USRE31902E - Dispersion strengthened metals - Google Patents
Dispersion strengthened metals Download PDFInfo
- Publication number
- USRE31902E USRE31902E US06/565,342 US56534283A USRE31902E US RE31902 E USRE31902 E US RE31902E US 56534283 A US56534283 A US 56534283A US RE31902 E USRE31902 E US RE31902E
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- United States
- Prior art keywords
- alloy
- atomized
- particles
- metal
- oxide
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- Expired - Lifetime
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- 239000006185 dispersion Substances 0.000 title abstract description 16
- 229910052751 metal Inorganic materials 0.000 title description 42
- 239000002184 metal Substances 0.000 title description 42
- 150000002739 metals Chemical class 0.000 title description 8
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 48
- 239000000956 alloy Substances 0.000 claims abstract description 48
- 239000002245 particle Substances 0.000 claims abstract description 39
- 238000000034 method Methods 0.000 claims abstract description 24
- 230000008569 process Effects 0.000 claims abstract description 19
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 14
- 238000002386 leaching Methods 0.000 claims abstract description 5
- 239000000126 substance Substances 0.000 claims abstract description 5
- 230000001590 oxidative effect Effects 0.000 claims description 13
- 239000001307 helium Substances 0.000 claims description 8
- 229910052734 helium Inorganic materials 0.000 claims description 8
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 8
- 230000006872 improvement Effects 0.000 claims description 6
- 229910052782 aluminium Inorganic materials 0.000 claims description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 238000005728 strengthening Methods 0.000 claims description 5
- 239000007789 gas Substances 0.000 claims description 3
- VHUUQVKOLVNVRT-UHFFFAOYSA-N Ammonium hydroxide Chemical group [NH4+].[OH-] VHUUQVKOLVNVRT-UHFFFAOYSA-N 0.000 claims description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical group O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 claims description 2
- 239000000908 ammonium hydroxide Substances 0.000 claims description 2
- 238000000498 ball milling Methods 0.000 claims description 2
- 229910052802 copper Inorganic materials 0.000 claims description 2
- 239000010949 copper Substances 0.000 claims description 2
- 238000000227 grinding Methods 0.000 claims description 2
- 229910017604 nitric acid Inorganic materials 0.000 claims description 2
- 239000003795 chemical substances by application Substances 0.000 claims 2
- 239000011261 inert gas Substances 0.000 claims 1
- 239000007788 liquid Substances 0.000 claims 1
- 230000003647 oxidation Effects 0.000 abstract description 19
- 238000007254 oxidation reaction Methods 0.000 abstract description 19
- 230000009471 action Effects 0.000 abstract description 2
- 239000000843 powder Substances 0.000 description 16
- 238000000889 atomisation Methods 0.000 description 11
- 239000007800 oxidant agent Substances 0.000 description 10
- 229910044991 metal oxide Inorganic materials 0.000 description 9
- 150000004706 metal oxides Chemical class 0.000 description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 8
- 239000001301 oxygen Substances 0.000 description 8
- 229910052760 oxygen Inorganic materials 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- 239000000203 mixture Substances 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- 229910002065 alloy metal Inorganic materials 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 230000008030 elimination Effects 0.000 description 3
- 238000003379 elimination reaction Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 3
- 238000010791 quenching Methods 0.000 description 3
- 230000000171 quenching effect Effects 0.000 description 3
- 239000003870 refractory metal Substances 0.000 description 3
- 238000010301 surface-oxidation reaction Methods 0.000 description 3
- 229910000881 Cu alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- 235000011114 ammonium hydroxide Nutrition 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000011065 in-situ storage Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 239000002923 metal particle Substances 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000009692 water atomization Methods 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical class [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- JRBRVDCKNXZZGH-UHFFFAOYSA-N alumane;copper Chemical compound [AlH3].[Cu] JRBRVDCKNXZZGH-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052790 beryllium Inorganic materials 0.000 description 1
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 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
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 229910052732 germanium Inorganic materials 0.000 description 1
