US3125446A - Zirconium base alloy - Google Patents
Zirconium base alloy Download PDFInfo
- Publication number
- US3125446A US3125446A US3125446DA US3125446A US 3125446 A US3125446 A US 3125446A US 3125446D A US3125446D A US 3125446DA US 3125446 A US3125446 A US 3125446A
- Authority
- US
- United States
- Prior art keywords
- zirconium
- alloy
- base alloy
- zirconium base
- aluminum
- 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 48
- 239000000956 alloy Substances 0.000 title description 48
- 229910052726 zirconium Inorganic materials 0.000 title description 40
- REDXJYDRNCIFBQ-UHFFFAOYSA-N aluminium(3+) Chemical class [Al+3] REDXJYDRNCIFBQ-UHFFFAOYSA-N 0.000 title description 38
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 title description 36
- 229910052782 aluminium Inorganic materials 0.000 description 24
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 24
- ZOKXTWBITQBERF-UHFFFAOYSA-N molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 16
- 229910052750 molybdenum Inorganic materials 0.000 description 16
- 239000011733 molybdenum Substances 0.000 description 16
- 229910052790 beryllium Inorganic materials 0.000 description 14
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium(0) Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 14
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 14
- 229910052796 boron Inorganic materials 0.000 description 14
- 238000005260 corrosion Methods 0.000 description 12
- 238000002844 melting Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- -1 8.66% Chemical compound 0.000 description 4
- 239000000470 constituent Substances 0.000 description 4
- 239000012535 impurity Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910001295 No alloy Inorganic materials 0.000 description 2
- 229910001093 Zr alloy Inorganic materials 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 235000014121 butter Nutrition 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 231100000078 corrosive Toxicity 0.000 description 2
- 231100001010 corrosive Toxicity 0.000 description 2
- 230000003247 decreasing Effects 0.000 description 2
- 230000002939 deleterious Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 231100001004 fissure Toxicity 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 239000008188 pellet Substances 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 230000004580 weight loss Effects 0.000 description 2
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 present invention relates to an improved zirconium base alloy.
- a zirconium base alloy containing aluminum preferably one of aluminum.
- improved zirconium base alloys comprising from 3% to by weight, aluminum, and from 0.1% to 4%, by weight, molybdenum; in addition there may be present from .05 to 1%, by weight, of beryllium, and/ or up to 1% boron, and the balance being zirconium, with incidental amounts of impurities.
- the alloys are characterized by good corrosion behavior, high mechanical strength, and low temperature coefiicient of mechanical strength.
- Beryllium is a highly desirable constituent, especially when the zirconium base alloy is employed as a member in apparatus subjected to high temperature water and steam since it greatly improves the corrosion behavior of the alloy, in that, the alloy will deteriorate by oxidation less rapidly than similar zirconium alloys excluding beryllium in appreciable amounts.
- the alloy may be employed as a structural member in high temperature boilers and other apparatus wherein its combination of properties renders it highly useful.
- boron in amounts up to 1%, by weight, depending on the proportions of the other compo- 3,125,446 Patented Mar. 17, 1964 ice nents and it is found to be a highly effective strengthener when alloyed with the aforementioned elements in the zirconium base alloy.
- the alloy should be melted by any oneof several procedures which will ensure homogeneity and a minimum of contamination.
- un-alloyed, high purity, sponge zirconium together with the proper amounts of aluminum, molybdenum and boron can be fed into a conventional arc melting furnace containing an inert atmosphere.
- a tungsten electrode may be used.
- a consumable electrode consisting of the un-alloyed sponge zirconium combined with pellets or wire or other shapes of the alloying elements may be compacted to form the electrode, and then vacuum arc melted.
- the resulting ingot should be vacuum arc remelted once or twice using it as a consumable electrode, to achieve homogeneity, then may be hot worked to the desired shape.
- Example I An alloy of the following composition was prepared by double vacuum arc melting; aluminum, 8.66%, molybdenum,l.89%, beryllium, .42%, and boron .15 and zirconium balance with incidental amounts of impurities. Specimens of the resulting ingot survived fourteen days in both standard corrosion environments (680 F. water and 750 F. steam) without developing cracks, fissures or a flaking corrosion product. Other specimens of the ingot survived 200 days under the same conditions showing only a slight weight loss. Better results would normally be expected since examination showed more than the usual segregation of the boron constituent. Hardness readings taken on section specimens from the tested ingot ranged from 45 to 50 Rockwell C.
