US3199331A - Process for the extrusion of ultra-fine wires - Google Patents
Process for the extrusion of ultra-fine wires Download PDFInfo
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- US3199331A US3199331A US267208A US26720863A US3199331A US 3199331 A US3199331 A US 3199331A US 267208 A US267208 A US 267208A US 26720863 A US26720863 A US 26720863A US 3199331 A US3199331 A US 3199331A
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- 238000001125 extrusion Methods 0.000 title claims description 58
- 238000000034 method Methods 0.000 title claims description 31
- 229910052751 metal Inorganic materials 0.000 claims description 65
- 239000002184 metal Substances 0.000 claims description 65
- 239000011159 matrix material Substances 0.000 claims description 49
- 239000002245 particle Substances 0.000 claims description 33
- 239000000843 powder Substances 0.000 claims description 29
- 239000006185 dispersion Substances 0.000 claims description 22
- 239000000203 mixture Substances 0.000 claims description 15
- 238000010438 heat treatment Methods 0.000 claims description 8
- 239000000463 material Substances 0.000 description 28
- 229910045601 alloy Inorganic materials 0.000 description 19
- 239000000956 alloy Substances 0.000 description 19
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 12
- 150000002739 metals Chemical class 0.000 description 7
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 6
- 239000010410 layer Substances 0.000 description 5
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 229910003460 diamond Inorganic materials 0.000 description 4
- 239000010432 diamond Substances 0.000 description 4
- 239000011261 inert gas Substances 0.000 description 4
- 150000001247 metal acetylides Chemical class 0.000 description 4
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052786 argon Inorganic materials 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- 239000011872 intimate mixture Substances 0.000 description 3
- 230000001590 oxidative effect Effects 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
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- 238000005266 casting Methods 0.000 description 2
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- 238000005121 nitriding Methods 0.000 description 2
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- 238000004881 precipitation hardening Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 238000004857 zone melting Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
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- 238000000137 annealing Methods 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 238000005256 carbonitriding Methods 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 238000010622 cold drawing Methods 0.000 description 1
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- 230000005494 condensation Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 239000012153 distilled water Substances 0.000 description 1
- 235000012438 extruded product Nutrition 0.000 description 1
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- 239000007788 liquid Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
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- 238000005272 metallurgy Methods 0.000 description 1
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- 238000002360 preparation method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 238000005491 wire drawing Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/02—Making uncoated products
- B21C23/04—Making uncoated products by direct extrusion
- B21C23/08—Making wire, bars, tubes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/20—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by extruding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/12—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of wires
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S72/00—Metal deforming
- Y10S72/70—Deforming specified alloys or uncommon metal or bimetallic work
Definitions
- Hcretc-fore production of ultrafine wires been achieved by drawing processes whereby the metal or alloy is drawn through a hole in a plate or block of hard-e material known as a die. This operation converts the starting material, a rod, for example, to an elongated product of reduced cross-section.
- the drawing process is re- ,eated using dies with smal er holes until the desired reduction in area and cross-section is obtained.
- the wire drawing process while effective to produce wires, is accompanied by numerous disadvantages.
- the billet container With respect to pick-up on the inner surface of the billet container, when the billet material is held and extruded from a billet container having an oxidized, nitrided or carbonitrided inner surface adjacent the billet material, pick-up on the billet container surface is eliminated.
- the oxidized-nitrided or carbonitrided surface provides a surface which is substantially nonreactive with the extrusion material; that is, the extrusion material will not weld, alloy or react with the treated surface.
- the oxidizing, carbonitriding or nitriding of the billet container may be carried out by methods well known by those skilled in the art.
- Heating member 12 containing heating coils IA surrounds the extrusion container lit and heats the extrusion material 16 by radiation to the desired initial temperature.
- a suitable closure disc 28 Positioned between the ram and the extrusion material is a suitable closure disc 28.
- the ram 18 is advanced against the extrusion material by mechanical or hydraulic means not shown to express the billet material through the die 24, and extrude the ultrafine wire
- the extruded wire is preferably collected on an automatically driven spool not shown.
- Appropriate means (not shown) may be employed for maintaining a nonoxidizing inert atmosphere within or about the extrusion chamber as taose skilled in the art will readily understand.
- a principal object of the iresent invention is to provide a process of producing dispersion strengthened ultrafine wires by extrusion.
- Another object or" the present invention is to provide extruded dispcrsion-strengthened or hardened wires having diameters of less than about 10 mils (.01 inch).
- a further object of the present invention is to provide a dispersion-strengthened ultrafine wire extrusion process which is effective in producing a more economic product than heretofore possible.
- the invention accordingly comprises the product possessing the features, proper ies and the relation of components and the process involving the several steps and the relation and order of one or more of such steps with respect to each of the others which are exemplified in the following detailed disclosure and the scope of the appiication of which will be indicated in the claims.