- GNPVGFCGXDBREM-UHFFFAOYSA-N germanium atom Chemical compound [Ge] GNPVGFCGXDBREM-UHFFFAOYSA-N 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 229910052738 indium Inorganic materials 0.000 description 1
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 1
- 239000011872 intimate mixture Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- 239000010955 niobium Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052762 osmium Inorganic materials 0.000 description 1
- SYQBFIAQOQZEGI-UHFFFAOYSA-N osmium atom Chemical compound [Os] SYQBFIAQOQZEGI-UHFFFAOYSA-N 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 229910052702 rhenium Inorganic materials 0.000 description 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 description 1
- 229910052703 rhodium Inorganic materials 0.000 description 1
- 239000010948 rhodium Substances 0.000 description 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 235000011121 sodium hydroxide Nutrition 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229910052716 thallium Inorganic materials 0.000 description 1
- BKVIYDNLLOSFOA-UHFFFAOYSA-N thallium Chemical compound [Tl] BKVIYDNLLOSFOA-UHFFFAOYSA-N 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
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- 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
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
-
- 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
- C22C1/1078—Alloys containing non-metals by internal oxidation of material in solid state
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/001—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
- C22C32/0015—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C32/00—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
- C22C32/001—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides
- C22C32/0015—Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ with only oxides with only single oxides as main non-metallic constituents
- C22C32/0021—Matrix based on noble metals, Cu or alloys thereof
Definitions
- This invention pertains to an improved process for producing improved dispersion strengthened alloy metal products.
- Dispersion strengthened metal products such as copper dispersion strengthened with aluminum oxide
- Welding electrodes for example, require good electrical and thermal conductivities together with good strength and hardness at elevated temperatures.
- Dispersion strengthening has been recognized in the past as a method for increasing strength and hardness of metals.
- a solid solution alloy comprising a relatively noble matrix metal having relatively low heat or free energy of oxide formation and a solute metal having relatively high negative heat or free energy of oxide formation can be dispersion strengthened by heating the alloy under oxidizing conditions to preferentially oxidize the solute metal. This technique of oxidizing the solute metal to a solute metal oxide is known in the art as in situ internal oxidation or more simply internal oxidation.
- a dilute solid solution alloy powder is obtained by atomizing an alloy melt of matrix metal with a minor amount of solute metal wherein the melt is atomized by nitrogen and collected as powder in water.
- oxygen in the atomization chamber tends to oxidize the solute metal on the surface of the alloy particles.
- a copper-aluminum alloy tends to become oxidized during atomization to form an aluminum oxide film on the particle surfaces.
- Further oxidation of the surface aluminum can occur upon the powder contacting water in the collection tank.
- the hot powder falling into the water generates steam in the atomization chamber which further contributes to the surface oxidation of the alloy particles.
- the accumulative effect of surface oxidation is the formation of a relatively thick aluminum oxide film on the surface of the alloy particles.
- the surface oxide film formed on the alloy particles remains intact and can be detrimental in subsequent internal oxidation by forming a barrier to internal oxidation.
- Subsequent processing can inhibit interparticle bonding during subsequent fabrication of the powder into compacted fully dense parts obtained, for example, by hot forging and rolling.
- the final product can be weak and brittle.
- the powder particles tend to stretch out into elongated fibers thus improving interparticle bonding, although surface oxide film has been found to remain on fiber interfaces and causes diminished mechanical properties due to improper and incomplete interparticle or interfiber bonding.
- Elimination of the surface oxide has been found to substantially improve the mechanical properties of the dispersion strengthened alloy such as stress rupture strength as well as substantially improve the internal oxidation step for dispersion strengthening alloys.
- the surface oxide forms a barrier to the diffusion of oxygen into the alloy particles and, therefore, elimination of the surface oxide provides efficient, uniform, and effective oxidation of higher solute metal alloys.