- Example II An ingot was prepared by consumable arc-melting of an alloy composed of 96% zirconium, 1% molybdenum and 3 aluminum. Hardness readings taken on section specimens from the tested ingot ranged from 33 to 35 Rockwell C at 25 C. Other hardness tests were made up to 1000 C., using Vickers 2 /2 kg. hardness numbers:
- Example 111 Tern erature, C Har ness No Alloys composed of 3% to 10% aluminum and from 0.05 to 1% beryllium have properties similar to alloys containing molybdenum.
- FOREIGN PATENTS A zirconium base alloy comprising from 3% to 10% 813,124 tB 't M 6,1959
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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)
Description
United States Patent 3,125,446 ZIRCONIUM BASE ALLOY Richard E. Johnson, Pittsburgh, Pa., and William D. McMullen, Ames, Iowa, assignors to Westinghouse Electric Corporation, East Pittsburgh, Pa., :1 corporation of Pennsylvania No Drawing. Filed Feb. 26, 1960, Ser. No. 11,120 1 Claim. (Cl. 75-177) The present invention relates to an improved zirconium base alloy. In particular it relates to a zirconium base alloy containing aluminum.
It has been heretofore proposed to alloy zirconium-with suitable elements to provide an alloy having high mechanical strength and good corrosion resistance. These endeavors have been successful to a certain extent. However, it has been acknowledged by those skilled in the art that aluminum in appreciable quantities has a deleterious effect upon zirconium base alloys especially when employed in, highly corrosive atmospheres.
It is an object of the present invention to provide a zirconium base alloy having predetermined proportions of aluminum, and molybdenum and beryllium and with or without boron, characterized by high mechanical strength, low corrosion rate, and low temperature coeflicient of mechanical strength.
Other objects of the invention will in part be obvious and will in part appear hereinafter.
1 In accordance with the present invention improved zirconium base alloys have been produced comprising from 3% to by weight, aluminum, and from 0.1% to 4%, by weight, molybdenum; in addition there may be present from .05 to 1%, by weight, of beryllium, and/ or up to 1% boron, and the balance being zirconium, with incidental amounts of impurities. The alloys are characterized by good corrosion behavior, high mechanical strength, and low temperature coefiicient of mechanical strength.
Aluminum in amounts of from 3% up to 10%, by weight, raises the range of stability of alpha-zirconium to a higher temperature, thus making it harder and stronger and more creep resistant than the alloy without aluminum at a given temperature. It also imparts to the zirconium base alloy a low temperature coefiicient of mechanical strength. That is, an increase in temperature renders a relatively slight decrease in hardness as compared to the same alloy without the aluminum. Molybdenum, on the other hand, while only slightly soluble in alpha-zirconium causes a considerable increase in strength and hardness in amounts up to about 4%, by weight. Molybdenum in amounts materially above 4% results in alloys having a decreased hardness and considerable loss in ductility. Beryllium is a highly desirable constituent, especially when the zirconium base alloy is employed as a member in apparatus subjected to high temperature water and steam since it greatly improves the corrosion behavior of the alloy, in that, the alloy will deteriorate by oxidation less rapidly than similar zirconium alloys excluding beryllium in appreciable amounts.
The alloy may be employed as a structural member in high temperature boilers and other apparatus wherein its combination of properties renders it highly useful.
It is permissible to add boron in amounts up to 1%, by weight, depending on the proportions of the other compo- 3,125,446 Patented Mar. 17, 1964 ice nents and it is found to be a highly effective strengthener when alloyed with the aforementioned elements in the zirconium base alloy.
The alloy should be melted by any oneof several procedures which will ensure homogeneity and a minimum of contamination. For example, un-alloyed, high purity, sponge zirconium together with the proper amounts of aluminum, molybdenum and boron can be fed into a conventional arc melting furnace containing an inert atmosphere. A tungsten electrode may be used. A consumable electrode consisting of the un-alloyed sponge zirconium combined with pellets or wire or other shapes of the alloying elements may be compacted to form the electrode, and then vacuum arc melted. The resulting ingot should be vacuum arc remelted once or twice using it as a consumable electrode, to achieve homogeneity, then may be hot worked to the desired shape.