- an intimate mixture of a matrix metal and a dispersion strengthening material is introduced into an extrusion billet container and then heated to an initial temperature at which the compressive flow stress of the matrix metal is about 10-25 percent of the room temperature value.
- con pressive flow stress is meant the value of strain or con1- pression required to cause plastic deformation.
- the heated mix is then expressed through the die opening at a sui ficient rate to further heat the mix by internal friction of deformation to a temperature which is in excess of the initial temperature and below the solidus temperature of the matrix metal.
- solidus temperature as used in the specification and claims, is intended to include in its scope the melting point of the matrix metals or the temperature of appearance of the first liquid for a matrix alloy when the matrix alloy is slowly heated. In this manner an ultrafine dispersion strengthened wire is produced.
- the extrusion is carried out under a non-oxidizing atmosphere.
- the extrusion may be carried out under an atmosphere of inert gas such as argon.
- the intimate mixture of the matrix metal and the dispersion material is prepared by blending powders of the metal and dispersion material. The powder mix is then extruded to form a dispersion strengthened ultrafine wire.
- the matrix metal powder can be prepared for example by such methods as atomization, comminution, and vapor condensation.
- the metal powder is prepared in accordance with US. Patent 3,049,421 to L. R. Allen et al.
- the principal requirements of the matrix metal powder is that the metal powder be free of inclusions such as graphite, carbides, oxides and dirt having a particle size in excess of 20 percent of the diameter of the wire to be extruded.
- the particle size of inclusions must be less than 20 percent, and preferably less than 10 percent, of the wire diameter, it is to be understood that it is preferable that the metal powder be free of inclusions.
- the alloy power is prepared or treated to provide an alloy power having a particle size of the second phase or intermetallic harder constituents of less than 20 percent of the product wire diameter.
- the dispersion material can be prepared by the same methods as described for the preparation of the matrix metal powder.
- dispersion materials powders of metals, metallic compounds, alloys, oxides, carbides and nitrides, for example, are suitable.
- the principal requirements of the dispersion powders are that they have a particle size of less than 20 percent, and preferably less than percent, of the wire diameter to permit extrusion of the ultrafine wire, that they have a low or zero solubility with respect to the matrix metal and that they have a higher hot hardness or strength than the matrix metal. 7 1
- the intimate mixture of matrix metal and the dispersion material is provided by treating the matrix metal powder to form a thin skin or surface layer of the dispersion material on the metal powder.
- the surface of the metal powder is coated, plated, oxidized, carburized, or nitn'ded, for example, to provide a thin layer of the dispersion compound on the powder particles.
- the coating, plating, oxidizing, carburizing and nitriding can be carried out by methods well known by those skilled in the art.
- the layer or coating of the dispersion material on the metal power is broken during the extrusion so that the metal powder becomes the continuous metal matrix and the dispersion coating or skin becomes the dispersed phase.
- fine powder particles are preferred to coarse powder particles. Finer powdeparticles provide more homogeneous mixtures with uniform spacing of the dispersed material in the matrix metal. Additionally finer powder particles provide smaller interparticle spacing between the dispersed phase particles which, for example, impede deformation on working. In this manner greater strength is achieved in the extruded ultrafine wire.
- the dispersed phase particle size is on the order of .1 micron to .001 micron and preferably less than .05 micron.
- the invention is not to be limited to the size of the particles for the matrix metal and that a particle size may be selected, depending on the degree of strengthening desired in the extruded wire and the extrusion ratio, since a larger particle requires a larger extrusion ratio to give a wire of equivalent strength.
- FIG. 10 illustrates a diagrammatic, fragmentary, sectional View of a direct vertical extrusion apparatus of the'type used in practicing the present invention.
- the drawing 10 represents the billet or extrusion container having a /2 inch inner diameter bore.
- the inner surface of the extrusion container 10 is oxidized, nitrided or carbonitrided to provide a layer 11 which is nonreactive to extrusion material 16 which is shown as a powder mix.
- the matrix metal powder to be extruded must be free of hard particles in excess of 20 percent, and preferably less than 10 percent of the diameter of ultrafine wire to be extruded.
- hard particle as used in the specification and claims is meant inclusions such as graphite, carbides,
- intermetallic particles such as intermetallic compounds or hard second phases which are present in certain alloys.
- the non-intentional hard particle inclusions are removed by zone melting techniques which are familiar to those skilled in the art.
- the metal to be extruded or the metals which form the alloy to be extruded are zone melted to remove inclusions having a particle size in excess of 20 percent of the diamture interval for extrusion.
- the zone melting is carried out in vacuum or in a clean atmosphere of inert gas such as argon or under a suitable flux.