- Significant improvements in the properties of internally oxidized alloys can be achieved by atomizing alloys in helium and collecting the alloy powder dry.
- the process for dispersion strengthening of alloy metal can be substantially improved by the elimination of the surface oxide build-up on the alloy metal particles by preventing the oxide surface formation or by removing the oxide build-up prior to the step of internal oxidation.
- the improved process comprises atomization of alloy metal and eliminating the surface oxide by preventing oxide build-up or by removing the oxide prior to the step of internal oxidation and forming consolidated dispersion strengthened metals.
- the powdered alloy comprising a relatively noble matrix metal and a solute metal is produced by conventional techniques such as melting the metal under inert or reducing conditions and thereafter comminuting the alloy by atomization to form a particulate alloy having an average particle size of less than about 300 microns.
- Water atomization of molten metal alloys is shown in U.S. Pat. No. 2,956,304 wherein metal particles are produced at particularly small particle sizes less than about 100 mesh. Water atomization similarly causes considerable surface oxidation of alloy particles due to the high temperatures of molten metal as well as the oxidizing characteristics of the water itself.
- the noble matrix metal in the alloy can be defined broadly as those metals having a melting point of at least about 200° C. and whose oxides have a negative free energy of formation at 25° C. of from 0 to 70 kilocalories per gram atom of oxygen.
- Suitable alloy matrix metals include, for example, iron, cobalt, nickel, copper, cadmium, thallium, germanium, tin, lead, antimony, bismuth, molybdenum, tungsten, rhenium, indium, palladium, osmium, platinum, and rhodium as more particularly set forth in U.S. Pat. No. 3,779,714.
- the matrix metal In any particular combination of matrix metal and solute metal in the alloy to be dispersion strengthened by internal oxidation, the matrix metal must be relatively noble with respect to the solute metal so that the solute metal will be preferentially oxidized. This is achieved by selecting the solute metal such that its negative free energy of oxide formation at 25° C. is at least 60 kilocalories per gram atom of oxygen greater than the negative free energy of formation of the oxide of the matrix metal at 25° C. Such solute metals have a negative free energy of oxide formation per gram atom of oxygen of over 80 kilocalories and generally over 120 kilocalories.
- Suitable alloy solute metals include: silicon, titanium, zirconium, aluminum, beryllium, thorium, chromium, magnesium, manganese, niobium, tantalum, and vanadium (VO), as more particularly set forth in U.S. Pat. No. 3,779,714.
- atomized alloy particles substantially free of oxide surface film are internally oxidized to form dispersion-strengthened metal.
- atomized alloy particles are processed to remove the oxide build-up on the particle surface formed during atomization.
- the surface oxide film can be mechanically removed such as by milling, grinding or roll flaking the atomized alloy particles.
- Ballmilling for example, can be used at a 4:1 to 8:1 ratio of ball/metal for 2 to 8 hours.
- Roll flaking can be used to reduce thickness of the atomized particles as well as remove oxide films which are believed to break up and/or redistribute the surface oxide over a larger surface area generated by the flaking of spherical powder. Flakes have larger surface:volume ratio than spheres of same volume.
- the surface oxide film can be removed by chemical action such as leaching.
- atomized copper alloy powder can be leached in dilute nitric acid, ammonium hydroxide and also in mixtures of ammonium and sodium hydroxides.
- a further method of preventing surface oxide build-up on the atomized alloy particles pertains to collecting the alloy powder in a dry medium and avoid wet collection mediums such as water. Dry collection within helium, for instance, prevents contact with an oxidizing substance as well as avoids steam formation within the atomization chamber.
- Helium is substantially better than nitrogen in that the thermal conductivity thereof is 6.5 times that of nitrogen whereby much faster quenching, without appreciable oxidation, can be achieved.
