EP1688508B1 - Legierung auf der Basis von Zirkonium mit sehr guter Kriechfestigkeit - Google Patents

Legierung auf der Basis von Zirkonium mit sehr guter Kriechfestigkeit Download PDF

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EP1688508B1
EP1688508B1 EP05007163.8A EP05007163A EP1688508B1 EP 1688508 B1 EP1688508 B1 EP 1688508B1 EP 05007163 A EP05007163 A EP 05007163A EP 1688508 B1 EP1688508 B1 EP 1688508B1
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Prior art keywords
alloy
zirconium
ppm
creep
recrystallization
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EP1688508A1 (de
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Yong Hwan Jeong
Jong Hyuk Baek
Byoung Kwon Choi
Sang Yoon Park
Myung Ho Lee
Je Geon Bang
Jeong Yong Park
Jun Hwan Kim
Hyun Gil Kim
Youn Ho Jung
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Korea Atomic Energy Research Institute KAERI
Korea Hydro and Nuclear Power Co Ltd
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Korea Atomic Energy Research Institute KAERI
Korea Hydro and Nuclear Power Co Ltd
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    • 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18—High-melting or refractory metals or alloys based thereon
    • C22F1/186—High-melting or refractory metals or alloys based thereon of zirconium or alloys based thereon

Definitions

  • the present invention relates to a zirconium based alloy composite having an excellent creep resistance and, more particularly, to a zirconium based alloy composite finally heat-treated to have a degree of recrystallization in the range of 40 ⁇ 70% in order to improve the creep resistance.
  • a nuclear fuel cladding tube for nuclear power plant is one of the important parts for nuclear reactor core.
  • the cladding tube confines nuclear fuel and prevents nuclear fission products from flowing into cooling water.
  • the outer wall of c ladding tube is exposed to the cooling water at 320°C under the pressure of 15 MPa.
  • Composition of alloy is very important, because a cladding tube accompanies deterioration of mechanical properties by embrittlement and growth phenomena due to irradiation of neutrons and corrosive environment of high temperature and pressure.
  • Zirconium alloys such as Zircaloy -4, which have excellent mechanical strength at high temperature, creep resistance, corrosion resistance, thermal conductivity, and low absorption of neutrons, were developed in the early 1960's, and have generally been used up to now.
  • the conventional Zircaloy-4 cladding tube is faced with difficulties in use, because the nuclear power plant is being operated in the condition of high inflammation, long -term period, high temperature coolant and high pH, for the improvement of economical efficiency.
  • a new nuclear fuel cladding tube having highly improved reliability in the prevention of breakages and thermal allowance is required to enhance the stability and economical efficiency of nuclear reactor.
  • development of new alloy cladding tube is being carried out to improve the corrosion resistance and creep resistance.
  • the development of new alloy for cladding tube has a trend toward reducing or eliminating the content of tin(Sn) and adding niobium(Nb).
  • US Patent No. 5,832,050 disclosed a zirconium alloy composite and a manufacturing method thereof, which improved corrosion resistance and creep resistance by containing more than 96 wt.% zirconium and adding 8-100 ppm sulfur (hereinafter, % indicates weight percent).
  • the above patent has an independent claim describing the composition of zirconium alloy containing 8-100 ppm sulfur (preferably 8-30 ppm) and more than 96% zirconium, and 8 dependant claims for 8 alloys as follows.
  • US Patent Application Publication No. 2004/0018491 disclosed the following alloy composite with improved corrosion resistance by heat treatment for recrystallization and limiting the composition and size of precipitate, and a manufacturing method thereof.
  • Zirconium alloy containing (0.03 ⁇ 0.25% Fe) + one or more elements selected from 0.8 ⁇ 1.3% Cr, V, Nb, less than 2000 ppm Sn, 500-2000 ppm 0, less than 100 ppm C, 3-35 ppm S, and less than 50 ppm Si)
  • US Patent No. 5,254,308 disclosed an alloy containing niobium and iron to maintain the mechanical characteristic of alloy accor ding to the reduction of tin content.
