US3156560A - Ductile niobium and tantalum alloys - Google Patents
Ductile niobium and tantalum alloys Download PDFInfo
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- US3156560A US3156560A US818263A US81826359A US3156560A US 3156560 A US3156560 A US 3156560A US 818263 A US818263 A US 818263A US 81826359 A US81826359 A US 81826359A US 3156560 A US3156560 A US 3156560A
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- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 title claims description 28
- 239000010955 niobium Substances 0.000 title claims description 27
- 229910001257 Nb alloy Inorganic materials 0.000 title description 9
- 229910001362 Ta alloys Inorganic materials 0.000 title description 9
- 229910052758 niobium Inorganic materials 0.000 claims description 23
- 229910052751 metal Inorganic materials 0.000 claims description 22
- 239000002184 metal Substances 0.000 claims description 22
- 229910052715 tantalum Inorganic materials 0.000 claims description 19
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 19
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 10
- 239000012535 impurity Substances 0.000 claims description 10
- 229910052727 yttrium Inorganic materials 0.000 claims description 9
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 9
- 229910052747 lanthanoid Inorganic materials 0.000 claims description 6
- 150000002602 lanthanoids Chemical class 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 5
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 229910052757 nitrogen Inorganic materials 0.000 claims description 5
- 229910052706 scandium Inorganic materials 0.000 claims description 5
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 4
- 239000001301 oxygen Substances 0.000 claims description 4
- 229910052760 oxygen Inorganic materials 0.000 claims description 4
- 230000000737 periodic effect Effects 0.000 claims description 3
- 150000001875 compounds Chemical class 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 description 17
- 239000000956 alloy Substances 0.000 description 17
- 229910052684 Cerium Inorganic materials 0.000 description 13
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 12
- 238000005266 casting Methods 0.000 description 9
- 229910052746 lanthanum Inorganic materials 0.000 description 8
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 7
- 238000002844 melting Methods 0.000 description 7
- 230000008018 melting Effects 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 7
- 238000007792 addition Methods 0.000 description 6
- RHDUVDHGVHBHCL-UHFFFAOYSA-N niobium tantalum Chemical compound [Nb].[Ta] RHDUVDHGVHBHCL-UHFFFAOYSA-N 0.000 description 6
- 150000002910 rare earth metals Chemical class 0.000 description 6
- 229910001122 Mischmetal Inorganic materials 0.000 description 4
- 229910052779 Neodymium Inorganic materials 0.000 description 4
- 229910052777 Praseodymium Inorganic materials 0.000 description 4
- 229910052772 Samarium Inorganic materials 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 description 4
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 description 4
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000005242 forging Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 238000009489 vacuum treatment Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- -1 notably Substances 0.000 description 2
- 238000009700 powder processing Methods 0.000 description 2
- 238000005245 sintering Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910000636 Ce alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910052692 Dysprosium Inorganic materials 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052693 Europium Inorganic materials 0.000 description 1
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- 229910052765 Lutetium Inorganic materials 0.000 description 1
- 229910052773 Promethium Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- AJHQUQJABBRDOW-UHFFFAOYSA-N [Nb].[La] Chemical compound [Nb].[La] AJHQUQJABBRDOW-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 239000012298 atmosphere Substances 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 description 1
- OGPBJKLSAFTDLK-UHFFFAOYSA-N europium atom Chemical compound [Eu] OGPBJKLSAFTDLK-UHFFFAOYSA-N 0.000 description 1
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 229910052756 noble gas Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- VQMWBBYLQSCNPO-UHFFFAOYSA-N promethium atom Chemical compound [Pm] VQMWBBYLQSCNPO-UHFFFAOYSA-N 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/02—Alloys based on vanadium, niobium, or tantalum
Definitions
- the metals niobium and tantalum normally occur together in nature and have similar chemical, physical and mechanical properties. When substantially pure, both metals have high resistance to corrosive attack by nearly all of the mineral acids and have quite high mechanical strength over wide temperature ranges. Thus, the metals are particularly useful for making structural elements subjected to corrosive environments, such as gas turbine parts.
- niobium and tantalum and niobium-tantalum alloys of adequate size to form structural shapes such as sheets, rods, tubes, wires, bars and the like has heretofore been principally effected by mechanically pressing substantially pure niobium, tantalum or niobium-tantalum alloy powders into bars, usually two to three feet long and up to about one square inch in cross-section, and sintering the pressed bars in a vacuum. Bars sintered in this fashion usually have a density of about 90 percent of the theoretical density. Higher densities are obtained by rolling or forging the sintered bars and then reheating in vacuum.