- Helium quenching enables faster quenching of the atomized particles, thus minimizing oxidation of the solute metal such as aluminum at the particle surface and further minimizes migration of solute metal from the center of the alloy particle to the particle surface which can detrimentally deplete the alloy particle of solute metal.
- the alloy particles being substantially free of surface oxide build-up can be internally oxidized by a variety of methods such as disclosed in U.S. Pat. Nos. 3,488,185; 3,552,954; and 3,179,515.
- a particularly preferred method is shown in commonly assigned U.S. Pat. No. 3,779,714 wherein 100 weight parts of alloy particles are mixed with about 0.1 to 10 weight parts of oxidant. The exact proportion of oxidant mixture depends on the solute metal to be oxidized and the concentration of solute metal in the alloy.
- the preferred oxidant comprises an intimate mixture of heat-reducible metal oxide having a negative free energy of formation at 25° C. of up to about 70 kilocalories per gram atom of oxygen, and finely divided hard, refractory metal oxide having a negative free energy of formation exceeding the negative free energy of formation of the heat-reducible metal oxide by at least about 60 kilocalories per gram atom of oxygen at 25° C.
- the heat-reducible metal oxide is present in the oxidant in an amount sufficient for complete oxidation of the solute metal in the alloy.
- the hard, refractory oxide in the oxidant is present in substantially the same equivalent elemental proportion as the solute metal in the alloy, and both are of a particle size suitable for dispersion strengthening of the oxidant residue resulting from the internal oxidation, as set forth in U.S. Pat. No. 3,779,714.
- the oxidant residue comprises particles of in situ residue of heat-reducible metal oxide and particles of hard, refractory metal oxide uniformly distributed therein and the residue of heat-reducible metal oxide is intimately dispersed within the alloy powder.
- the dispersion-strengthened metal mixture is eventually coalesced and consolidated by hot-working to form a solid metal workpiece whereby the residue of heat-reducible metal is dispersion strengthened by the hard, refractory metal oxide and forms an integral part of the dispersion strengthened resulting workpiece.
- Dispersion strengthened metal powders are ordinarily consolidated under heat and pressure such as by extrusion at temperatures usually above about 1400° F. wherein the extrudate emerges from the extrusion press typically in cylindrical bar stock which then can be cold drawn and machined to the desired configuration of the workpiece.
- a copper alloy containing 0.2% by weight alloyed aluminum was atomized by helium and collected dry. The powder was then heat treated in accordance with the process of U.S. Pat. No. 3,779,714 and finally hot extruded into 1/4" dia rods. Table 1 shows the room temperature mechanical properties of this material compared with the conventional alloy made by nitrogen atomization and water collection.
- the 100 hour rupture strength at 1550° F. was more than doubled when the alloy powder was atomized by helium and collected dry. This also comprises a significant improvement over the best values reported in literature for similar composition in as extruded condition.
- Preston and Grant 1 report a 100 rupture stength value of 6,000 psi for internally oxidized Cu-0.23% Al alloy. The room temperature properties reported by them are similar to those of He/dry material.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
A process for dispersion strengthing of atomized alloy particles by internal oxidation is substantially improved by providing atomized particles substantially free of oxide surface film to enhance the efficiency of the internal oxidation step. The atomized alloy particles can be produced by dry collection to prevent oxide film formation, or alternatively, the oxide surface film can be removed by mechanical action removal or by chemical leaching.
Description
This invention pertains to an improved process for producing improved dispersion strengthened alloy metal products.
Dispersion strengthened metal products, such as copper dispersion strengthened with aluminum oxide, have many commercial and industrial uses. Welding electrodes, for example, require good electrical and thermal conductivities together with good strength and hardness at elevated temperatures. Dispersion strengthening has been recognized in the past as a method for increasing strength and hardness of metals. A solid solution alloy comprising a relatively noble matrix metal having relatively low heat or free energy of oxide formation and a solute metal having relatively high negative heat or free energy of oxide formation can be dispersion strengthened by heating the alloy under oxidizing conditions to preferentially oxidize the solute metal. This technique of oxidizing the solute metal to a solute metal oxide is known in the art as in situ internal oxidation or more simply internal oxidation.