  • the alloy comprises 0.45 ⁇ 0.75% Sn (preferably 0.6%), 0.4 ⁇ 0.53% Fe (preferably 0.45%), 0.2 ⁇ 0.3% Cr (preferably 0.25%), 0.3 ⁇ 0.5% Nb (preferably 0.45%), 0.012 ⁇ 0.03% Ni (preferably 0.02%), 50-200 ppm Si (preferably 100 ppm), and 1000-2000 ppm O (preferably 1600 ppm), where Fe/Cr ratio is controlled to 1.5, and addition of niobium is decided according to the iron content, which gives an influence to hydrogen absorption.
  • the alloy has been produced to have excel lent corrosion resistance and strength by controlling the contents of Ni, Si, C, and O.
  • US Patent No. 5,334,345 disclosed an alloy composites containing 1.0 ⁇ 2.0% Sn, 0.07 ⁇ 0.70% Fe, 0.05 ⁇ 0.15% Cr, 0.16 ⁇ 0.40% Ni, 0.015 ⁇ 0.30% Nb (preferably 0.015 ⁇ 0.20%), 0.002 ⁇ 0.05% Si (preferably 0.015 ⁇ 0.05%), and 900-1600 ppm O to improve the corrosion resistance and hydrogen absorption resistance.
  • US Patent No. 5,334,345 disclosed an alloy composites containing 1.0 ⁇ 2.0% Sn, 0.07 ⁇ 0.70% Fe, 0.05 ⁇ 0.15% Cr, 0.16 ⁇ 0.40% Ni, 0.015 ⁇ 0.30% Nb (preferably 0.015 ⁇ 0.20%), 0.002 ⁇ 0.05% Si (preferably 0.015 ⁇ 0.05%), and 900-1600 ppm O to improve the corrosion resistance and hydrogen absorption resistance.
  • 5,366,690 disclosed an alloy composite containing 0 ⁇ 1.5% Sn (preferably 0.6%), 0 ⁇ 0.24% Fe (preferably 0.12%), 0-0 .15% Cr (preferably 0.10%), 0-2300 ppm N, 0-100 ppm Si (preferably 100 ppm), 0-1600 ppm oxygen (preferably 1200 ppm), and 0 ⁇ 0.5% Nb (preferably 0.45%) by mainly controlling the contents of Sn, N, and Nb.
  • US Patent No. 5,211,774 disclosed a zirconium alloy composite developed for the purpose of improving ductility, creep strength and corrosion resistance in the environment of neutron irradiation.
  • the alloy is formed in the composition of 0.8 ⁇ 1.2% Sn, 0.2 ⁇ 0.5% Fe (preferably 0.35%), 0.1 ⁇ 0.4% Cr (preferably 0.25%), 0 ⁇ 0.6% Nb, 50-200 ppm Si (preferably 50ppm), and 900-1800 ppm O (preferably 1600ppm), and the decrease of corrosion resistance due to hydrogen absorption and difference of process is prevented by controlling the silicon content.
  • European Patent No . 195,155 disclosed a duplex cladding tube using a zirconium alloy , which contains 0.1 ⁇ 0.3% Sn, 0.05 ⁇ 0.2% Fe, 0.05 ⁇ 0.4% Nb, 0.03 ⁇ 0.1% Cr and/or Ni, where in Fe+Cr+Ni content should not exceed 0.25% and oxygen content is 300-1200 ppm.
  • 5,080,861 disclosed a zirconium alloy containing 0 ⁇ 0.6% Nb, 0 ⁇ 0.2% Sb, 0 ⁇ 0.2% Te, 0.5 ⁇ 1.0% Sn, 0.18 ⁇ 0.24% Fe, 0.07 ⁇ 0.13% Cr, 900-2000 ppm O, 0-70 ppm Ni, and 0-200 ppm C to improve the corrosion resistance of alloy in high inflammati on. It is reported that the size of precipitate is limited in 1200-1800 A and up to 2% bismuth may be added instead of tellurium or antimony.
