WO2022213545A1 - Zirconium alloy and preparation method therefor, cladding tube, and fuel assembly - Google Patents

Zirconium alloy and preparation method therefor, cladding tube, and fuel assembly Download PDF

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WO2022213545A1
WO2022213545A1 PCT/CN2021/117835 CN2021117835W WO2022213545A1 WO 2022213545 A1 WO2022213545 A1 WO 2022213545A1 CN 2021117835 W CN2021117835 W CN 2021117835W WO 2022213545 A1 WO2022213545 A1 WO 2022213545A1
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zirconium alloy
zirconium
alloy
niobium
cladding tube
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PCT/CN2021/117835
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French (fr)
Chinese (zh)
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陈刘涛
高长源
石林
张利斌
王旭
陈敏莉
陈汉森
邹红
聂立红
邓勇军
陈建新
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岭澳核电有限公司
中广核研究院有限公司
中国广核集团有限公司
中国广核电力股份有限公司
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Publication of WO2022213545A1 publication Critical patent/WO2022213545A1/en

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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C16/00Alloys based on zirconium
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/002Hybrid process, e.g. forging following casting
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/08Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tubular bodies or pipes
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/02Making non-ferrous alloys by melting
    • C22C1/03Making non-ferrous alloys by melting using master alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing 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
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/186High-melting or refractory metals or alloys based thereon of zirconium or alloys based thereon
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C3/00Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
    • G21C3/02Fuel elements
    • G21C3/04Constructional details
    • G21C3/06Casings; Jackets
    • G21C3/07Casings; Jackets characterised by their material, e.g. alloys
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors

Definitions

  • the invention relates to the technical field of nuclear fuel, in particular to a zirconium alloy and a preparation method thereof, a cladding tube and a fuel assembly.
  • Zirconium alloys are widely used as structural materials for nuclear fuel assemblies because of their small thermal neutron absorption cross-section, excellent corrosion resistance, radiation resistance and mechanical properties. Studies have shown that the existing zirconium alloys have strong creep resistance, but also have shortcomings in corrosion resistance.
  • the technical problem to be solved by the present invention is to provide a zirconium alloy with excellent corrosion resistance and creep resistance and a preparation method thereof, a cladding tube made of the zirconium alloy, and a fuel assembly having the cladding tube .
  • the technical scheme adopted by the present invention to solve the technical problem is: to provide a zirconium alloy, comprising the following components by mass percentage: niobium 0.48%-0.95%, tin 0.37%-0.75%, iron 0.03%-0.15%, vanadium 0-0. 0.15%, also including oxygen 1100ppm-1600ppm, the balance is Zr;
  • the present invention also provides a preparation method of the above-mentioned zirconium alloy, comprising the following steps:
  • the temperature of the forging is 800°C-1100°C.
  • the temperature of the beta quenching is 950°C-1100°C.
  • the temperature of the intermediate annealing is 550°C-600°C.
  • step S5 the billet is extruded or hot rolled before cold rolling.
  • the temperature of the final annealing is 440°C-600°C.
  • the preparation method further comprises the following steps:
  • the present invention also provides a cladding tube, which is made of the zirconium alloy described in any one of the above.
  • the present invention also provides a fuel assembly comprising the cladding tube described above.
  • the zirconium alloy of the present invention has more excellent corrosion resistance performance and creep resistance performance through the ratio of each component, and is suitable for the cladding, lattice and other components of the nuclear power plant reactor fuel assembly.
  • Guide tube to improve the service performance and safety of the fuel assembly.
  • the zirconium alloy of the present invention is a zirconium-tin-niobium alloy with a low content of transition metals, which comprises the following composition in mass percentage:
  • the zirconium alloy also includes: C (carbon) ⁇ 100ppm, N (nitrogen) ⁇ 45ppm. Understandably, some inevitable and small amounts of impurities are also included.