- Powder processing of niobium, tantalum and niobiumtantalurn alloys has been heretofore required by virtue of the fact that bodies produced by melting and casting techniques have been virtually unworkable at room temperature, unless made from niobium or tantalum which was previously subjected to an extremely high vacuum.
- High vacuum treatment withdraws nonmetallic impurities, specifically oxygen, nitrogen, and carbon, which are normally present in the metals. These nonmetallics cause an extremely large embrittling eifect on the material, which effect previously has been removed only by subjecting the metals to high vacuum treatment.
- both the powder processing and the vacuum treatments result in increased production costs, which lower the usefulness of the niobium, tantalum and niobium-tantalum alloys.
- An additional object of this invention is to provide niobium, tantalum and niobium-tantalum alloys in which the nonmetallic embrittling elements present are precipitated as second phases.
- the alloys of the present invention include niobium, tantalum and niobiumtantalum alloys which contain from about 2 to about 10 weight percent of scandium, yttrium, or about 2 to about 10 weight percent of the rare earth elements of the lanthanide series of the Periodic Table to combine with the nonmetllic impurities, notably, oxygen, nitrogen and carbon, and form a second phase dispersion which overcomes the embrittling effects of the nonmetallics.
- the lanthanide series of the rare earth elements will be understood to consist of the elements having atomic numbers from 57 to 71, inclusive, and comprise the elements lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holrnium, erbium, ytterbium, and lutetium.
- Commercial lanthanum contains about 99.9 weight percent lanthanum, less than 0.1 percent cerium, less than 0.1 percent neodymium, less than 0.1 percent praseodymium, and less than 0.1 percent samarium, usually with trace amounts of others of the rare earth metals.
- cerium usually contains about 97 percent cerium, about 0.9 percent neodymium, about 0.5 percent praseodymium, about 0.1 percent samarium, and about 1.5 percent lanthanum, plus others of the rare earth elements.
- Commercial mischmetal normally contains from about 47 to 52 percent cerium, from about 18 to 19 percent neodymium, from about 5 to 6 percent praseodymium, about 1 percent samarium, and from 24 to 27 percent lanthanum.
- the alloys may be readily prepared by are melting the various constituents together in an argon or other noble gas atmosphere.
- alloys having the following nominal compositions were prepared by melting commercially obtainable pulverulent tantalum and niobium with commercial cerium, lanthanum and mischmetal, an alloy or commercial mixture of the lanthanide series elements.
- the powdered tantalum contained 0.05 percent niobium and the powdered niobium contained 0.15 percent tantalum.
- the following alloys were melted in a conventional arc melting furnace employing a water-cooled, tungstentipped non-consumable electrode and a water-cooled copper crucible.
- the Rockwell hardness, scale A was determined for each alloy in the as-cast condition and bears a direct relationship to ductility. Upon inspection of the data shown in Table I, it will be seen that increasing additions of cerium produced a decrease in the as-cast hardness of the niobium alloys and the corresponding decrease in hardness in the comparable niobium-lanthanum, niobium-misclnnetal, and tantalum-mischmetal alloys. The yttrium additions exhibited effects on the niobium similar to those of the rare earth metals by reducing the hardness as the amount of yttrium added was increased. The
- the casting made by are melting the niobium powder without scandium, yttrium or lanthanide series rare earth additions (nominally 100% niobium) was found to be brittle and could not be cold rolled any measurable degree or hot forged without serious cracking. Similar brittleness was exhibited by the 100% tantalum casting. However, the niobium alloy casting containing 2.3 percent cerium was successfully hot forged, and the niobium alloy casting containing 4.6 percent cerium was cold reduced 8 percent in thickness by rolling before serious cracks developcd.
- the niobium alloy casting containing 5 percent cerium was reduced in thickness 67 percent by hot forging and then cold reduced 76 percent in thickness by rolling to form 20 mil thick sheet.
- the niobium alloy casting containing 8 percent cerium was cold reduced 88 percent in thickness with only minor edge cracking developing.
- the hot forgnig disclosed previously was accomplished by heating the castings to 1500 C. in an argon atmosphere and immediately forging in air.
