US2746861A - Ternary zirconium base alloy containing sn and ti - Google Patents
Ternary zirconium base alloy containing sn and ti Download PDFInfo
- Publication number
- US2746861A US2746861A US376279A US37627953A US2746861A US 2746861 A US2746861 A US 2746861A US 376279 A US376279 A US 376279A US 37627953 A US37627953 A US 37627953A US 2746861 A US2746861 A US 2746861A
- Authority
- US
- United States
- Prior art keywords
- alloys
- zirconium
- alloy containing
- base alloy
- zirconium base
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910045601 alloy Inorganic materials 0.000 title description 27
- 239000000956 alloy Substances 0.000 title description 27
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 title description 7
- 229910052726 zirconium Inorganic materials 0.000 title description 7
- 229910052718 tin Inorganic materials 0.000 description 11
- 239000010936 titanium Substances 0.000 description 10
- 229910052719 titanium Inorganic materials 0.000 description 10
- 238000012360 testing method Methods 0.000 description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 6
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 239000004035 construction material Substances 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 229910001128 Sn alloy Inorganic materials 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 2
- XNFDWBSCUUZWCI-UHFFFAOYSA-N [Zr].[Sn] Chemical compound [Zr].[Sn] XNFDWBSCUUZWCI-UHFFFAOYSA-N 0.000 description 2
- ROOXNKNUYICQNP-UHFFFAOYSA-N ammonium persulfate Chemical compound [NH4+].[NH4+].[O-]S(=O)(=O)OOS([O-])(=O)=O ROOXNKNUYICQNP-UHFFFAOYSA-N 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 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
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001093 Zr alloy Inorganic materials 0.000 description 1
- FGKRRBWIHMRUCR-UHFFFAOYSA-N [Sn].[Ti].[Zr] Chemical compound [Sn].[Ti].[Zr] FGKRRBWIHMRUCR-UHFFFAOYSA-N 0.000 description 1
- 229910001870 ammonium persulfate Inorganic materials 0.000 description 1
- 239000012300 argon atmosphere Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- PMTRSEDNJGMXLN-UHFFFAOYSA-N titanium zirconium Chemical compound [Ti].[Zr] PMTRSEDNJGMXLN-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
- C22C16/00—Alloys based on zirconium
Definitions
- the objects of this invention are accomplished by providing zirconium-tin-titanium alloys. Although the desirable properties are obtained with practically all titanium contents, it is preferable to restrict the titanium content to a content of 6% by weight. The tin content should not exceed 4% if the alloys are to be fabricated.
- the alloy of this invention thus preferably contains from 0.5 to 4% by weight of tin and from 2 to 6% of titanium, the best alloy containing about 4% of either component.
- the alloys may be produced by any method known to those skilled in the art.
- the alloys were prepared by drilling holes into pieces of metallic zirconium, putting suitable quantities nited States Patent
- the ingots of the alloys were first upset-forged'and then hot-rolled at 1000 C. to yield Aa-inch thick slabs. Then about 0.01 inch of the slabs was shaved ofl? from the surface on each side in order to remove any gaseous contaminants.
- These scalped" slabs were then cold-rolled in reductions of approximately 0.002 inch per pass until a total reduction of from 20 to 30% had been obtained.
- the cold-rolled alloys were then annealed for one hour at 700 C. in a straightening press.
- the sheets resulting thereby were again scalped 0.01 inch on each side and cut into testing specimens.
- the hardness was determined at three stages of the alloys, namely, as cast, cold-rolled, and annealed. In addition to these, the hardness was also determined in some instances after the alloys had been heated to 955 C. and brine-quenched.
- the specimens were taken parallel to the rolling direction.
- the specimens were 5 inches long and inch wide; they had a l /z-inch long reduced section which was 0.5 inch wide and from 0.04 to 0.08 inch thick.
- the tensile strength was tested in an argon atmosphere at 500 C. with the head of the testing machine traveling at 0.02 inch per minute.
- the yield strength was determined as the 0.02% offset yield strength, which is the stress developed in tension producing an offset of 0.2% from the original modulus line.
- Determination of the elongation was carried out by punching bench marks in the tensile specimens before testing. These bench marks were one inch apart before testing. After testing, the two halves of the broken specimen were placed together and the distance between the bench marks was measured. The increment in distance between the marks was an indication of the elongation of the specimen.
- the alloys produced were tested as to hardness, tensile strength, and elongation, the characteristics primarily of interest for construction materials.