  • Nb niobium
  • studies have shown that the solid solution niobium in the zirconium alloy is beneficial to the corrosion resistance and creep resistance of the zirconium alloy, but the high content of niobium will be sensitive to heat treatment. Therefore, in the present invention, in order to ensure the zirconium alloy The alloy has excellent corrosion resistance and creep resistance.
  • the content of Nb is controlled at 0.48wt% to 0.95wt%, and the content of Nb, Fe, V is required to satisfy the relationship (Nb-0.45%) ⁇ Fe+ V, can ensure that enough niobium atoms are dissolved in the matrix, so as to ensure that the zirconium alloy has excellent corrosion resistance and creep resistance.
  • Tin (Sn) has a large solid solubility in zirconium. After a certain amount of tin is incorporated, the strength and creep resistance of zirconium alloys will be improved, but the addition of tin will reduce the uniform corrosion resistance of zirconium alloys. On the other hand, the addition of tin can improve the corrosion resistance of zirconium alloys in high Li concentration environments. In the present invention, after comprehensively considering corrosion resistance and creep resistance, the content of tin is controlled at 0.37wt% to 0.75wt%.
  • Iron (Fe) and vanadium (V) are transition metal elements, which can be added to the zirconium alloy to increase the corrosion resistance of the zirconium alloy.
  • the addition of vanadium can improve the hydrogen absorption resistance of the zirconium alloy.
  • Such transition metal elements such as iron and vanadium need to be added in an appropriate amount in zirconium alloys, and if they are added too much (over 0.2%), the corrosion resistance of zirconium alloys will decrease.
  • the content of elements such as Fe and V is strictly controlled, the Fe content is controlled at 0.03wt% to 0.15wt%, the V content is controlled at 0 to 0.15wt%, and the total amount of Fe and V in the zirconium alloy is controlled ⁇ 0.2wt%, to ensure that the zirconium alloy has sufficient corrosion resistance and sufficient oxidation resistance when serving in the stack.
  • the content of niobium, iron and vanadium satisfies (Nb-0.45%) ⁇ Fe+V, so as to ensure that enough Nb element is dissolved in the zirconium alloy, and tin is mixed, so that the zirconium alloy matrix is solid-dissolved in the zirconium alloy. Sufficient solid solution atoms, so that the alloy maintains excellent creep resistance.
  • the addition of oxygen (O) can improve the strength and creep resistance of the zirconium alloy, but as the oxygen content increases, the machinability of the zirconium alloy will decrease, especially the punching resistance. Therefore, the oxygen content is controlled at 1100ppm-1600ppm.
  • the preparation method of the zirconium alloy of the present invention may comprise the following steps:
  • the zirconium raw material uses nuclear grade sponge zirconium. Niobium, tin, iron and vanadium elements are added in the form of pure metals or master alloys.
  • the alloy ingot is forged into a billet at a temperature of 800°C-1100°C.
  • the temperature of ⁇ quenching is 950°C-1100°C, and the temperature is kept for a long enough time to make the whole billet reach the quenching temperature.
  • the billet after ⁇ quenching is subjected to multiple cold rolling, and intermediate annealing is performed between cold rolling.
  • the billet is extruded or hot rolled, and then the billet is subjected to at least 4 passes of cold rolling.
  • the temperature of the intermediate annealing is 550°C-600°C.
  • zirconium alloy When zirconium alloy is used as the cladding tube material, stress relief annealing or recrystallization annealing is preferred, and the annealing temperature is 440-600°C, and the prepared cladding has excellent corrosion resistance and sufficient creep resistance.
  • the prepared guide tube has excellent creep resistance and sufficient corrosion resistance.
  • the lattice strip prepared at an annealing temperature of 540-600°C has excellent creep resistance, radiation growth resistance and sufficient corrosion resistance.
  • the zirconium alloy profiles are prepared through the above steps S1-S6.
  • Zirconium alloys can also be made into sheets or tubes according to the needs of the application.
  • preparation method of the present invention may further comprise the following steps:
  • step S7 The zirconium alloy obtained in step S6 is processed into a cladding tube, a grid or a guide tube for use in a fuel assembly.