Several processes for internal oxidation have been suggested. Commonly assigned U.S. Pat. No. 3,779,714, incorporated herein by reference, provides an improved alloy-oxidant mixture wherein the oxidant includes an oxide which releases oxygen to oxidize the solute metal of the alloy. A further improvement is set forth in commonly assigned U.S. Pat. No. 3,893,844 which provides improved dispersion strengthened metals by first recrystallizing the alloy powder prior to internal oxidation to increase the grain size of the alloy to a grain size at least as large as Grain Size No. 6 as measured by ASTM Test. No. E-112.
In commonly assigned U.S. Pat. No. 3,779,714, a dilute solid solution alloy powder is obtained by atomizing an alloy melt of matrix metal with a minor amount of solute metal wherein the melt is atomized by nitrogen and collected as powder in water. During the atomization process, however, oxygen in the atomization chamber tends to oxidize the solute metal on the surface of the alloy particles. For instance, a copper-aluminum alloy tends to become oxidized during atomization to form an aluminum oxide film on the particle surfaces. Further oxidation of the surface aluminum can occur upon the powder contacting water in the collection tank. The hot powder falling into the water generates steam in the atomization chamber which further contributes to the surface oxidation of the alloy particles. The accumulative effect of surface oxidation is the formation of a relatively thick aluminum oxide film on the surface of the alloy particles.
It now has been found that the surface oxide film formed on the alloy particles remains intact and can be detrimental in subsequent internal oxidation by forming a barrier to internal oxidation. Subsequent processing can inhibit interparticle bonding during subsequent fabrication of the powder into compacted fully dense parts obtained, for example, by hot forging and rolling. The final product can be weak and brittle. In a subsequent hot extrusion step, the powder particles tend to stretch out into elongated fibers thus improving interparticle bonding, although surface oxide film has been found to remain on fiber interfaces and causes diminished mechanical properties due to improper and incomplete interparticle or interfiber bonding. Elimination of the surface oxide has been found to substantially improve the mechanical properties of the dispersion strengthened alloy such as stress rupture strength as well as substantially improve the internal oxidation step for dispersion strengthening alloys. The surface oxide forms a barrier to the diffusion of oxygen into the alloy particles and, therefore, elimination of the surface oxide provides efficient, uniform, and effective oxidation of higher solute metal alloys. Significant improvements in the properties of internally oxidized alloys can be achieved by atomizing alloys in helium and collecting the alloy powder dry. These and other advantages will become more apparent by referring to the Detailed Description of the Invention.
The process for dispersion strengthening of alloy metal can be substantially improved by the elimination of the surface oxide build-up on the alloy metal particles by preventing the oxide surface formation or by removing the oxide build-up prior to the step of internal oxidation. The improved process comprises atomization of alloy metal and eliminating the surface oxide by preventing oxide build-up or by removing the oxide prior to the step of internal oxidation and forming consolidated dispersion strengthened metals.
In practicing this invention, the powdered alloy comprising a relatively noble matrix metal and a solute metal is produced by conventional techniques such as melting the metal under inert or reducing conditions and thereafter comminuting the alloy by atomization to form a particulate alloy having an average particle size of less than about 300 microns. Water atomization of molten metal alloys is shown in U.S. Pat. No. 2,956,304 wherein metal particles are produced at particularly small particle sizes less than about 100 mesh. Water atomization similarly causes considerable surface oxidation of alloy particles due to the high temperatures of molten metal as well as the oxidizing characteristics of the water itself.