- microstructure of these alloys was determined on sections of the alloys, which had been annealed for three hours at 700 C.; these sections were polished by hand to 4/0 paper and etched with a 2% ammonium bifiuoride- 2% ammonium persulfate solution.
- the alloys were found to consist of one single phase with the exception of minor carbide particles which were formed from a low contaminating carbon content.
- the alloys of this invention are used advantageously as construction materials in the chemical industry where the equipment has to undergo temperature increases.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
TERNARY ZIRCONIUM BASE ALLOY CONTAINING Sn AND Ti Walston Chubb, Jr., and Lyle L. Marsh, Jr., Columbus,
Ohio, assignors to the United States of America as represented by the United States Atomic Energy Commission No Drawing. Application July 17, 1253, Serial No. 376,279
1 Claim. (Cl. 75-177) This invention deals with a zirconium-base alloy, and in particular with a ternary zirconium-tin alloy.
It is an object of this invention to provide an alloy which has high tensile strength at elevated temperature.
It is also an object of this invention to provide an alloy which is characterized by a high degree of ductility.
Alloys which have the above-mentioned properties are being used as construction material, for instance, for equipment which is subjected to high temperatures.
The objects of this invention are accomplished by providing zirconium-tin-titanium alloys. Although the desirable properties are obtained with practically all titanium contents, it is preferable to restrict the titanium content to a content of 6% by weight. The tin content should not exceed 4% if the alloys are to be fabricated. The alloy of this invention thus preferably contains from 0.5 to 4% by weight of tin and from 2 to 6% of titanium, the best alloy containing about 4% of either component.
The alloys may be produced by any method known to those skilled in the art. For the experiments described below the alloys were prepared by drilling holes into pieces of metallic zirconium, putting suitable quantities nited States Patent For the hardness tests, the ingots of the alloys were first upset-forged'and then hot-rolled at 1000 C. to yield Aa-inch thick slabs. Then about 0.01 inch of the slabs was shaved ofl? from the surface on each side in order to remove any gaseous contaminants. These scalped" slabs were then cold-rolled in reductions of approximately 0.002 inch per pass until a total reduction of from 20 to 30% had been obtained. The cold-rolled alloys were then annealed for one hour at 700 C. in a straightening press. The sheets resulting thereby were again scalped 0.01 inch on each side and cut into testing specimens. The hardness was determined at three stages of the alloys, namely, as cast, cold-rolled, and annealed. In addition to these, the hardness was also determined in some instances after the alloys had been heated to 955 C. and brine-quenched.
For the tensile strength tests, the specimens were taken parallel to the rolling direction. The specimens were 5 inches long and inch wide; they had a l /z-inch long reduced section which was 0.5 inch wide and from 0.04 to 0.08 inch thick. The tensile strength was tested in an argon atmosphere at 500 C. with the head of the testing machine traveling at 0.02 inch per minute. The yield strength was determined as the 0.02% offset yield strength, which is the stress developed in tension producing an offset of 0.2% from the original modulus line.
Determination of the elongation was carried out by punching bench marks in the tensile specimens before testing. These bench marks were one inch apart before testing. After testing, the two halves of the broken specimen were placed together and the distance between the bench marks was measured. The increment in distance between the marks was an indication of the elongation of the specimen.
In the following table the properties of some of the alloys of this invention are summarized.
0.68% Sn, 2% Sn, 3.9% Sn, 8.9% Sn, 3.9% Sn, Components of Zirconium Alloy 3.3 T1 4.5% Ti 1.2% Ti 1.6% T1 4.2% Ti 0.2% ofiset yield strength at 500 C., p. S. l 24, 000 25, 600 25, 400 28, 100 32, 000 Ultimate strength at 500 0., p. s. i 44, 000 42, 400 38, 800 42, 600 50, 000 Elongation in 1 at 500 0., percent 22 28 29 35 18 Reduction of area at 500 0., percent 28 34 35 34 22 Hardness as cast, Rockwell A 54 52 53 56 Hardness, cold-rolled, Rockwell A 60 62 60 60 63 Hardness, cold-rolled and annealed 1 h 0.,
Rockwell "A" 1 56 58 58 57 60 Hardness after brine-quenched from 955 0.,
Rockwell 21" 63 54 55 68 1 This alloy was annealed for 3 hours at 700 C.
of tin and titanium thereinto, and then sealing the holes with zirconium chips. These zirconium pieces were then heated in a graphite crucible by high-frequency induction at an absolute pressure of less than 10 microns of mercury. A charge of about 200 grams was melted in each case; the crucible was first charged with about half of this quantity, and only after this first portion had melted was there added the remainder of the charge. The melted alloys were then allowed to cool slowly. The ingots obtained thereby weighed between and grams, part of the material having been taken up by the graphite of the crucible. In some instances, the alloys were produced in an arc melting furnace, and satisfactory results were then also obtained. It will be understood that, instead of melting the materials in two installments, the entire charge may be placed into a crucible at the beginning.