- the inclusions in the matrix metal are removed by filtration techniques;
- the heated molten metal is passed through a ceramic or stainless steel sieve of suitable mesh orifice size to filter out the inclusions.
- the filtration is carried out in vacuum or a clean atmosphere of inert gas.
- the matrix metal free of hard particles is then comminuted to powder under non-contaminating conditions.
- the particle size of intermetallic particles may be reduced by rapidly cooling the alloy from a molten condition.
- the molten alloy is poured in a stream through a stainless steel or ceramic screen into a container of distilled water.
- the molten alloy is rapidly cooled and formed into shot in which the intermetallic particle size is reduced to less than about 5 microns.
- the screen serves to form equal streams of the molten alloy which upon introduction into the water are rapidly cooled and formed into shot.
- the heating and pouring is carried out under clean atmosphere of a non-reactive inert gas such as argon or nitrogen.
- the alloy is heated and the molten alloy poured into a heavy walled chill mold such as copper or graphite to rapidly cool the molten alloy.
- a heavy walled chill mold such as copper or graphite
- the mold is cooled by a coolant such as water although other cooling media may be employed.
- the heating, pouring and casting is preferably carried out under vacuum. In this manner, the intermetallic particle size of less than about 25 microns can be achieved.
- the casting is then comminuted to the desired particle size under non-contaminating conditions.
- one of the important features is that of maintaining the temperature of the matrix metal being extruded within the abovementioned temperature interval: that is, between the initial temperature and the solidus temperature in order to obtain continuous uniform extrusion of ultrafine wire. It has been determined that once the particular matrix metal to be extruded has been heated to the initial temperature the temperature to which themetal will be raised during the extrusion due to the heat of deformation will be controlled by the extrusion rate and hence the ram speed.
- the billet material be extruded through a sharp or shearing-edged orifice in a die having a flat surface adjacent the billet material; that is to say the surface of the die against which the billet material is placed should not have any coning or tapering lead-in surface or rounded edge to the die orifice.
- the extrusion can be carried out at lower pressures which permit higher extrusion rates of the wire.
- the internal frictional heating of the billet material at the point of maximum deformation can be sufficiently controlled to maintain the proper tempera- Additionally the extrusion can be carried out without exceeding the limiting stresses for the extrusion tool's.
- the ram speed it is to be understood that for a given extrusion rate the ram speed will vary with the extrusion ratio.
- Example 1 In this example the extrusion material consisted of commercial atomized aluminum metal powder having a particle size of about 20 microns. The aluminum metal powder was free of hard particles and had an aluminum oxide coating of 5-10 percent by weight. 45 grams of the oxide coated aluminum powder was then placed in the /2 inch diameter extrusion container and heated to a temperature of 455 C. At this temperature the compressive flow stress of the matrix aluminum metal particles is about 20 percent of the room temperature value. The extrusion mixture was then expressed through a diamond die having an orifice of 0.003 inch diameter at extrusion rates of 100 feet per minute of 0.003 inch wire. The bulk temperature of the extrusion was maintained below about 550 C. Above 550 C.
- the extrusion interrupts itself by splitting molten aluminum at ram speeds as low as 0.1 inch per minute.
- the 0.003 inch diameter wire produced was uniform and was tested for tensile strength.
- the tensile strength of the Wire was 33,500 lbs/sq. inch. This tensile strength compares favorably with aluminum wire having a larger diameter and prepared by normal methods.
- Example 2 In this example the aluminum oxide coated aluminum metal powder of Example 1 was further oxidized by steam treatment at 200 C. to produce a layer of aluminum oxide of about -l5 percent aluminum oxide by Weight. 45 grams of the oxide coated aluminum particles were introduced into the A2 inch diameter extrusion container and heated to a temperature of 500 C. At this temperature the compressive flow stress of the matrix aluminum metal particles is about 12 percent of the room temperature value. The extrusion mixture was then expressed through a diamond die having an orifice of .003 inch diameter at extrusion rates of 100 feet per minute of 0.003 inch wire. The temperature of the extrusion was maintained below about 550 C. The 0.003 inch diameter wire produced was uniform and was tested for tensile strength. The tensile strength of the Wire was 46,250 lbs/sq. inch. This tensile strength compares favorably with aluminum Wire of larger diameter prepared by normal methods.
- Example 1 While preferred embodiments of the invention as practiced with respect to aluminum as the matrix metal have been described in the foregoing examples, the table set forth below is exemplary of the invention as applied to other matrix metals. Included in the table is Example 1.