  • European Patent No. 345,531 disclosed a similar composition of zirconium alloy to the above patent.
  • the alloy is formed in the composition of 0 ⁇ 0.6% Nb, 0 ⁇ 0.1% Mo, 1.2 ⁇ 1.70% Sn, 0.07-0. 24% Fe, 0.05 ⁇ 0.13% Cr, 0 ⁇ 0.08% Ni, and 900-1800 ppm O.
  • European Patent No. 532,830 disclosed a zirconium alloy containing 0 ⁇ 0.6% Nb, 0.8 ⁇ 1.2% Sn, 0.2-0.5% Fe (preferably 0.35%), 0.1 ⁇ 0.4% Cr (preferably 0.25%), 50-200 ppm Si (preferably 100ppm), and 900-1800 ppm O (preferably 1600ppm) for the improvement of corrosion resistance, irradiation stability, mechanical strength and creep resistance of alloy.
  • 2,624,136 disclosed a zirconium alloy by adding both Nb and V, which contains 0.1 ⁇ 0.35% Fe, 0.1 ⁇ 0.4% V, 0.05 ⁇ 0.3% O, 0 ⁇ 0.25% Sn, 0 ⁇ 0.25% Nb, and more than 0.5% V/Fe, and an optimum manufacturing method of alloy.
  • Japanese Patent No. 62,180,027 disclosed a zirconium alloy containing 1.7 ⁇ 2.5% Nb, 0.5 ⁇ 2.2% Sn, 0.04 ⁇ 1.0% Fe to improve the mechani cal strength and nodular corrosion resistance of allo y, where Fe+Mo content is limited in 0.2 ⁇ 1.0%.
  • Japanese Patent No. 2,213,437 disclosed niobium added alloys based on Zr-Sn-Fe-V alloy also to improve the nodular corrosion resistance , This patent sugges ted an alloy composite containing 0.25 ⁇ 1.5% Zr, 0.15 ⁇ 1.0% Nb, and Fe, and another alloy composite containing 0.25 ⁇ 1.5% Zr, 0.5 ⁇ 1.0% Nb, 0.05 ⁇ 0.15% Sn, and Ni.
  • 62,207,835 disclosed a ternary alloy containing 0.2 ⁇ 2.0% Zr, 0.5 ⁇ 3.0 Nb %, 9 00-2500 ppm Sn, and O.
  • Japanese Patent No. 62,297,449 disclosed an alloy containing 1 ⁇ 2.5% Nb, 0.5 ⁇ 2.0% Sn, 0.1 ⁇ 1.0% Mo, 1.5 ⁇ 2.5% Mo+Nb to improve corrosion resistance, ductility and strength, and a manufacturing method by solution heat -treatment in ⁇ + ⁇ or ⁇ -phase.
  • Japanese Patent No. 62,180,027 disclosed an alloy having a similar composition of 1.7 ⁇ 2.5% Nb, 0.5 ⁇ 2.2% Sn, 0.04 ⁇ 1.0% Fe, 0.2 ⁇ 1.0% Mo, 0.2 ⁇ 1.0% Fe+Mo , where Fe is further added.
  • US Patent No. 4,863,685 , No. 4,986,975 , No. 5,024,809 , and No. 5,026,516 disclosed zirconium alloys containing 0.5 ⁇ 2.0% Sn and about 0.5 ⁇ 1.0% other solute atoms. These alloy s further contain 0.09 ⁇ 0.16% oxygen.
  • the alloy in accordance with US Patent No. 4,863,685 contains tin and other solute atoms such as Mo, Te, mixture thereof, Nb-Te, or Nb-Mo.