The following examples are illustrative of the present invention. In these examples, percentages given for the composition are by weight.
Example I An alloy of the following composition was prepared by double vacuum arc melting; aluminum, 8.66%, molybdenum,l.89%, beryllium, .42%, and boron .15 and zirconium balance with incidental amounts of impurities. Specimens of the resulting ingot survived fourteen days in both standard corrosion environments (680 F. water and 750 F. steam) without developing cracks, fissures or a flaking corrosion product. Other specimens of the ingot survived 200 days under the same conditions showing only a slight weight loss. Better results would normally be expected since examination showed more than the usual segregation of the boron constituent. Hardness readings taken on section specimens from the tested ingot ranged from 45 to 50 Rockwell C.
Example II An ingot was prepared by consumable arc-melting of an alloy composed of 96% zirconium, 1% molybdenum and 3 aluminum. Hardness readings taken on section specimens from the tested ingot ranged from 33 to 35 Rockwell C at 25 C. Other hardness tests were made up to 1000 C., using Vickers 2 /2 kg. hardness numbers:
Temperature, C 200 400 500 600 700 800 1,000 Hardness No 270 223 192 141 62. 6 28. 8 2. 7
Example 111 Tern erature, C Har ness No Alloys composed of 3% to 10% aluminum and from 0.05 to 1% beryllium have properties similar to alloys containing molybdenum.
It will be understood that the above description is only exemplary and not in limitation of the invention.
We claim as our invention: FOREIGN PATENTS A zirconium base alloy comprising from 3% to 10% 813,124 tB 't M 6,1959
by weight aluminum, from 0.1% to 4% by weight molyb- Grea n am ay denum, from 0.05% to 1% by Weight beryllium, up to OTHER REFERENCES 1% boron and the balance zirconium with incidental 5 Zirconium 2nd edition y G L Miller 1957 p y amounts of lmpurmes Butter worths Scientific Publications, London (page 258 References Cited in the file of this patent relied upon). UNITED STATES PATENTS 3,005,706 Thomas et al Oct. 24, 1961 10
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Publication Number | Publication Date |
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US3125446A true US3125446A (en) | 1964-03-17 |
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US3125446D Expired - Lifetime US3125446A (en) | Zirconium base alloy |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4094706A (en) * | 1973-05-11 | 1978-06-13 | Atomic Energy Of Canada Limited | Preparation of zirconium alloys |
US4169743A (en) * | 1974-12-23 | 1979-10-02 | General Electric Company | Zirconium-base alloy nuclear fuel container and method |
US4197145A (en) * | 1974-12-23 | 1980-04-08 | General Electric Company | Zirconium-base alloy structural component for nuclear reactor and method |
US4226647A (en) * | 1973-05-11 | 1980-10-07 | Atomic Energy Of Canada Limited | Heat-treated zirconium alloy product |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB813124A (en) * | 1956-02-21 | 1959-05-06 | Atomic Energy Authority Uk | Improvements in or relating to the heat treatment of zirconium alloys |
US3005706A (en) * | 1958-05-27 | 1961-10-24 | Westinghouse Electric Corp | High strength alloys of zirconium |
-
0
- US US3125446D patent/US3125446A/en not_active Expired - Lifetime
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB813124A (en) * | 1956-02-21 | 1959-05-06 | Atomic Energy Authority Uk | Improvements in or relating to the heat treatment of zirconium alloys |
US3005706A (en) * | 1958-05-27 | 1961-10-24 | Westinghouse Electric Corp | High strength alloys of zirconium |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4094706A (en) * | 1973-05-11 | 1978-06-13 | Atomic Energy Of Canada Limited | Preparation of zirconium alloys |
US4226647A (en) * | 1973-05-11 | 1980-10-07 | Atomic Energy Of Canada Limited | Heat-treated zirconium alloy product |
US4169743A (en) * | 1974-12-23 | 1979-10-02 | General Electric Company | Zirconium-base alloy nuclear fuel container and method |
US4197145A (en) * | 1974-12-23 | 1980-04-08 | General Electric Company | Zirconium-base alloy structural component for nuclear reactor and method |
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