  • the above-mentioned zirconium alloy is made into a cladding tube of a fuel assembly.
  • the fuel assembly includes the above-mentioned cladding tube made of zirconium alloy, and also includes fuel pellets sealed in the cladding tube. Since the cladding tube is made of the above-mentioned zirconium alloy, the cladding tube has better corrosion resistance and creep resistance than the cladding tube made of the conventional Zr-4 alloy, thereby improving the service performance and safety of the fuel assembly.
  • the zirconium alloys of Examples 1 to 4 were prepared.
  • Table 1 shows the content of each component in the zirconium alloys of Examples 1 to 4 and Comparative Example 1.
  • the zirconium alloys and Zr-4 alloys (Zr-1.30Sn-0.20Fe-0.10Cr-0.12O) prepared in Examples 1 to 4 and Comparative Example 1 were used as Comparative Example 2 to conduct corrosion tests.
  • the corrosion test was carried out in an autoclave, the corrosion conditions were 360°C/18.6MPa/deionized water, and the test time was 130 days. The results are shown in Table 2 below.
  • the zirconium alloys prepared in Examples 1 to 4 and Comparative Example 1 and the Zr-4 alloy (Zr-1.30Sn-0.20Fe-0.10Cr-0.12O) as Comparative Example 2 were subjected to internal pressure creep tests.
  • the creep test was carried out on a professional creep machine, the temperature was 400°C, the hoop stress was 130MPa, and the test time was 240 hours. The results are shown in Table 3 below.
  • the zirconium alloys within the content range of each component of the present invention and satisfying the content relationship have excellent corrosion resistance performance and creep resistance performance, and are suitable for use as nuclear power plant reactor cladding materials. , lattice material and guide tube material.

Abstract

Disclosed are a zirconium alloy and a preparation method therefor, a cladding tube, and a fuel assembly. The zirconium alloy comprises the following components in percentages by mass: 0.48% to 0.95% of niobium, 0.37% to 0.75% of tin, 0.03% to 0.15% of iron, and 0 to 0.15% of vanadium, and further comprises 1100 ppm to 1600 ppm of oxygen and the balance of Zr, wherein the contents of niobium, iron and vanadium satisfy the following relationship: (Nb-0.45%)≥Fe+V and Fe+V≤0.2%. Due to the proportion of each component, the zirconium alloy of the present invention has a more excellent corrosion resistance and creep resistance compared with an existing Zr-4 alloy, and is suitable for cladding, grillwork and a guide tube of a fuel assembly of a nuclear power plant reactor and improves the service performance and safety performance of the fuel assembly.

Description

锆合金及其制备方法、包壳管及燃料组件Zirconium alloy and preparation method thereof, cladding tube and fuel assembly 技术领域technical field
本发明涉及核燃料技术领域,尤其涉及一种锆合金及其制备方法、包壳管及燃料组件。The invention relates to the technical field of nuclear fuel, in particular to a zirconium alloy and a preparation method thereof, a cladding tube and a fuel assembly.
背景技术Background technique
锆合金因其具有小的热中子吸收截面、优异的耐腐蚀性能、抗辐照性能及力学性能,被广泛用作核燃料组件结构材料。有研究表明,现有使用的锆合金在具有较强的抗蠕变性能的同时,在耐腐蚀性能方面存在不足。Zirconium alloys are widely used as structural materials for nuclear fuel assemblies because of their small thermal neutron absorption cross-section, excellent corrosion resistance, radiation resistance and mechanical properties. Studies have shown that the existing zirconium alloys have strong creep resistance, but also have shortcomings in corrosion resistance.