- Test specimens were prepared from the 20 mil sheet fabricated from the 5 percent cerium alloy disclosed previously, and tensile test results under various conditions were obtained from these specimens. The results are listed in Table II.
- the present alloy exhibits a substantial improvement in strength over substantially pure ductile niobium.
- substantially pure niobuim in the cold rolled state has a room temperature ultimate tensile strength of 100,000 p.s.i. and in the annealed (presumably, recrystallized) state, exhibits an ultimate tensile strength of 50,000 p.s.i.
- the arc melted alloys of my invention have improved ductility over nominally pure arc melted castings of niobium and tantalum and further have improved room temperature strength over the vacuum sintered commercial niobium sheet metal.
- a body composed of (a) at least weight percent of a matrix metal selected from the group consisting of niobium and tantalum, said matrix containing small amounts of ox gen, carbon and nitrogen as nonmetallic impurities and, (b) a compound of a metal selected from the group consisting of scandium, yttrium and the rare earth elements of the lanthanide series of the Periodic Table of Elements, and combinations thereof together with said nonmetallic impurities, said selected metal being added in amounts of from about 2 to 10 weight percent of said alloy to combine with said nonmetallic impurities and increase the ductility of said matrix metal.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Powder Metallurgy (AREA)
Description
United States Patent 3,156,560 DUCTELE NIOBIUM AND TANTALUM ALLQYS John W. Semmel, Jr., Wyoming, Ohio, assignor to General Electric Company, a corporation of New York No Drawing. Filed June 5, 1959, Ser. No. 818,263 6 Claims. (Cl. 75-174) This invention relates to niobium and tantalum alloys and more particularly to niobium and tantalum alloys which are ductile at both room temperature and elevated temperatures. This application is a continuation-in-part of my application Serial No. 631,059, filed December 28, 1956, and now abandoned and assigned to the same assignee as the present application.
The metals niobium and tantalum normally occur together in nature and have similar chemical, physical and mechanical properties. When substantially pure, both metals have high resistance to corrosive attack by nearly all of the mineral acids and have quite high mechanical strength over wide temperature ranges. Thus, the metals are particularly useful for making structural elements subjected to corrosive environments, such as gas turbine parts.
The production of bodies of niobium and tantalum and niobium-tantalum alloys of adequate size to form structural shapes such as sheets, rods, tubes, wires, bars and the like has heretofore been principally effected by mechanically pressing substantially pure niobium, tantalum or niobium-tantalum alloy powders into bars, usually two to three feet long and up to about one square inch in cross-section, and sintering the pressed bars in a vacuum. Bars sintered in this fashion usually have a density of about 90 percent of the theoretical density. Higher densities are obtained by rolling or forging the sintered bars and then reheating in vacuum.
Processing limitations normally present in producing coherent bodies from powdered or pulverulent materials limit production to bodies of relatively small cross-sectional areas. Therefore, the size of bodies which may be fabricated by the usual sintering procedures without resorting to brazing or welding operations is similarly limited.
Powder processing of niobium, tantalum and niobiumtantalurn alloys has been heretofore required by virtue of the fact that bodies produced by melting and casting techniques have been virtually unworkable at room temperature, unless made from niobium or tantalum which was previously subjected to an extremely high vacuum. High vacuum treatment withdraws nonmetallic impurities, specifically oxygen, nitrogen, and carbon, which are normally present in the metals. These nonmetallics cause an extremely large embrittling eifect on the material, which effect previously has been removed only by subjecting the metals to high vacuum treatment. Obviously, both the powder processing and the vacuum treatments result in increased production costs, which lower the usefulness of the niobium, tantalum and niobium-tantalum alloys.
It is therefore a principal object of this invention to provide niobium, tantalum and niobium-tantalum alloys which can be melted and cast under protective atmospheres to produce ingots ductile at both room temperature and at elevated temperatures.
An additional object of this invention is to provide niobium, tantalum and niobium-tantalum alloys in which the nonmetallic embrittling elements present are precipitated as second phases.
Generally, the alloys of the present invention include niobium, tantalum and niobiumtantalum alloys which contain from about 2 to about 10 weight percent of scandium, yttrium, or about 2 to about 10 weight percent of the rare earth elements of the lanthanide series of the Periodic Table to combine with the nonmetllic impurities, notably, oxygen, nitrogen and carbon, and form a second phase dispersion which overcomes the embrittling effects of the nonmetallics.