The alloys produced were tested as to hardness, tensile strength, and elongation, the characteristics primarily of interest for construction materials.
These results show that titanium increases the yield strength of a zirconium-tin alloy and also that a tin content improves the yield strength of a zirconium-titanium alloy. The 0.2% ofiset yield strength for pure zirconium was found to range between 4000 and 11,000 p. s. i., which is considerably less than that found with the alloys. Stainless steel 347, which is a steel containing from 17 to 19% chromium and from 9 to 12% nickel, has a yield strength of 31,000 p. s. i. at 500 C.
The microstructure of these alloys was determined on sections of the alloys, which had been annealed for three hours at 700 C.; these sections were polished by hand to 4/0 paper and etched with a 2% ammonium bifiuoride- 2% ammonium persulfate solution. The alloys were found to consist of one single phase with the exception of minor carbide particles which were formed from a low contaminating carbon content.
The alloys of this invention are used advantageously as construction materials in the chemical industry where the equipment has to undergo temperature increases.
It will be understood that this invention is not to be OTHER REF REN ES limited to the details given herein but that it may be modified within the scope of the appended claim. Anderson et Preliminary Survey Of Zirconium wh i l d i Alloys, Bureau of Mines Rept. of Investigations 4658, A ternary zirconium-base alloy containing about 4% 5 March 1950, 43 Pages, Particularly P g 40-43.
h wei t of tin and about 49 b wei t of titanium.
y gh y gh 1138-1140.
References Cited in the file of this patent UNITED STATES PATENTS 2,490,571 Anicettic Dec. 6, 1949 Schwope et aL: Journal of Metals, Nov. 1952, pages
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US376279A US2746861A (en) | 1953-07-17 | 1953-07-17 | Ternary zirconium base alloy containing sn and ti |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US376279A US2746861A (en) | 1953-07-17 | 1953-07-17 | Ternary zirconium base alloy containing sn and ti |
Publications (1)
Publication Number | Publication Date |
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US2746861A true US2746861A (en) | 1956-05-22 |
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US376279A Expired - Lifetime US2746861A (en) | 1953-07-17 | 1953-07-17 | Ternary zirconium base alloy containing sn and ti |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2822302A (en) * | 1956-01-16 | 1958-02-04 | Radio Mfg Company Inc | Non-emissive electrode |
KR20180134889A (en) | 2016-04-22 | 2018-12-19 | 니끼 쇼꾸바이 카세이 가부시키가이샤 | Dispersion of silica-based composite fine particles and production method thereof |
KR20190058715A (en) | 2015-03-31 | 2019-05-29 | 니끼 쇼꾸바이 카세이 가부시키가이샤 | Silica-based composite fine-particle dispersion, method for producing same, and polishing slurry including silica-based composite fine-particle dispersion |
US20230197296A1 (en) * | 2020-05-07 | 2023-06-22 | Westinghouse Electric Sweden Ab | A cladding tube for a fuel rod for a nuclear reactor, a fuel rod, and a fuel assembly |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2490571A (en) * | 1948-12-29 | 1949-12-06 | Metal Hydrides Inc | Pyrophoric alloy of zirconium, lead, and titanium, and sparking device containing the same |
-
1953
- 1953-07-17 US US376279A patent/US2746861A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2490571A (en) * | 1948-12-29 | 1949-12-06 | Metal Hydrides Inc | Pyrophoric alloy of zirconium, lead, and titanium, and sparking device containing the same |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2822302A (en) * | 1956-01-16 | 1958-02-04 | Radio Mfg Company Inc | Non-emissive electrode |
KR20190058715A (en) | 2015-03-31 | 2019-05-29 | 니끼 쇼꾸바이 카세이 가부시키가이샤 | Silica-based composite fine-particle dispersion, method for producing same, and polishing slurry including silica-based composite fine-particle dispersion |
KR20180134889A (en) | 2016-04-22 | 2018-12-19 | 니끼 쇼꾸바이 카세이 가부시키가이샤 | Dispersion of silica-based composite fine particles and production method thereof |
US20230197296A1 (en) * | 2020-05-07 | 2023-06-22 | Westinghouse Electric Sweden Ab | A cladding tube for a fuel rod for a nuclear reactor, a fuel rod, and a fuel assembly |
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