为满足燃料不断提高的需求,不能只在耐腐蚀性能或只在抗蠕变性能等单一方面上性能优异,有必要通过优化成分配比和添加其他元素开发出在耐腐蚀性能和抗蠕变性能都优良的锆合金。In order to meet the ever-increasing demand for fuels, it is not possible to excel only in corrosion resistance or creep resistance. It is necessary to optimize the composition ratio and add other elements. Zirconium alloy with excellent properties.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题在于,提供一种具有优异的耐腐蚀能性能和抗蠕变性能的锆合金及其制备方法、该锆合金制成的包壳管及具有该包壳管的燃料组件。The technical problem to be solved by the present invention is to provide a zirconium alloy with excellent corrosion resistance and creep resistance and a preparation method thereof, a cladding tube made of the zirconium alloy, and a fuel assembly having the cladding tube .
本发明解决其技术问题所采用的技术方案是:提供一种锆合金,包括以下质量百分比的成分:铌0.48%~0.95%、锡0.37%~0.75%、铁0.03%~0.15%、钒0~0.15%,还包括氧1100ppm-1600ppm,余量为Zr;The technical scheme adopted by the present invention to solve the technical problem is: to provide a zirconium alloy, comprising the following components by mass percentage: niobium 0.48%-0.95%, tin 0.37%-0.75%, iron 0.03%-0.15%, vanadium 0-0. 0.15%, also including oxygen 1100ppm-1600ppm, the balance is Zr;
其中,铌、铁和钒的含量满足以下关系:(Nb-0.45%)≥Fe+V、Fe+V≤0.2%。Wherein, the contents of niobium, iron and vanadium satisfy the following relationships: (Nb-0.45%)≥Fe+V, Fe+V≤0.2%.
优选地,所述锆合金中,C≤100ppm,N≤45ppm。Preferably, in the zirconium alloy, C≤100ppm, N≤45ppm.
本发明还提供一种上述的锆合金的制备方法,包括以下步骤:The present invention also provides a preparation method of the above-mentioned zirconium alloy, comprising the following steps:
S1、提供分别含有锆、铌、锡、铁和钒成分的原料,根据锆合金中各成分所占的质量百分比称取原料;S1. Provide raw materials containing zirconium, niobium, tin, iron and vanadium components respectively, and weigh the raw materials according to the mass percentage of each component in the zirconium alloy;
S2、将所述原料进行熔炼,制得合金锭;S2, smelting the raw material to obtain an alloy ingot;
S3、将所述合金锭锻造成坯料;S3, forging the alloy ingot into a billet;
S4、将所述坯料进行β淬火;S4, the blank is subjected to beta quenching;
S5、将经过β淬火后的坯料进行多次冷轧,冷轧之间进行中间退火;S5. The billet after β quenching is subjected to multiple cold rolling, and intermediate annealing is carried out between cold rolling;
S6、将经过冷轧后的坯料进行最终退火,制得锆合金。S6. Final annealing is performed on the cold-rolled billet to obtain a zirconium alloy.
优选地,步骤S3中,所述锻造的温度为800℃-1100℃。Preferably, in step S3, the temperature of the forging is 800°C-1100°C.
优选地,步骤S4中,所述β淬火的温度为950℃-1100℃。Preferably, in step S4, the temperature of the beta quenching is 950°C-1100°C.
优选地,步骤S5中,所述中间退火的温度为550℃-600℃。Preferably, in step S5, the temperature of the intermediate annealing is 550°C-600°C.
优选地,步骤S5中,进行冷轧之前将所述坯料进行挤压或热轧。Preferably, in step S5, the billet is extruded or hot rolled before cold rolling.
优选地,步骤S6中,所述最终退火的温度为440℃-600℃。Preferably, in step S6, the temperature of the final annealing is 440°C-600°C.
优选地,所述制备方法还包括以下步骤:Preferably, the preparation method further comprises the following steps:
S7、将所述锆合金加工成包壳管、格架或者导向管。S7, processing the zirconium alloy into a cladding tube, a lattice or a guide tube.
本发明还提供一种包壳管,采用以上任一项所述的锆合金制成。The present invention also provides a cladding tube, which is made of the zirconium alloy described in any one of the above.
本发明还提供一种燃料组件,包括以上所述的包壳管。The present invention also provides a fuel assembly comprising the cladding tube described above.