- dispersion hardened ultrafine metal wire having a diameter of less than about 0.01 inch comprising forming a powder of matrix metal having hard particle sizes of less than 20 percent of said wire diameter, intimately mixing a dispersion hardening material having a particle size of less than 20 percent of said wire diameter with said matrix metal, introducing said mixture into a billet container, heating said mixture to an initial temperature at which the compressive flow stress of said matrix metal is about 1025 percent of the room temperature value, expressing said mixture through a shearing-edged opening in a substantially flat die surface at a sufficient extrusion rate to further heat said mixture to a temperature which is in excess of said initial temperature and below the solidus temperature of said matrix metal to thereby form a dispersion hardened extruded wire.
- the process of producing dispersion hardened ultrafine metal wire having a diameter of less than about .01 inch comprising forming a powder of a matrix metal having hard particle sizes of less than 20 percent of said Wire diameter, treating said matrix metal powder to form thereon a thin layer of a dispersion hardening material selected from the group consisting of metals, metallic compounds, alloys, oxides, carbides, and nitrides, insoluble in said matrix metal, introducing said treated matrix metal into an extrusion container, heating said treated matrix metal to an initial temperature at which the compressor flow stress of said matrix metal is about 10-25 percent of the room temperature value, expressing said mixture through a shearing-edged opening in a substantially fiat die surface at a suflicient extrusion rate to further heat said matrix metal to a temperature which is in excess of said initial temperature and below the solidus temperature of said matrix metal to thereby form a dispersion hardened extruded wire.
- a dispersion hardening material selected from the group consisting of metals, metallic
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- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Aug. 10, 1965 L. R. ALLEN 3,199,331
PROCESS FOR THE EXTRUSION 0F ULTRA-FINE WIRES Filed March 22, 1963 +HHHHHHH4HI H BY Lloy d R United States Patent no F i/ il This invention relates to metallurgy and more particularly to a method of producing dispersion-strengthened ultra-fine wires by extrusion. This application is in part a co tinuation of my c ding applications Serial No. 228,734, filed August 31,1962 and Serial No. 195,62 filed May 17,1962.
Hcretc-fore production of ultrafine wires been achieved by drawing processes whereby the metal or alloy is drawn through a hole in a plate or block of hard-e material known as a die. This operation converts the starting material, a rod, for example, to an elongated product of reduced cross-section. The drawing process is re- ,eated using dies with smal er holes until the desired reduction in area and cross-section is obtained. The wire drawing process, while effective to produce wires, is accompanied by numerous disadvantages. For example, due to the work hardening which takes place during cold drawing the ductility of the metal wire decreases and tensile strength increases with the result that the metal wire produced tends to become hard and brittle and often requires annealing to permit still further reduction to sma ler sizes or diameters. Such drawing processes are relatively slow and add greatly to the cost of the drawn wire. For example, the cost of a series or" dies is quite large.
In the extrusion of metals wherein a heated billet, suitably confined, is expressed through a die orifice, considerable difficulty has been encountered because of the lack of control of such factors as the speed of extrusion, the temperature of extrusion, the extrusion ratio, and the extrusion pressure and llow stress. While various extrusion processes have been successfully practiced in producing extruded products of relatively large dimensions such as rods, tubes, and the like, attempts to apply such known extrusion practice to the production of ultrafine wires have not been generally successful. Consequently, no tech A e or method has been devised for obtaining dispersion strengthened ultrafine wires by extrusion.
With respect to pick-up on the inner surface of the billet container, when the billet material is held and extruded from a billet container having an oxidized, nitrided or carbonitrided inner surface adjacent the billet material, pick-up on the billet container surface is eliminated. The oxidized-nitrided or carbonitrided surface provides a surface which is substantially nonreactive with the extrusion material; that is, the extrusion material will not weld, alloy or react with the treated surface. The oxidizing, carbonitriding or nitriding of the billet container may be carried out by methods well known by those skilled in the art. Heating member 12 containing heating coils IA surrounds the extrusion container lit and heats the extrusion material 16 by radiation to the desired initial temperature. Extending into the extrusion container is a ram 18 which is supported on suitable columns 2 3. The extrusion container ll) is supported on die holder 22 and is provided with a shearing-edged flat diamond die 24 and die backup adapter ring 26. Pick-up on the die bearing surface is greatly reduced or eliminated when the metal is expressed through a diamond die.
Positioned between the ram and the extrusion material is a suitable closure disc 28. The ram 18 is advanced against the extrusion material by mechanical or hydraulic means not shown to express the billet material through the die 24, and extrude the ultrafine wire The extruded wire is preferably collected on an automatically driven spool not shown. Appropriate means (not shown) may be employed for maintaining a nonoxidizing inert atmosphere within or about the extrusion chamber as taose skilled in the art will readily understand.
A principal object of the iresent invention is to provide a process of producing dispersion strengthened ultrafine wires by extrusion.