The lanthanide series of the rare earth elements will be understood to consist of the elements having atomic numbers from 57 to 71, inclusive, and comprise the elements lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holrnium, erbium, ytterbium, and lutetium. Commercial lanthanum contains about 99.9 weight percent lanthanum, less than 0.1 percent cerium, less than 0.1 percent neodymium, less than 0.1 percent praseodymium, and less than 0.1 percent samarium, usually with trace amounts of others of the rare earth metals. Commercial cerium usually contains about 97 percent cerium, about 0.9 percent neodymium, about 0.5 percent praseodymium, about 0.1 percent samarium, and about 1.5 percent lanthanum, plus others of the rare earth elements. Commercial mischmetal normally contains from about 47 to 52 percent cerium, from about 18 to 19 percent neodymium, from about 5 to 6 percent praseodymium, about 1 percent samarium, and from 24 to 27 percent lanthanum.
According to the present invention, the alloys may be readily prepared by are melting the various constituents together in an argon or other noble gas atmosphere. For example, alloys having the following nominal compositions were prepared by melting commercially obtainable pulverulent tantalum and niobium with commercial cerium, lanthanum and mischmetal, an alloy or commercial mixture of the lanthanide series elements. According to the suppliers analysis, the powdered tantalum contained 0.05 percent niobium and the powdered niobium contained 0.15 percent tantalum.
The following alloys were melted in a conventional arc melting furnace employing a water-cooled, tungstentipped non-consumable electrode and a water-cooled copper crucible.
Table l Misch- As-Cast Nb, 'Ia, Ce, La, Metal, Y, Hardness, Percent Percent Percent Percent Percent Percent Rockwell Nomlnally pure commercial pulverulent metal.
The Rockwell hardness, scale A was determined for each alloy in the as-cast condition and bears a direct relationship to ductility. Upon inspection of the data shown in Table I, it will be seen that increasing additions of cerium produced a decrease in the as-cast hardness of the niobium alloys and the corresponding decrease in hardness in the comparable niobium-lanthanum, niobium-misclnnetal, and tantalum-mischmetal alloys. The yttrium additions exhibited effects on the niobium similar to those of the rare earth metals by reducing the hardness as the amount of yttrium added was increased. The
results further indicated that while percentage additions of from 2 to 10 weight percent will combine with all the nonmetallics, for alloys containing normal percentages of nonmetallics no more than about 5 weight percent additions need be made. Thus, where fabricating operations such as welding are not comtemplated, additions of 2 to 5 weight percent are preferred.
Accompanynig the decrease of hardness noted from the results of Table I was an increase in the ductility. In these alloys, the powdered niobium used contained, on analysis, about 0.38 weight per cent oxygen, 0.11 per cent nitrogen and 0.08 per cent carbon. This amount of nonmetallic impurities in either niobium or tantalum or combinations thereof will severely reduce the workability of the material and render it useless for shaping into articles. Currently, the only manner in which melted niobium or tantalum bodies containing these nonmetallic impurities can be rendered ductile is by subjecting them to an extremely high vacuum during a melting process, for example, by subjecting the metals to vacuum during electron beam melting. The principal drawback, however, is the fact that the material thus produced is ex tremely expensive, on the order $200 per pound, due to the complex procedure which must be followed during melting and due to a comparatively greater probability of producing a poor ingot.
Referring once again to Table I, the casting made by are melting the niobium powder without scandium, yttrium or lanthanide series rare earth additions (nominally 100% niobium) was found to be brittle and could not be cold rolled any measurable degree or hot forged without serious cracking. Similar brittleness was exhibited by the 100% tantalum casting. However, the niobium alloy casting containing 2.3 percent cerium was successfully hot forged, and the niobium alloy casting containing 4.6 percent cerium was cold reduced 8 percent in thickness by rolling before serious cracks developcd. The niobium alloy casting containing 5 percent cerium was reduced in thickness 67 percent by hot forging and then cold reduced 76 percent in thickness by rolling to form 20 mil thick sheet. The niobium alloy casting containing 8 percent cerium was cold reduced 88 percent in thickness with only minor edge cracking developing. The hot forgnig disclosed previously was accomplished by heating the castings to 1500 C. in an argon atmosphere and immediately forging in air.
Test specimens were prepared from the 20 mil sheet fabricated from the 5 percent cerium alloy disclosed previously, and tensile test results under various conditions were obtained from these specimens. The results are listed in Table II.