  • the alloy composite in accordance with US Patent No. 4,986,975 contains solute atoms such as Cu, Ni, and Fe, wherein the content of solute atoms is limited in the range of 0.24 ⁇ 0.40% and at least 0.05% Cu should be added.
  • US Patent No. 4,938,920 intended to develop an alloy with improved corrosion resistance by modifying conventional Zircaloy-4. This patent reduces Sn content to 0 ⁇ 0.8% and adds 0 ⁇ 0.3% V and 0 ⁇ 1% Nb, wherein Fe content is 0.2 ⁇ 0.8%, Cr content is 0-0.4%, and Fe+Cr+V content is limited in 0.2 5 ⁇ 1.0%. Additionally, oxygen content is 1000-1600 ppm.
  • alloy having the composition of 0.8%Sn-0.22%Fe-0.11%Cr-0.14%0, 0.4%Nb - 0.67%Fe-0.33%Cr-0.15%O, 0.75%Fe -0.25%V-0.1%O, or 0.25%Sn - 0.2%Fe-0.15%V-0.1%0 under the condition of 400°C for 200 days in steam atmosphere , the alloy showed an excellent corrosion resistance.
  • the corrosion of alloy was about 60% to that of Zircaloy-4, and tensile strength of the alloy was similar to that of Zircaloy-4.
  • US Patent No. 4,963,323 or Japanese Pate nt No. 1,188,646 modified alloy composition of the conventional Zircaloy-4 in order to develop a nuclear cladding material having improved corrosion resistance Sn content is reduced , and Nb is added to compensate the strength loss due t o the reduction of Sn , maintaining nitrogen content below 60 ppm.
  • the alloy has the composition of 0.2 ⁇ 1.15% Sn, 0.19 ⁇ 0.6% Fe (preferably 0.19 ⁇ 0.24%), 0.07 ⁇ 0.4% Cr (preferably 0.07 ⁇ 0.13%), 0.05 ⁇ 0.5% Nb, and less than 60 ppm N. Additionally, US Patent No.
  • 5,017,336 controlled the alloy composition of Zircaloy-4 by adding Nb, Ta, V, and Mo, and suggested a zirconium alloy containing 0.2 ⁇ 0.9% Sn, 0.18 ⁇ 0.6% Fe, 0.07 ⁇ 0.4% Cr, 0.05 ⁇ 0.5% Nb, 0.01 ⁇ 0.2% Ta, 0.05 ⁇ 1% V, and 0.05 ⁇ 1% Mo.
  • US Patent No. 5,196,163 or Japanese Patent No. 63,035,751 also modified alloy composition of the conventional Zircaloy-4 by adding Ta as well as Sn, Fe, and Cr, and by selectively adding Nb.
  • the patent disclosed zirconium alloy containing 0.2 ⁇ 1.15% Sn, 0.19 ⁇ 0.6% Fe (preferably 0.19 ⁇ 0.2 4%), 0.07 ⁇ 0.4% Cr (preferably 0.07 ⁇ 0.13%), 0.01 ⁇ 0.2% Ta, 0.05 ⁇ 0.5% Nb, and less than 60 ppm N.
  • French Patent No. 2,769,637 disclosed a similar composition of zirconium alloy to the above patents , containing 0.2 ⁇ 1.7% Sn, 0.18 ⁇ 0.6% Fe, 0.07 ⁇ 0.4% Cr, 0.05 ⁇ 1.0% Nb, and selectively 0.01 ⁇ 0.1% Ta or less than 60 ppm N. Additionally, this patent presented heat -treatment factors with regard to the composition.