Another object or" the present invention is to provide extruded dispcrsion-strengthened or hardened wires having diameters of less than about 10 mils (.01 inch).
A further object of the present invention is to provide a dispersion-strengthened ultrafine wire extrusion process which is effective in producing a more economic product than heretofore possible.
Other objects of the invention will in part be obvious and will in part appear hereinafter.
The invention accordingly comprises the product possessing the features, proper ies and the relation of components and the process involving the several steps and the relation and order of one or more of such steps with respect to each of the others which are exemplified in the following detailed disclosure and the scope of the appiication of which will be indicated in the claims.
F or a fuller understanding of the nature and objects of the invention reference should be had to the following detailed description taken in connection with the accompanying drawing which is a diagrammatic, fra mentary sectional view of an extrusion apparatus for practicing the present invention.
in accordance with the present invention an intimate mixture of a matrix metal and a dispersion strengthening material is introduced into an extrusion billet container and then heated to an initial temperature at which the compressive flow stress of the matrix metal is about 10-25 percent of the room temperature value. By con pressive flow stress is meant the value of strain or con1- pression required to cause plastic deformation. The heated mix is then expressed through the die opening at a sui ficient rate to further heat the mix by internal friction of deformation to a temperature which is in excess of the initial temperature and below the solidus temperature of the matrix metal. The term solidus temperature, as used in the specification and claims, is intended to include in its scope the melting point of the matrix metals or the temperature of appearance of the first liquid for a matrix alloy when the matrix alloy is slowly heated. In this manner an ultrafine dispersion strengthened wire is produced. Preferably the extrusion is carried out under a non-oxidizing atmosphere. For example, the extrusion may be carried out under an atmosphere of inert gas such as argon.
In one preferred embodiment of the present invention the intimate mixture of the matrix metal and the dispersion material is prepared by blending powders of the metal and dispersion material. The powder mix is then extruded to form a dispersion strengthened ultrafine wire.
In this embodiment the matrix metal powder can be prepared for example by such methods as atomization, comminution, and vapor condensation. In one preferred embodiment of the present invention the metal powder is prepared in accordance with US. Patent 3,049,421 to L. R. Allen et al. The principal requirements of the matrix metal powder is that the metal powder be free of inclusions such as graphite, carbides, oxides and dirt having a particle size in excess of 20 percent of the diameter of the wire to be extruded. Although the particle size of inclusions must be less than 20 percent, and preferably less than 10 percent, of the wire diameter, it is to be understood that it is preferable that the metal powder be free of inclusions. Further, where the metal to be extruded is an alloy powder, the alloy power is prepared or treated to provide an alloy power having a particle size of the second phase or intermetallic harder constituents of less than 20 percent of the product wire diameter.
In this embodiment of the invention, the dispersion material can be prepared by the same methods as described for the preparation of the matrix metal powder. As dispersion materials, powders of metals, metallic compounds, alloys, oxides, carbides and nitrides, for example, are suitable. The principal requirements of the dispersion powders are that they have a particle size of less than 20 percent, and preferably less than percent, of the wire diameter to permit extrusion of the ultrafine wire, that they have a low or zero solubility with respect to the matrix metal and that they have a higher hot hardness or strength than the matrix metal. 7 1
In another preferred embodiment of the present invention, the intimate mixture of matrix metal and the dispersion material is provided by treating the matrix metal powder to form a thin skin or surface layer of the dispersion material on the metal powder. In this embodiment of the invention, the surface of the metal powder is coated, plated, oxidized, carburized, or nitn'ded, for example, to provide a thin layer of the dispersion compound on the powder particles. The coating, plating, oxidizing, carburizing and nitriding can be carried out by methods well known by those skilled in the art. In accordance with this embodiment, the layer or coating of the dispersion material on the metal power is broken during the extrusion so that the metal powder becomes the continuous metal matrix and the dispersion coating or skin becomes the dispersed phase.
With respect to the particle size of the dispersion material, fine powder particles are preferred to coarse powder particles. Finer powdeparticles provide more homogeneous mixtures with uniform spacing of the dispersed material in the matrix metal. Additionally finer powder particles provide smaller interparticle spacing between the dispersed phase particles which, for example, impede deformation on working. In this manner greater strength is achieved in the extruded ultrafine wire. Preferably the dispersed phase particle size is on the order of .1 micron to .001 micron and preferably less than .05 micron. It is to be understood that the invention is not to be limited to the size of the particles for the matrix metal and that a particle size may be selected, depending on the degree of strengthening desired in the extruded wire and the extrusion ratio, since a larger particle requires a larger extrusion ratio to give a wire of equivalent strength.
