sections, a, plurality of said sections comprising compact bonded masses of metal powders, assembling said sections in contiguous relation and immersing the assembly in a body of molten metal of lower melting point than the metals of said sections, to impregnate said metal powder sections withsaid molten metal and bond said sections together.
2. A shell body formed at least in part of a compact mass of ferrous metal powders interspersed with an impregnating metal of lower melting point than said powders and selected from the group consisting of lead and alloys thereof, babbitt, copper alloys, silver alloys, zinc base alloys, tin base alloys and cadmium base alloys.
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JPS54112803U (en) * 1978-01-30 1979-08-08
EP0113833A2 (en) * 1983-01-18 1984-07-25 Rheinmetall GmbH Projectile with explosive and incendiary action
EP0143775A2 (en) * 1983-11-23 1985-06-05 VOEST-ALPINE Aktiengesellschaft Sub-calibre penetrator and method of making the same
FR2619900A1 (en) * 1987-08-26 1989-03-03 Stribling Gerald Non-explosive projectile for fighting against lightweight targets
US4899661A (en) * 1988-02-18 1990-02-13 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Projectile containing a fragmentation jacket
EP0779966A2 (en) * 1995-06-07 1997-06-25 Lockheed Martin Energy Systems, Inc. Non-lead, environmentally safe projectiles and explosives containers
US6565988B1 (en) * 1999-05-21 2003-05-20 Plansee Aktiengesellschaft Composite for high thermal stress
EP1367357A1 (en) * 2002-05-31 2003-12-03 Giat Industries Fragmenting hull and war head ammunition comprising such a hull
US20080047458A1 (en) * 2006-06-19 2008-02-28 Storm Roger S Multi component reactive metal penetrators, and their method of manufacture
US10415939B2 (en) * 2014-03-14 2019-09-17 Hirtenberger Defence Europe GmbH Projectile

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US2577187A (en) * 1946-08-12 1951-12-04 North American Aviation Inc Method of forming bearings
US2504509A (en) * 1947-10-10 1950-04-18 Gen Motors Corp Method of repairing damaged sheet metal
US2714556A (en) * 1950-11-25 1955-08-02 Sintercast Corp America Powder metallurgical method of shaping articles from high melting metals
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
US2706693A (en) * 1951-02-10 1955-04-19 Allied Prod Corp Process of impregnating metal bearings
US2721378A (en) * 1951-06-11 1955-10-25 Birmingham Small Arms Co Ltd Process for manufacture of porous structure
US2719095A (en) * 1951-06-13 1955-09-27 American Electro Metal Corp Production of corrosion-resistant coatings on copper infiltrated ferrous skeleton bodies
US2819515A (en) * 1951-06-26 1958-01-14 Thompson Prod Inc Method of making a blade
US2706759A (en) * 1951-07-14 1955-04-19 Gibson Electric Company Refractory contacts
US2741828A (en) * 1951-08-31 1956-04-17 Isthmian Metals Inc Composite metal structure
US2725265A (en) * 1951-11-26 1955-11-29 Thompson Prod Inc Valve stem guides
US2694126A (en) * 1952-02-28 1954-11-09 Westinghouse Electric Corp Electrical contact member
US2753859A (en) * 1952-03-07 1956-07-10 Thompson Prod Inc Valve seat insert
US2805624A (en) * 1952-03-11 1957-09-10 Olin Mathieson Metallurgical process
US2807437A (en) * 1952-05-01 1957-09-24 Thompson Prod Inc Method for making intricate hollow powder metal parts
US2753858A (en) * 1952-05-27 1956-07-10 Thompson Prod Inc Valve seat insert ring
US2756492A (en) * 1952-09-13 1956-07-31 Eaton Mfg Co Manufacture of composite ductile wire
US2814100A (en) * 1953-01-02 1957-11-26 Ohio Commw Eng Co Method of sealing a port in a glass object
US2775024A (en) * 1953-05-29 1956-12-25 Thompson Prod Inc Powder metal multi-ring bushing