本发明的锆合金,通过各组分的配比,较于现有的Zr-4合金具有更优异的耐腐蚀能性能和抗蠕变性能,适用于核电站反应堆燃料组件的包壳、格架以及导向管,提高燃料组件的服役性能和安全性。Compared with the existing Zr-4 alloy, the zirconium alloy of the present invention has more excellent corrosion resistance performance and creep resistance performance through the ratio of each component, and is suitable for the cladding, lattice and other components of the nuclear power plant reactor fuel assembly. Guide tube to improve the service performance and safety of the fuel assembly.
具体实施方式Detailed ways
本发明的锆合金,为过渡族金属含量低的锆锡铌合金,其包括以下质量百分比的成分:The zirconium alloy of the present invention is a zirconium-tin-niobium alloy with a low content of transition metals, which comprises the following composition in mass percentage:
Nb(铌)0.48%~0.95%、Sn(锡)0.37%~0.75%、Fe(铁)0.03%~0.15%和V(钒)0~0.15%,还包括O(氧)1100-1600ppm,余量为Zr(锆)。Nb (niobium) 0.48%-0.95%, Sn (tin) 0.37%-0.75%, Fe (iron) 0.03%-0.15% and V (vanadium) 0-0.15%, also including O (oxygen) 1100-1600ppm, the remainder The amount is Zr (zirconium).
其中,铌、铁和钒的含量满足以下关系:(Nb-0.45%)≥Fe+V、Fe+V≤0.2%。Wherein, the contents of niobium, iron and vanadium satisfy the following relationships: (Nb-0.45%)≥Fe+V, Fe+V≤0.2%.
该锆合金还包括:C(碳)≤100ppm、N(氮)≤45ppm。可以理解地,还包括一些不可避免且量少的杂质。The zirconium alloy also includes: C (carbon)≤100ppm, N (nitrogen)≤45ppm. Understandably, some inevitable and small amounts of impurities are also included.
对于Nb(铌),研究表明,锆合金中固溶铌对锆合金的耐腐蚀性能和抗蠕变性能都有好处,但铌的含量过高会对热处理敏感,因此本发明中,为保证锆合金具有优良的耐腐蚀性能和抗蠕变性能,Nb的含量控制在0.48wt%~0.95wt%,并要求Nb、Fe、V三种元素的含量满足关系式(Nb-0.45%)≥Fe+V,能够保证基体中固溶足够的铌原子,从而保证锆合金具有优良的耐腐蚀性能和抗蠕变性能。For Nb (niobium), studies have shown that the solid solution niobium in the zirconium alloy is beneficial to the corrosion resistance and creep resistance of the zirconium alloy, but the high content of niobium will be sensitive to heat treatment. Therefore, in the present invention, in order to ensure the zirconium alloy The alloy has excellent corrosion resistance and creep resistance. The content of Nb is controlled at 0.48wt% to 0.95wt%, and the content of Nb, Fe, V is required to satisfy the relationship (Nb-0.45%) ≥ Fe+ V, can ensure that enough niobium atoms are dissolved in the matrix, so as to ensure that the zirconium alloy has excellent corrosion resistance and creep resistance.
锡(Sn)在锆中的固溶度较大,融入一定量的锡后,会提高锆合金的强度和抗蠕变性能,但是锡的添加会降低锆合金的耐均匀腐蚀能力。另一方面,锡的添加可以提高锆合金在高Li浓度环境下的耐腐蚀性能。本发明在综合考虑耐腐蚀性能和抗蠕变性能后,将锡的含量控制在0.37wt%~0.75wt%。Tin (Sn) has a large solid solubility in zirconium. After a certain amount of tin is incorporated, the strength and creep resistance of zirconium alloys will be improved, but the addition of tin will reduce the uniform corrosion resistance of zirconium alloys. On the other hand, the addition of tin can improve the corrosion resistance of zirconium alloys in high Li concentration environments. In the present invention, after comprehensively considering corrosion resistance and creep resistance, the content of tin is controlled at 0.37wt% to 0.75wt%.