  • US Patent No. 5,560,790 disclosed an alloy composite containing 0.5 ⁇ 1.5% Nb, 0.9 ⁇ 1.5% Sn, 0.3 ⁇ 0.6% Fe, 0.005 ⁇ 0.2% Cr, 0.005 ⁇ 0.04% C, 0.05 ⁇ 0.15% O, and 0.005 ⁇ 0.015% Si, wherein the distance between precipitates of (Zr(Nb,Fe) 2 , Zr(Fe,Cr,Nb), (Zr,Nb) 3 Fe) containing Sn or Fe is 0.20 ⁇ 0.40 ⁇ m, and the precipitate containing Fe is limited to 60% by volume of total precipitate.
  • Japanese Patent No. 5,214,500 suggested an alloy composite and size of precipitate in order to improve the corrosion resistance.
  • the alloy composite contains 0.5 ⁇ 2.0% Sn, 0.05 ⁇ 0.3% Fe, 0.05 ⁇ 0.3% Cr, 0.05 ⁇ 0.15% Ni, 0.05 ⁇ 0.2% O, 0 ⁇ 1.2% Nb , and the balance Zr, wherein the average size of precipitate is limited to below 0.5 ⁇ m.
  • Japanese Patent No. 8,086,954 suggested heat -treatment factors induced in the hot/cold-working of ⁇ -phase and disclosed a zirconium alloy composite containing 0.4 ⁇ 1.7% Sn, 0.25 ⁇ 0.75% Fe, 0.05 ⁇ 0.30% Cr, 0 ⁇ 0.10% Ni, and 0 ⁇ 1.0% Nb.
  • Japanese Patent No. 9,111,379 suggested a zirconium alloy containing 0.5 ⁇ 1.7% Sn, 0.1 ⁇ 0.3% Fe, 0.05 ⁇ 0.02% Cr, 0.05 ⁇ 0.2% Cu, 0.01 ⁇ 1.0% Nb, and 0.01 ⁇ 0.20% Ni to avoid nodular corrosion.
  • Japanese Patent No. 10,273,746 suggested a zirconium alloy containing 0.3 ⁇ 0.7% Sn, 0.2 ⁇ 0.25% Fe, 0.1 ⁇ 0.15% Cr, and 0.05 ⁇ 0.20% Nb to improve the processability and corrosion resistance of alloy.
  • European Patent No. 198,570 limited the niobium content in 1 ⁇ 2.5% in a binary alloy formed of Zr-Nb, and suggested a heat -treatment temperature in a manufacturing process of alloy, wherein the second phase containing Nb should be uniformly distributed and the size of the second phase should be maintained below 800 A.
  • US Patent No. 5,125,985 suggested an alloy containing 0.07 ⁇ 0.28% of one or more elements selected from 0.5 ⁇ 2.0% Nb, 0.7 ⁇ 1.5% Sn, Fe, Ni, and Cr, and stated that the creep characteristic of material may be controlled by utilizing various manufacturing processes , where in one of the characteristics in manufacturing process is to utilize ⁇ -quenching heat-treatment as an intermediate process.
  • zirconium alloys such as Zircaloy -4 have been carried out.
  • nuclear power plants are presently operated in a severe condition to increase the economical efficiency, and thereby a nuclear cladding tube manufactured with conventional alloy such as Zircaloy-4 reached the limit of use. Therefore, it is necessary to develop a new zirconium alloy having more excellent creep resistance.
  • An object of the present invention is to provide a zirconium alloy having an excellent creep resistance, which has higher stability and economical efficiency than a conventional material, by minimizing creep deformation of cladding tube or reactor core structures during the operation of light or heavy water reactor in the nuclear power plant.
  • the present invention provides a zirconium alloy according to claim 1.
  • a zirconium alloy having a very excellent creep resistance may be manufactured by use of the zirconium alloy composite with the degree of recrystallization maintained in the range of 40 ⁇ 70% by controlling final heat-treatment in vacuum, in accordance with the present invention
  • Niobium(Nb) improves the corrosion resistance of zirconium alloy.
  • solid solubility about 0.3-0.6%
  • the improvement of corrosion resistance may be obtained only when the composition and size of precipitate are properly controlled.