The noble matrix metal in the alloy can be defined broadly as those metals having a melting point of at least about 200° C. and whose oxides have a negative free energy of formation at 25° C. of from 0 to 70 kilocalories per gram atom of oxygen. Suitable alloy matrix metals include, for example, iron, cobalt, nickel, copper, cadmium, thallium, germanium, tin, lead, antimony, bismuth, molybdenum, tungsten, rhenium, indium, palladium, osmium, platinum, and rhodium as more particularly set forth in U.S. Pat. No. 3,779,714.
In any particular combination of matrix metal and solute metal in the alloy to be dispersion strengthened by internal oxidation, the matrix metal must be relatively noble with respect to the solute metal so that the solute metal will be preferentially oxidized. This is achieved by selecting the solute metal such that its negative free energy of oxide formation at 25° C. is at least 60 kilocalories per gram atom of oxygen greater than the negative free energy of formation of the oxide of the matrix metal at 25° C. Such solute metals have a negative free energy of oxide formation per gram atom of oxygen of over 80 kilocalories and generally over 120 kilocalories. Suitable alloy solute metals include: silicon, titanium, zirconium, aluminum, beryllium, thorium, chromium, magnesium, manganese, niobium, tantalum, and vanadium (VO), as more particularly set forth in U.S. Pat. No. 3,779,714. In accordance with the process of this invention, atomized alloy particles substantially free of oxide surface film are internally oxidized to form dispersion-strengthened metal.
In accordance with one aspect of this invention, atomized alloy particles are processed to remove the oxide build-up on the particle surface formed during atomization. The surface oxide film can be mechanically removed such as by milling, grinding or roll flaking the atomized alloy particles. Ballmilling, for example, can be used at a 4:1 to 8:1 ratio of ball/metal for 2 to 8 hours. Roll flaking can be used to reduce thickness of the atomized particles as well as remove oxide films which are believed to break up and/or redistribute the surface oxide over a larger surface area generated by the flaking of spherical powder. Flakes have larger surface:volume ratio than spheres of same volume. These and similar processes which deform or flatten the powder particle would be suitable.
In accordance with a further aspect of this invention, the surface oxide film can be removed by chemical action such as leaching. For example, atomized copper alloy powder can be leached in dilute nitric acid, ammonium hydroxide and also in mixtures of ammonium and sodium hydroxides.
Still, a further method of preventing surface oxide build-up on the atomized alloy particles pertains to collecting the alloy powder in a dry medium and avoid wet collection mediums such as water. Dry collection within helium, for instance, prevents contact with an oxidizing substance as well as avoids steam formation within the atomization chamber. Helium is substantially better than nitrogen in that the thermal conductivity thereof is 6.5 times that of nitrogen whereby much faster quenching, without appreciable oxidation, can be achieved. Helium quenching enables faster quenching of the atomized particles, thus minimizing oxidation of the solute metal such as aluminum at the particle surface and further minimizes migration of solute metal from the center of the alloy particle to the particle surface which can detrimentally deplete the alloy particle of solute metal.
The alloy particles being substantially free of surface oxide build-up can be internally oxidized by a variety of methods such as disclosed in U.S. Pat. Nos. 3,488,185; 3,552,954; and 3,179,515. A particularly preferred method is shown in commonly assigned U.S. Pat. No. 3,779,714 wherein 100 weight parts of alloy particles are mixed with about 0.1 to 10 weight parts of oxidant. The exact proportion of oxidant mixture depends on the solute metal to be oxidized and the concentration of solute metal in the alloy.