1 Reerystalllzed stateunneelcd 1 hour at 2800 F. in vacuum.
From the foregoing data, it may be seen that when a sufiicient amount of yttrium or rare earth metal is added to the basis metal, the nonmetallics become precipitated as a second phase and the embrittling ellect which they exert is removed. While amounts of scandium, yttrium or rare earth metals can be added to just precipitate all of the nonmetallics present, the normal procedure would be to add a slightly larger amount to insure that all the nonmetallics become combined. Also, should it become ne essary to weld or otherwise fuse portions of the niobium and tantalum alloys, the excess portion of the rare earth metals will be present to eliminate the possibility of recontamination of the alloy. As an additional factor, it may be noted that the present alloy exhibits a substantial improvement in strength over substantially pure ductile niobium. As a comparison, it has been reported that substantially pure niobuim in the cold rolled state has a room temperature ultimate tensile strength of 100,000 p.s.i. and in the annealed (presumably, recrystallized) state, exhibits an ultimate tensile strength of 50,000 p.s.i. These strengths are obviously quite lower than those obtained by using the alloys of this invention, as clearly indicated by the results in Table II.
From the foregoing, it may be seen that the arc melted alloys of my invention have improved ductility over nominally pure arc melted castings of niobium and tantalum and further have improved room temperature strength over the vacuum sintered commercial niobium sheet metal.
What I claim as new and desire to secure by Letters l .tent of t 1e United States is:
1. A body composed of (a) at least weight percent of a matrix metal selected from the group consisting of niobium and tantalum, said matrix containing small amounts of ox gen, carbon and nitrogen as nonmetallic impurities and, (b) a compound of a metal selected from the group consisting of scandium, yttrium and the rare earth elements of the lanthanide series of the Periodic Table of Elements, and combinations thereof together with said nonmetallic impurities, said selected metal being added in amounts of from about 2 to 10 weight percent of said alloy to combine with said nonmetallic impurities and increase the ductility of said matrix metal.
2. A body as defined in claim 1 wherein said selected metal is yttrium.
3. A body as defined in claim 1 wherein said selected metal is mischmetal.
4. A body as defined in claim 1 wherein said selected metal is cerium.
5. A body as defined in claim 1 wherein said selected metal is lanthanum.
6. A body as defined in claim 1 wherein said selected metal is added in amounts of from about 2 to 5 weight percent of said alloy.
References Cited in the file of this patent UNITED STATES PATENTS 2,187,630 Schafer Jan. 16, 1940 2,838,395 Rhodin June 10, 1958 2,838,396 Rhodin June 10, 1958 2,881,069 Rhodin Apr. 7, 1959 2,883,282 Wainer Apr. 21, 1959 FOREIGN PATENTS 323,315 Canada June 14, 1932 OTHER REFERENCES Trans. ofthe ASM, vol. 48, 1956, pages 677688, page 684 of special interest, article by Pugh.
Rare Metals Handbook, Pampel, Reinhold Publishing Company, 1954, page 340.
Claims (1)
1. A BODY COMPOSED OF (A) AT LEAST 90 WEIGHT PERCENT OF A MATRIX METAL SELECTED FROM THE GROUP CONSISTING OF NIOBIUM AND TANTALUM, AND MATRIX CONTAINING SMALL AMOUNTS OF OXYGEN, CARBON AND NITROGEN AS NONMETALLIC IMPURITIES AND, (B) A COMPOUND OF A METAL SELECTED FROM THE GROUP CONSISTING OF SCANDIUM, YTTRIUM AND THE RARE EARTH ELEMENTS OF THE LANTHANIDE SERIES OF THE PERIODIC TABLE OF ELEMENTS, AND COMBINATIONS THEREOF TOGETHER WITH SAID NONMETALLIC IMPURITIES, SAID SELECTED METAL BEING ADDED IN AMOUNTS OF FROM ABOUT 2 TO 10 WEIGHT PERCENT OF SAID ALLOY TO COMBINE WITH SAID NONMETALLIX IMPURITIES AND INCREASE THE DUCTILITY OF SAID MATRIX METAL.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US818263A US3156560A (en) | 1959-06-05 | 1959-06-05 | Ductile niobium and tantalum alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US818263A US3156560A (en) | 1959-06-05 | 1959-06-05 | Ductile niobium and tantalum alloys |