  • mechanical characteristic of alloy is improved by high precipitation when niobium is added above the solid solubility .
  • alloy performance becomes more sensitive to the con dition of heat-treatment, in the case that a large amount of precipitate is formed. Therefore, the niobium content must be in the range of 0.8 ⁇ 1.8 wt.%.
  • Tin(Sn) is known as a ⁇ -phase stabilizing element in the zirconium alloy, and improves mechanical strength by solution strengthening. However, it shows that corrosion of alloy is very rapidly accelerated in the environment of LiOH, if tin is not added at all. Accordingly, the present invention preferably controls the tin content in the range of 0.38 ⁇ 0.50 wt.% according to the content of niobium, where the content of tin does not give a great influence to the reduction of corrosion resistance.
  • Iron(Fe) is a major element added to the alloy to improve the corrosion resistance .
  • the present invention preferably adds iron in the range of 0.05 ⁇ 0.2 wt.% and, more preferably, in 0.1 ⁇ 0.2 wt.%.
  • Chromium(Cr) is also a major element added to the alloy to improve the corrosion resistance like Fe.
  • the present invention preferably adds chromium in the range of 0.05 ⁇ 0.2 wt.% and, more preferably, at 0.12 wt.%.
  • Copper(Cu) is also a major element added to the alloy to improve the corrosion resistance like iron and chromium, and has an excellent effect when added in a small amount. Accordingly, the present invention limits the content of copper in the range of 0.05 ⁇ 0.2 wt.% and, more preferably in the range of 0.05 ⁇ 0.15 wt.%.
  • Oxygen(O) contributes to the improvement of mechanical strength and creep resistance by solution strengthening.
  • the present invention preferably controls the content of oxygen in the range of 1000-1500 ppm (0.1-0.15 wt.%), because a problem may occur when an excessive amount is added.
  • Carbon(C) and silicon(Si) reduce hydrogen absorption and delay transition time of corrosion speed. Additionally, these two elements are impurity elements having a relationship with the corrosion resistance, and are added in the range of 60-100 ppm (0.006-0.010 wt.%).
  • Sulfur(S) is an impurity element contributing to the improvement of creep resistance without affecting corrosion characteristic when used below 30 ppm.
  • the sulfur is added more than 0.0020 wt.%, creep deformation is no more decreased. Accordingly, the present invention controls the content of sulfur in the range of 6-20 ppm (0.0006-0.0020 wt.%) to improve the creep resistance.
  • the zirconium alloy having an excellent creep resistance in accordance with the present invention may be manufactured by controlling the degree of recrystallization of alloy in the range of 40-70%.
  • the zirconium alloy having an excellent creep resistance in accordance with the present invention may be manufactured by a conventional method in the field of invention, however, more preferably, the zirconium alloy is manufactured by final heat -treatment controlling the degree of recrystallization in the range of 40-70%, after ⁇ -heat-treatment and cold-working.
  • the manufacturing method of zirconium alloy composite in accordance with the present invention comprises the steps of: destroying structure of individual zirconium alloy ingots having the above composition by forging in ⁇ -phase; ⁇ -quenching which performs rapid cooling after solution heat -treatment in ⁇ -phase to homogenize the alloy composite, wherein the ⁇ -quenching process is performed to disperse precipitate uniformly in a metal matrix and to control the size of precipitate; hot-rolling the ⁇ -quenched material; heat -treating in vacuum between four times of cold-working; and final heat-treating in vacuum by co ntrolling the degree of recrystallization in the range of 40 ⁇ 70%.
  • the final heat -treatment process is preferably performed at 470-570°C for 3-8 hours under monitoring of the degree of recrystallization of metal within the range of 40 ⁇ 70%.
  • the creep resistance of zirconium alloy in accordance with the present invention may be improved by controlling the degree of recrystallization of alloy in the range of 40-70%, and thereby the zirconium alloy composite has an excel lent creep resistance.