Reference will now be made to the drawing which illustrates a diagrammatic, fragmentary, sectional View of a direct vertical extrusion apparatus of the'type used in practicing the present invention. In the drawing 10 represents the billet or extrusion container having a /2 inch inner diameter bore. The inner surface of the extrusion container 10 is oxidized, nitrided or carbonitrided to provide a layer 11 which is nonreactive to extrusion material 16 which is shown as a powder mix.
As discussed hereinbefore, in order to obtain uniform continuous extrusion of ultrafine wire, the matrix metal powder to be extruded must be free of hard particles in excess of 20 percent, and preferably less than 10 percent of the diameter of ultrafine wire to be extruded. By
the term hard particle as used in the specification and claims is meant inclusions such as graphite, carbides,
oxides, dirt and other foreign impurities and/or intermetallic particles such as intermetallic compounds or hard second phases which are present in certain alloys.
In one preferred embodiment of the present invention, the non-intentional hard particle inclusions are removed by zone melting techniques which are familiar to those skilled in the art. In this embodiment of the invention the metal to be extruded or the metals which form the alloy to be extruded are zone melted to remove inclusions having a particle size in excess of 20 percent of the diamture interval for extrusion.
eter of the ultrafine wire. Preferably the zone melting is carried out in vacuum or in a clean atmosphere of inert gas such as argon or under a suitable flux.
In another preferred embodiment of this aspect of the invention, the inclusions in the matrix metal are removed by filtration techniques; In this embodiment of the invention the heated molten metal is passed through a ceramic or stainless steel sieve of suitable mesh orifice size to filter out the inclusions. Preferably the filtration is carried out in vacuum or a clean atmosphere of inert gas.
The matrix metal free of hard particles is then comminuted to powder under non-contaminating conditions.
With respect to alloys the particle size of intermetallic particles may be reduced by rapidly cooling the alloy from a molten condition. In one preferred embodiment of the present invention the molten alloy is poured in a stream through a stainless steel or ceramic screen into a container of distilled water. In this maner the molten alloy is rapidly cooled and formed into shot in which the intermetallic particle size is reduced to less than about 5 microns. The screen serves to form equal streams of the molten alloy which upon introduction into the water are rapidly cooled and formed into shot. Preferably the heating and pouring is carried out under clean atmosphere of a non-reactive inert gas such as argon or nitrogen.
In another preferred embodiment of this aspect of the invention the alloy is heated and the molten alloy poured into a heavy walled chill mold such as copper or graphite to rapidly cool the molten alloy. Preferably the mold is cooled by a coolant such as water although other cooling media may be employed. The heating, pouring and casting is preferably carried out under vacuum. In this manner, the intermetallic particle size of less than about 25 microns can be achieved. The casting is then comminuted to the desired particle size under non-contaminating conditions.
In accordance with the present invention one of the important features is that of maintaining the temperature of the matrix metal being extruded within the abovementioned temperature interval: that is, between the initial temperature and the solidus temperature in order to obtain continuous uniform extrusion of ultrafine wire. It has been determined that once the particular matrix metal to be extruded has been heated to the initial temperature the temperature to which themetal will be raised during the extrusion due to the heat of deformation will be controlled by the extrusion rate and hence the ram speed.
One important aspect of the present invention is that the billet material be extruded through a sharp or shearing-edged orifice in a die having a flat surface adjacent the billet material; that is to say the surface of the die against which the billet material is placed should not have any coning or tapering lead-in surface or rounded edge to the die orifice. By extruding the billet material through this type of die the extrusion can be carried out at lower pressures which permit higher extrusion rates of the wire. Thus the internal frictional heating of the billet material at the point of maximum deformation can be sufficiently controlled to maintain the proper tempera- Additionally the extrusion can be carried out without exceeding the limiting stresses for the extrusion tool's. With respect to the ram speed it is to be understood that for a given extrusion rate the ram speed will vary with the extrusion ratio.
The invention will now be described by way of the following non-limiting examples:
Example 1 In this example the extrusion material consisted of commercial atomized aluminum metal powder having a particle size of about 20 microns. The aluminum metal powder was free of hard particles and had an aluminum oxide coating of 5-10 percent by weight. 45 grams of the oxide coated aluminum powder was then placed in the /2 inch diameter extrusion container and heated to a temperature of 455 C. At this temperature the compressive flow stress of the matrix aluminum metal particles is about 20 percent of the room temperature value. The extrusion mixture was then expressed through a diamond die having an orifice of 0.003 inch diameter at extrusion rates of 100 feet per minute of 0.003 inch wire. The bulk temperature of the extrusion was maintained below about 550 C. Above 550 C. the extrusion interrupts itself by splitting molten aluminum at ram speeds as low as 0.1 inch per minute. The 0.003 inch diameter wire produced was uniform and was tested for tensile strength. The tensile strength of the Wire was 33,500 lbs/sq. inch. This tensile strength compares favorably with aluminum wire having a larger diameter and prepared by normal methods.