US2968091A (en) * 1954-01-29 1961-01-17 American Can Co Method of applying solder to a joint
US2856856A (en) * 1955-06-02 1958-10-21 Louis S Michael Segmented rotating band for artillery projectiles
US2960754A (en) * 1955-11-09 1960-11-22 Erie Resistor Corp Network assembly method
US3026806A (en) * 1957-03-22 1962-03-27 Russell Mfg Co Ballistic missile nose cone
US3027694A (en) * 1959-06-15 1962-04-03 B H Hadley Packaging rectangular objects and embedding them in a matrix
US3026804A (en) * 1959-12-28 1962-03-27 B H Hadley Shrapnel packaging
US3224071A (en) * 1960-03-14 1965-12-21 Philips Corp Brazing method for porous bodies
US3170228A (en) * 1960-04-25 1965-02-23 Carrier Corp Method of making heat exchangers
DE1205292B (en) * 1960-05-17 1965-11-18 Plansee Metallwerk Refractory metal susceptors for induction furnaces and processes for their manufacture
US3353249A (en) * 1964-03-25 1967-11-21 Westinghouse Air Brake Co Method of making a fabricated valve bushing
US3373003A (en) * 1965-04-01 1968-03-12 Siemens Ag Multi-layer bonded metal structure
US3499739A (en) * 1966-04-27 1970-03-10 Franklin Mint Inc Bimetallic token with annular ring having different permeability than inner portion
US3466166A (en) * 1967-01-03 1969-09-09 Gen Electric Method for making a hollow metal article
US3779715A (en) * 1970-01-15 1973-12-18 Permanence Corp Heat resistant high strength composite structure of hard metal particles in a matrix, and method of making the same
US3717442A (en) * 1971-05-17 1973-02-20 Johnson & Co Inc A Brazing alloy composition
US3848307A (en) * 1972-04-03 1974-11-19 Gen Electric Manufacture of fluid-cooled gas turbine airfoils
JPS54112802U (en) * 1978-01-30 1979-08-08
JPS54112803U (en) * 1978-01-30 1979-08-08
JPS5831895Y2 (en) * 1978-01-30 1983-07-14 三菱マテリアル株式会社 Insoluble anode made of sintered material for metal electroplating
JPS5831896Y2 (en) * 1978-01-30 1983-07-14 三菱マテリアル株式会社 Insoluble anode made of sintered material for metal electroplating
EP0113833A3 (en) * 1983-01-18 1985-05-15 Rheinmetall Gmbh Projectile with explosive and incendiary action
EP0113833A2 (en) * 1983-01-18 1984-07-25 Rheinmetall GmbH Projectile with explosive and incendiary action
US4662280A (en) * 1983-01-18 1987-05-05 Rheinmetal Gmbh Explosive and incendiary projectile
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
FR2619900A1 (en) * 1987-08-26 1989-03-03 Stribling Gerald Non-explosive projectile for fighting against lightweight targets
US4899661A (en) * 1988-02-18 1990-02-13 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Projectile containing a fragmentation jacket
EP0779966A2 (en) * 1995-06-07 1997-06-25 Lockheed Martin Energy Systems, Inc. Non-lead, environmentally safe projectiles and explosives containers
EP0779966A4 (en) * 1995-06-07 1998-07-22 Lockheed Martin Energy Sys Inc Non-lead, environmentally safe projectiles and explosives containers
US6565988B1 (en) * 1999-05-21 2003-05-20 Plansee Aktiengesellschaft Composite for high thermal stress
EP1367357A1 (en) * 2002-05-31 2003-12-03 Giat Industries Fragmenting hull and war head ammunition comprising such a hull
FR2840402A1 (en) * 2002-05-31 2003-12-05 Giat Ind Sa ENCLOSURE GENERATING CHIPS, EXPLOSIVE CHARGE AND AMMUNITION IMPLEMENTING SUCH AN ENVELOPE
US20080047458A1 (en) * 2006-06-19 2008-02-28 Storm Roger S Multi component reactive metal penetrators, and their method of manufacture
US8573128B2 (en) * 2006-06-19 2013-11-05 Materials & Electrochemical Research Corp. Multi component reactive metal penetrators, and their method of manufacture
US10415939B2 (en) * 2014-03-14 2019-09-17 Hirtenberger Defence Europe GmbH Projectile
US10648783B2 (en) 2014-03-14 2020-05-12 Hirtenberger Defence Europe GmbH Projectile

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