  • the safety and economical efficiency of zirconium alloy composite in accordance with the present invention may be much improved by minimizing the creep deformation, compared to a conventional material.
  • the zirconium alloy composite in accordance with the present invention may be effectively used as a nuclear cladding tube, supporting lattice, and material for the structures of reactor core in the nuclear power plant utilizing light or heavy water react or.
  • the safety of nuclear fuel rod may be secured in the reactor core operating in high inflammation and long -term period by using the zirconium alloy composite in accordance with the present invention as the above structural material.
  • compositions of the above 13 alloys are arranged as the following table 1, where % indicates weight percent. Table 1.
  • Alloys 5 to 9 are embodiments of the invention Examples of alloy Composition (wt.%) Remarks
  • Example 1 Zr-0.8Nb-0.07Cu-0.140-0.008C-0.008Si-0.002S PRX
  • Example 2 Zr-1.1Nb-0.07Cu-0.140-0.008C-0.008Si-0.002S PRX
  • Example 3 Zr-1.5Nb-0.07Cu-0.140-0.008C-0.008Si-0.002S PRX
  • Example 4 Zr-1.8Nb-0.07Cu-0.140-0.008C-0.008Si-0.002S PRX
  • Example 5 Zr-1.5Nb-0.4Sn-0.140-0.008C-0.008Si-0.002S PRX
  • Example 6 Zr-1.5Nb-0.4Sn-0.1Cu-0.140-0.008C-0.008Si-0.002S PRX
  • Example 7 Zr
  • Ingots are manufactured by melting the zirconium having the above compositions, and then forged at 1000-1200°C in ⁇ -phase to destroy the ingot structure. Subsequently, solution heat -treatment is performed at 1015-1075°C to distribute atoms of the alloy more uniformly, and rapid cooling is performed to obtain ⁇ -quenched structure (martensite).
  • the ⁇ -quenched material is hot-rolled at 590 °C with the reduction rate of 70% followed by a first cold -working with the reduction rate of 50%, and heat -treatment in vacuum is performed at 570 ⁇ 580°C for 3 hours.
  • test pieces heat -treated in vacuum are processed through 3 times of cold -working, wherein interm ediate heat -treatment between the cold - working is performed at 570 °C for 2 hours.
  • test pieces of zirconium alloy in a substrate form are manufactured by final heat -treatment at 510 °C for 3-8 hours.
  • the test pieces of example s 2, 3, 7, 8, and 9 in a substrate form are manufactured to evaluate the creep characteristic with regard to the degree of recrystallization controlled by the final heat -treatment condition at intervals of 20°C from 470°C to 570°C.
  • the present invention co ntrols the degree of recrystallization in the range of 40-70% by properly selecting the temperature and time of heat -treatment.
  • the degree of recrystallization is calculated by analyzing a number of micro -structural photos (minimum 5 cuts) of metal matrix taken by transmission electron microscope with image analyzer, and by taking an average value.
  • Fig. 1 shows the change of the degree of recrystallization according to the heat-treatment temperature, when the temperature of final heat-treatment is changed in the manufacturing process of zirconium alloy. It showed a trend that the degree of recrystallization increases along S -curve as the heat treatment temperature increases under the condition of heat-treatment for a designated time.
  • EXPREIMENT 2 Creep test with regard to the degree of recrystallization of zirconium alloy
  • the creep deformation has a tendency to decrease as the degree of recrystallization increases, and all the alloys having the degree of recrystallization of 40 ⁇ 70% showed minimum creep deformation. However, the creep deformation has an adverse tendency to increase, when the degree of recrystallization is out of the above range. This indicates that the creep characteristic of zirconium alloy has a close relationship with the potential distribution in a matrix structure. The resistance to creep deformation is most excellent when the degree of recrystallization is contr olled in medium level of about 40 ⁇ 70%.