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| US3156560A true US3156560A (en) | 1964-11-10 |
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| US818263A Expired - Lifetime US3156560A (en) | 1959-06-05 | 1959-06-05 | Ductile niobium and tantalum alloys |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3236638A (en) * | 1963-11-01 | 1966-02-22 | Gen Electric | Columbium-base alloy of improved fabricability |
| US3243290A (en) * | 1963-07-22 | 1966-03-29 | Gen Electric | Tantalum base alloy |
| US3266892A (en) * | 1965-01-04 | 1966-08-16 | Samuel A Worcester | Columbium-hafnium base alloys with yttrium addition |
| US3268328A (en) * | 1964-11-03 | 1966-08-23 | Nat Res Corp | Metallurgy |
| US3285716A (en) * | 1964-07-20 | 1966-11-15 | Kawecki Chemical Company | Etched tantalum foil |
| US3335037A (en) * | 1963-12-27 | 1967-08-08 | Gen Electric | Method for producing tantalum sheet |
| US3805119A (en) * | 1970-09-29 | 1974-04-16 | Atomic Energy Commission | Superconductor |
| US5374393A (en) * | 1990-08-22 | 1994-12-20 | Duke University | High temperature turbine engine alloys containing gold |
| US11198927B1 (en) | 2019-09-26 | 2021-12-14 | United States Of America As Represented By The Secretary Of The Air Force | Niobium alloys for high temperature, structural applications |
| US11846008B1 (en) | 2019-09-26 | 2023-12-19 | United States Of America As Represented By Secretary Of The Air Force | Niobium alloys for high temperature, structural applications |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA323315A (en) * | 1932-06-14 | Allen Heany John | Tantalum and rare earth metal alloy | |
| US2187630A (en) * | 1935-07-09 | 1940-01-16 | Charles J Schafer | Alloy |
| US2838395A (en) * | 1956-11-14 | 1958-06-10 | Du Pont | Niobium base high temperature alloys |
| US2838396A (en) * | 1956-11-14 | 1958-06-10 | Du Pont | Metal production |
| US2881069A (en) * | 1956-11-14 | 1959-04-07 | Du Pont | Niobium base high temperature alloys |
| US2883282A (en) * | 1957-05-21 | 1959-04-21 | Horizons Inc | Protection of niobium from oxidation |
-
1959
- 1959-06-05 US US818263A patent/US3156560A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA323315A (en) * | 1932-06-14 | Allen Heany John | Tantalum and rare earth metal alloy | |
| US2187630A (en) * | 1935-07-09 | 1940-01-16 | Charles J Schafer | Alloy |
| US2838395A (en) * | 1956-11-14 | 1958-06-10 | Du Pont | Niobium base high temperature alloys |
| US2838396A (en) * | 1956-11-14 | 1958-06-10 | Du Pont | Metal production |
| US2881069A (en) * | 1956-11-14 | 1959-04-07 | Du Pont | Niobium base high temperature alloys |
| US2883282A (en) * | 1957-05-21 | 1959-04-21 | Horizons Inc | Protection of niobium from oxidation |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3243290A (en) * | 1963-07-22 | 1966-03-29 | Gen Electric | Tantalum base alloy |
| US3236638A (en) * | 1963-11-01 | 1966-02-22 | Gen Electric | Columbium-base alloy of improved fabricability |
| US3335037A (en) * | 1963-12-27 | 1967-08-08 | Gen Electric | Method for producing tantalum sheet |
| US3285716A (en) * | 1964-07-20 | 1966-11-15 | Kawecki Chemical Company | Etched tantalum foil |
| US3268328A (en) * | 1964-11-03 | 1966-08-23 | Nat Res Corp | Metallurgy |
| US3266892A (en) * | 1965-01-04 | 1966-08-16 | Samuel A Worcester | Columbium-hafnium base alloys with yttrium addition |
| US3805119A (en) * | 1970-09-29 | 1974-04-16 | Atomic Energy Commission | Superconductor |
| US5374393A (en) * | 1990-08-22 | 1994-12-20 | Duke University | High temperature turbine engine alloys containing gold |
| US11198927B1 (en) | 2019-09-26 | 2021-12-14 | United States Of America As Represented By The Secretary Of The Air Force | Niobium alloys for high temperature, structural applications |
| US11846008B1 (en) | 2019-09-26 | 2023-12-19 | United States Of America As Represented By Secretary Of The Air Force | Niobium alloys for high temperature, structural applications |
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