The preferred oxidant comprises an intimate mixture of heat-reducible metal oxide having a negative free energy of formation at 25° C. of up to about 70 kilocalories per gram atom of oxygen, and finely divided hard, refractory metal oxide having a negative free energy of formation exceeding the negative free energy of formation of the heat-reducible metal oxide by at least about 60 kilocalories per gram atom of oxygen at 25° C. The heat-reducible metal oxide is present in the oxidant in an amount sufficient for complete oxidation of the solute metal in the alloy. The hard, refractory oxide in the oxidant is present in substantially the same equivalent elemental proportion as the solute metal in the alloy, and both are of a particle size suitable for dispersion strengthening of the oxidant residue resulting from the internal oxidation, as set forth in U.S. Pat. No. 3,779,714. After internal oxidation, the oxidant residue comprises particles of in situ residue of heat-reducible metal oxide and particles of hard, refractory metal oxide uniformly distributed therein and the residue of heat-reducible metal oxide is intimately dispersed within the alloy powder. The dispersion-strengthened metal mixture is eventually coalesced and consolidated by hot-working to form a solid metal workpiece whereby the residue of heat-reducible metal is dispersion strengthened by the hard, refractory metal oxide and forms an integral part of the dispersion strengthened resulting workpiece. Dispersion strengthened metal powders are ordinarily consolidated under heat and pressure such as by extrusion at temperatures usually above about 1400° F. wherein the extrudate emerges from the extrusion press typically in cylindrical bar stock which then can be cold drawn and machined to the desired configuration of the workpiece.
The advantages of this invention wherein surface oxide build-up is either prevented or removed from alloy particles prior to the step of internally oxidizing are further illustrated in the following examples.
A copper alloy containing 0.2% by weight alloyed aluminum was atomized by helium and collected dry. The powder was then heat treated in accordance with the process of U.S. Pat. No. 3,779,714 and finally hot extruded into 1/4" dia rods. Table 1 shows the room temperature mechanical properties of this material compared with the conventional alloy made by nitrogen atomization and water collection.
TABLE 1
______________________________________
Room Temperature Properties of Internally
Oxidized Cu-0.20% Al alloy. (N.sub.2 /wet vs. He/dry)
Tensile Electrical
Atomization
Hardness Strength Elongation
Conductivity
______________________________________
(gas/collection)
(R.sub.B)
(psi) (%) (% IACS)
N.sub.2 /water
58 58,000 24 91
He/dry 68 68,000 22 92
______________________________________
There is a significant improvement in room temperature tensile strength and hardness on helium atomized and dry collected material. The improvement is even more dramatic at high temperatures. This is demonstrated by the data in Table 2.
TABLE 2
______________________________________
1550° F. Stress Rupture Properties of Internally
Oxidized Cu-0.20% Al alloy. (N.sub.2 /wet vs. He/dry)
100 Hour Rupture Strength
Atomization at 1550° F.
______________________________________
(gas/collection)
(psi)
N.sub.2 /water
3,800
He/dry 8,000
______________________________________
The 100 hour rupture strength at 1550° F. was more than doubled when the alloy powder was atomized by helium and collected dry. This also comprises a significant improvement over the best values reported in literature for similar composition in as extruded condition. Preston and Grant1 report a 100 rupture stength value of 6,000 psi for internally oxidized Cu-0.23% Al alloy. The room temperature properties reported by them are similar to those of He/dry material.
Claims (10)
1. In a process for dispersion-strengthening atomized alloy particles having an average particle size less than about 300 microns by internally oxidizing said alloy particles, the improvement comprising:
providing atomized .Iadd.copper/aluminum .Iaddend.alloy particles being substantially free of oxide surface film whereby said alloy is internally oxidized without obstruction of the oxide surface film.
2. The process of claim 1 wherein the atomized particles are dry collected within an inert gas or liquid to prevent oxide surface film formation on the atomized particles.
3. The process in claim 2 wherein the atomized particles are dry collected within helium gas.
4. The process of claim 1 wherein the atomized alloy particles are subjected to mechanical working to mechanically remove the oxide surface film.