Example 2 In this example the aluminum oxide coated aluminum metal powder of Example 1 was further oxidized by steam treatment at 200 C. to produce a layer of aluminum oxide of about -l5 percent aluminum oxide by Weight. 45 grams of the oxide coated aluminum particles were introduced into the A2 inch diameter extrusion container and heated to a temperature of 500 C. At this temperature the compressive flow stress of the matrix aluminum metal particles is about 12 percent of the room temperature value. The extrusion mixture was then expressed through a diamond die having an orifice of .003 inch diameter at extrusion rates of 100 feet per minute of 0.003 inch wire. The temperature of the extrusion was maintained below about 550 C. The 0.003 inch diameter wire produced was uniform and was tested for tensile strength. The tensile strength of the Wire was 46,250 lbs/sq. inch. This tensile strength compares favorably with aluminum Wire of larger diameter prepared by normal methods.
While preferred embodiments of the invention as practiced with respect to aluminum as the matrix metal have been described in the foregoing examples, the table set forth below is exemplary of the invention as applied to other matrix metals. Included in the table is Example 1.
Since certain changes may be made in the above products and process without departing from the scope of the invention herein involved, it is intended that all matter contained in the above description, or shown in the accompanying drawings, shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. The process of producing dispersion hardened ultrafine metal wire having a diameter of less than about 0.01 inch comprising forming a powder of matrix metal having hard particle sizes of less than 20 percent of said wire diameter, intimately mixing a dispersion hardening material having a particle size of less than 20 percent of said wire diameter with said matrix metal, introducing said mixture into a billet container, heating said mixture to an initial temperature at which the compressive flow stress of said matrix metal is about 1025 percent of the room temperature value, expressing said mixture through a shearing-edged opening in a substantially flat die surface at a sufficient extrusion rate to further heat said mixture to a temperature which is in excess of said initial temperature and below the solidus temperature of said matrix metal to thereby form a dispersion hardened extruded wire.
2. The process of claim 1 wherein an aluminum matrix is extruded at a temperature between about 400 C. and 550 C.
3. The process of clann 1 wherein a bismuth matrix metal is extruded at a temperature between 225 C. and 255 C.
4. The process of claim 1 wherein a cadmium matrix metal is extruded at a temperature between about 200 C. and 300 C.
5. The process of claim 1 wherein an indium matrix metal is extruded at a temperature between about 25 C. and C.
6. The process of claim 1 wherein a magnesium matrix metal is extruded at a temperature of between about 300 C. and 500 C.
7. The process of claim 1 wherein a zinc matrix metal is extruded at a temperature between about 250 C. and 400 C.
8. The process of claim 1 wherein a lead matrix metal is extruded at a temperature between about 200 C. and 310 C.
9. The process of producing dispersion hardened ultrafine metal wire having a diameter of less than about .01 inch comprising forming a powder of a matrix metal having hard particle sizes of less than 20 percent of said Wire diameter, treating said matrix metal powder to form thereon a thin layer of a dispersion hardening material selected from the group consisting of metals, metallic compounds, alloys, oxides, carbides, and nitrides, insoluble in said matrix metal, introducing said treated matrix metal into an extrusion container, heating said treated matrix metal to an initial temperature at which the compressor flow stress of said matrix metal is about 10-25 percent of the room temperature value, expressing said mixture through a shearing-edged opening in a substantially fiat die surface at a suflicient extrusion rate to further heat said matrix metal to a temperature which is in excess of said initial temperature and below the solidus temperature of said matrix metal to thereby form a dispersion hardened extruded wire.
References Cited by the Examiner UNITED STATES PATENTS 791,096 5/05 Hoopes 29193 988,921 4/11 Abbott 29-193 2,630,623 3/53 Chisholm et a1 207-10 2,686,864 8/54 Wroughton et al. 207-10 2,720,310 10/55 Yaclr 20710 2,738,064 3/56 Kreidler 2071O 2,974,790 3/61 Murphy et al. 207-1.2 3,088,589 5/63 Botes 20710 FOREIGN PATENTS 564,081 9/44 Great Britain.
OTHER REFERENCES Wire and Wire Products, October 1960, vol. 35, No. 10, pp. 1341, 1344, and 1345.
Metals Handbook 1948 ed., published by the American- Society for Metals: Cleveland, p. 975 relied on.
CHARLES W. LANHAM, Primary Examiner.
MICHAEL V. BRINDISI, Examiner.