  • Examples 5 to 9 are in accordance with example embodiments Degree of recrystallization % Creep deformation rate, % 350 ⁇ /120MPa ⁇ 192 h 350 ⁇ /120MPa ⁇ 7200 h
  • Example 1 68 0.31 0.62
  • Example 2 60 0.26 0.53
  • Example 3 53 0.24 0.51
  • Example 4 42 0.22 0.48
  • Example 5 48 0.19 0.45
  • Example 6 50 0.17 0.43
  • Example 7 49 0.21 0.46
  • Example 9 44 0.23 0.47
  • Example 12 59 0.27 0.54 Example 13 57 0.25 0.52 Zircaloy-4 8 0.72 1.12
  • the creep deformation of alloys having the compositions in examples 1-4, where the niobium content is chang ed in the range of 0.8 ⁇ 1.8 wt.% showed low values of 0.22 ⁇ 0.31% and 0.48 ⁇ 0.62% respectively under the condition of 192 hours and 7200 hours, which are lower than that of commercial Zircaloy-4.
  • Zr-1.5%Nb-0.4%Sn alloys having the compositions in accordance with example embodiments 5-9 showed excellent creep resistances due to addition of tin.
  • the creep deformation of alloys having the compositions in accordance with example 10-13 has been evaluated. As shown in Table 3, the creep deformation has an apparent tendency to decrease as the addition of sulfur increases, and the creep deformation doesn 't decrease any more when 0.002 wt.% sulfur is added. This ind icates that the creep resistance is most effectively improved when sulfur is added in the range of 0.0006 ⁇ 0.0020 wt.%.
  • the zirconium alloy in accordance with the present invention has an excellent creep resistance by controlling the temperature and time of final heat -treatment to maintain the degree of recrystallization in 40-70%, and has a better creep resistance than Zicaloy-4 as a conventional and commercial nuclear cladding ma terial. Additionally, the degree of recrystallization disclosed in the present invention may be applied to a manufacturing method of zirconium alloy having an excellent creep resistance, and will make a great contribution to the improvement of creep resistance.
  • the zirconium alloy in accordance with the present invention will significantly improve the safety and economical efficiency by minimizing the creep deformation in high inflammation and long -term operation condition, and may effectively be used as a nuclear cladding tube, supporting lattice, and material for the structures of reactor core in the nuclear power plant utilizing light or heavy water reactor.
  • the zirconium alloy in accordance with the present invention may replace Zircaloy-4 being used as a conventional nuclear cladding material.

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Claims (2)

  1. Legierung auf Basis von Zirkonium, umfassend:
    0,8-1,8 Gew.-% Niob; 0,38-0,50 Gew.-% Zinn; 0,10-0,15 Gew.-% Sauerstoff; 0,006-0,010 Gew.-% Kohlenstoff; 0,006-0,010 Gew.-% Silizium; 0,0005-0,0020 Gew.-% Schwefel; ein oder mehrere Elemente, ausgewählt aus 0,05-0,2 Gew.-% Eisen, 0,05-0,2 Gew.-% Kupfer und 0,05-0,2 Gew.-% Chrom; und der Ausgleich Zirkonium.
  2. Legierung auf Basis von Zirkonium nach Anspruch 1, wobei der Rekristallisationsgrad der Zirkoniumlegierung im Bereich von 40-70% geregelt ist.
EP05007163.8A 2005-02-07 2005-04-01 Legierung auf der Basis von Zirkonium mit sehr guter Kriechfestigkeit Not-in-force EP1688508B1 (de)

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KR100733701B1 (ko) 2007-06-28
CN1818111A (zh) 2006-08-16
JP4099493B2 (ja) 2008-06-11
CN1818111B (zh) 2010-12-22
US20060177341A1 (en) 2006-08-10
JP2006214001A (ja) 2006-08-17
EP1688508A1 (de) 2006-08-09

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