5. The process in claim 4 wherein the mechanical working is ball milling.
6. The process in claim 4 wherein the mechanical working is grinding.
7. The process in claim 4 wherein the mechanical working is flaking.
8. The process in claim 1 wherein the oxide surface film is removed by chemical leaching.
9. The process in claim 8 wherein the chemical leaching agent is nitric acid.
10. The process in claim 8 wherein the chemical leaching agent is ammonium hydroxide.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/565,342 USRE31902E (en) | 1980-05-02 | 1983-12-27 | Dispersion strengthened metals |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/146,140 US4315770A (en) | 1980-05-02 | 1980-05-02 | Dispersion strengthened metals |
| US06/565,342 USRE31902E (en) | 1980-05-02 | 1983-12-27 | Dispersion strengthened metals |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/146,140 Reissue US4315770A (en) | 1980-05-02 | 1980-05-02 | Dispersion strengthened metals |
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| Publication Number | Publication Date |
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| USRE31902E true USRE31902E (en) | 1985-05-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US06/565,342 Expired - Lifetime USRE31902E (en) | 1980-05-02 | 1983-12-27 | Dispersion strengthened metals |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4857266A (en) | 1988-12-05 | 1989-08-15 | The United States Of America As Represented By The United States Department Of Energy | Dispersion strengthened copper |
| WO1993014238A1 (en) * | 1992-01-21 | 1993-07-22 | United Technologies Corporation | Silver-metal oxide materials for electrical contacts |
| WO1993015240A1 (en) * | 1992-01-30 | 1993-08-05 | Commissariat A L'energie Atomique | High-hardness conductive material and method for manufacturing same |
| WO1995005491A1 (en) * | 1993-08-17 | 1995-02-23 | Ultram International, L.L.C. | Dispersion strengthened copper |
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| US3552954A (en) * | 1968-09-20 | 1971-01-05 | Handy & Harman | Method of making internally oxidized dispersion hardened copper product |
| US3709667A (en) * | 1971-01-19 | 1973-01-09 | Johnson Matthey Co Ltd | Dispersion strengthening of platinum group metals and alloys |
| US3740210A (en) * | 1971-07-06 | 1973-06-19 | Int Nickel Co | Mechanically alloyed aluminum aluminum oxide |
| US3779714A (en) * | 1972-01-13 | 1973-12-18 | Scm Corp | Dispersion strengthening of metals by internal oxidation |
| US3893844A (en) * | 1972-01-13 | 1975-07-08 | Scm Corp | Dispersion strengthened metals |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3552954A (en) * | 1968-09-20 | 1971-01-05 | Handy & Harman | Method of making internally oxidized dispersion hardened copper product |
| US3709667A (en) * | 1971-01-19 | 1973-01-09 | Johnson Matthey Co Ltd | Dispersion strengthening of platinum group metals and alloys |
| US3740210A (en) * | 1971-07-06 | 1973-06-19 | Int Nickel Co | Mechanically alloyed aluminum aluminum oxide |
| US3779714A (en) * | 1972-01-13 | 1973-12-18 | Scm Corp | Dispersion strengthening of metals by internal oxidation |
| US3893844A (en) * | 1972-01-13 | 1975-07-08 | Scm Corp | Dispersion strengthened metals |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4857266A (en) | 1988-12-05 | 1989-08-15 | The United States Of America As Represented By The United States Department Of Energy | Dispersion strengthened copper |
| WO1993014238A1 (en) * | 1992-01-21 | 1993-07-22 | United Technologies Corporation | Silver-metal oxide materials for electrical contacts |
| US5284527A (en) * | 1992-01-21 | 1994-02-08 | United Technologies Corporation | Method of making silver-metal oxide materials and electrical contacts |
| WO1993015240A1 (en) * | 1992-01-30 | 1993-08-05 | Commissariat A L'energie Atomique | High-hardness conductive material and method for manufacturing same |
| WO1995005491A1 (en) * | 1993-08-17 | 1995-02-23 | Ultram International, L.L.C. | Dispersion strengthened copper |
| US5551970A (en) * | 1993-08-17 | 1996-09-03 | Otd Products L.L.C. | Dispersion strengthened copper |
| US5567382A (en) * | 1993-08-17 | 1996-10-22 | Otd Products L.L.C. | Dispersion strengthened copper |
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