Claims (1)
1. THE PROCESS OF PRODUCING DISPERSION HARDENED ULTRAFING METAL WIRE HAVING A DIAMETER OF LESS THAN ABOUT 0.01 INCH COMPRISING FORMING A POWDER OF MATRIX METAL HAVING HARD PARTICLE SIZES OF LESS THAN 20 PERCENT OF SAID WIRE DIAMETER, INTIMATELY ,IXING A DISPRESION HARDENING MATERAIL HAVING A PARTICLE SIZE OF LESS THAN 20 PERCENT OF SAID WIRE DIAMETER WITH SAID MATRIX METAL, INTRODUCING SAID MIXTURE INTO A BILLET CONTAINER, HEATING SAID MIXTURE TO AN INITIAL TEMPERATURE AT WHICH THE COMPRESSIVE FLOW STRESS OF SAID MATRIX METAL IS ABOUT 10-25 PERCENT OF THE ROOM TEMPERATURE VALUE, EXPRESSING SAID MIXTURE THROUGH A SHEARING-EDGED OPENING IN A SUBSTANTIALLY FLAT DIE SURFACE AT A SUFFICIENT EXTRUSION RATE TO FURTHER HEAT SAID MIXTURE TO A TEMPERATURE WHICH IS IN EXCESS OF SAID INITIAL TEMPERATURE AND BELOW THE SOLIDUS TEMPERATURE OF SAID MATRIX METAL TO THEREBY FORM A DISPERSION HARDENED EXTRUDED WIRE.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
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US267208A US3199331A (en) | 1963-03-22 | 1963-03-22 | Process for the extrusion of ultra-fine wires |
US418573A US3297415A (en) | 1963-03-22 | 1964-10-16 | Dispersion strengthened ultra-fine wires |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US267208A US3199331A (en) | 1963-03-22 | 1963-03-22 | Process for the extrusion of ultra-fine wires |
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US3199331A true US3199331A (en) | 1965-08-10 |
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US267208A Expired - Lifetime US3199331A (en) | 1963-03-22 | 1963-03-22 | Process for the extrusion of ultra-fine wires |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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US4624706A (en) * | 1985-07-02 | 1986-11-25 | Inco Alloys International, Inc. | Weld wire from extruded nickel containing powder |
WO1992005293A1 (en) * | 1990-09-14 | 1992-04-02 | Alcan International Limited | Extrusion of reinforced composite material |
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US2630623A (en) * | 1948-11-12 | 1953-03-10 | Dow Chemical Co | Method of making a die-expressed article of a magnesium-base alloy |
US2686864A (en) * | 1951-01-17 | 1954-08-17 | Westinghouse Electric Corp | Magnetic levitation and heating of conductive materials |
US2720310A (en) * | 1950-04-03 | 1955-10-11 | Dow Chemical Co | Extrusion of metal |
US2738064A (en) * | 1951-12-29 | 1956-03-13 | Kreidler Alfred | Process for the production of sleeveshaped, specially thin-walled, hollow bodies with one or more strand-like extensions |
US2974790A (en) * | 1958-01-06 | 1961-03-14 | Curtiss Wright Corp | Cross-extrusion process |
US3088589A (en) * | 1959-01-10 | 1963-05-07 | John Robertson Co Inc | Method for continuous extrusion of metals |
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US791096A (en) * | 1904-01-26 | 1905-05-30 | Pittsburgh Reduction Company | Wire. |
US988921A (en) * | 1910-08-02 | 1911-04-04 | Edward L Abbott | Metal plate. |
GB564081A (en) * | 1943-06-04 | 1944-09-12 | Magnesium Elektron Ltd | Improvements in or relating to magnesium base alloys |
US2630623A (en) * | 1948-11-12 | 1953-03-10 | Dow Chemical Co | Method of making a die-expressed article of a magnesium-base alloy |
US2720310A (en) * | 1950-04-03 | 1955-10-11 | Dow Chemical Co | Extrusion of metal |
US2686864A (en) * | 1951-01-17 | 1954-08-17 | Westinghouse Electric Corp | Magnetic levitation and heating of conductive materials |
US2738064A (en) * | 1951-12-29 | 1956-03-13 | Kreidler Alfred | Process for the production of sleeveshaped, specially thin-walled, hollow bodies with one or more strand-like extensions |
US2974790A (en) * | 1958-01-06 | 1961-03-14 | Curtiss Wright Corp | Cross-extrusion process |
US3088589A (en) * | 1959-01-10 | 1963-05-07 | John Robertson Co Inc | Method for continuous extrusion of metals |
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Publication number | Priority date | Publication date | Assignee | Title |
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US4624706A (en) * | 1985-07-02 | 1986-11-25 | Inco Alloys International, Inc. | Weld wire from extruded nickel containing powder |
WO1992005293A1 (en) * | 1990-09-14 | 1992-04-02 | Alcan International Limited | Extrusion of reinforced composite material |
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