铁(Fe)和钒(V)为过渡族金属元素,添加在锆合金中能够增加锆合金的耐腐蚀性能,其中钒元素的添加可提高锆合金的抗吸氢性能。铁、钒的该类过渡族金属元素在锆合金中需要适量添加,添加过多(超过0.2%)时,会导致锆合金的耐腐蚀性能有所下降。因此,本发明中,严格控制了Fe、V等 元素的含量,Fe含量控制在0.03wt%~0.15wt%,V含量控制在0~0.15wt%,并且Fe和V在锆合金中的总量≤于0.2wt%,保证锆合金有足够的耐腐蚀性能,在堆内服役时足够抗氧化。Iron (Fe) and vanadium (V) are transition metal elements, which can be added to the zirconium alloy to increase the corrosion resistance of the zirconium alloy. The addition of vanadium can improve the hydrogen absorption resistance of the zirconium alloy. Such transition metal elements such as iron and vanadium need to be added in an appropriate amount in zirconium alloys, and if they are added too much (over 0.2%), the corrosion resistance of zirconium alloys will decrease. Therefore, in the present invention, the content of elements such as Fe and V is strictly controlled, the Fe content is controlled at 0.03wt% to 0.15wt%, the V content is controlled at 0 to 0.15wt%, and the total amount of Fe and V in the zirconium alloy is controlled ≤ 0.2wt%, to ensure that the zirconium alloy has sufficient corrosion resistance and sufficient oxidation resistance when serving in the stack.
在本发明的锆合金中,铌、铁和钒的含量满足(Nb-0.45%)≥Fe+V,保证锆合金中固溶足够的Nb元素,并配合锡,从而使锆合金基体中固溶足够的固溶原子,从而使合金保持优异的抗蠕变性能。In the zirconium alloy of the present invention, the content of niobium, iron and vanadium satisfies (Nb-0.45%)≥Fe+V, so as to ensure that enough Nb element is dissolved in the zirconium alloy, and tin is mixed, so that the zirconium alloy matrix is solid-dissolved in the zirconium alloy. Sufficient solid solution atoms, so that the alloy maintains excellent creep resistance.
本发明的锆合金中,氧(O)的加入能够提高锆合金的强度和抗蠕变性能,但随着氧含量的升高,锆合金的可加工性会降低,特别是抗冲压性能。因此,氧的含量控制在1100ppm-1600ppm。In the zirconium alloy of the present invention, the addition of oxygen (O) can improve the strength and creep resistance of the zirconium alloy, but as the oxygen content increases, the machinability of the zirconium alloy will decrease, especially the punching resistance. Therefore, the oxygen content is controlled at 1100ppm-1600ppm.
本发明的锆合金的制备方法,可包括以下步骤:The preparation method of the zirconium alloy of the present invention may comprise the following steps:
S1、提供分别含有锆、铌、锡、铁和钒成分的原料,根据锆合金中各成分所占的质量百分比称取原料(配料计算)。S1. Provide raw materials containing zirconium, niobium, tin, iron and vanadium respectively, and weigh the raw materials according to the mass percentage of each component in the zirconium alloy (calculation of ingredients).
其中,锆原料使用核级海绵锆。铌、锡、铁和钒元素以纯金属或中间合金的形式添加。Among them, the zirconium raw material uses nuclear grade sponge zirconium. Niobium, tin, iron and vanadium elements are added in the form of pure metals or master alloys.
S2、将原料进行熔炼,制得合金锭。S2, smelting the raw material to obtain an alloy ingot.
将所有原料放入真空熔炼炉中进行熔炼,调节O、C和N的含量,最后制得合金锭。Put all the raw materials into a vacuum melting furnace for melting, adjust the content of O, C and N, and finally obtain an alloy ingot.
S3、将合金锭在800℃-1100℃的温度下锻造成坯料。S3, the alloy ingot is forged into a billet at a temperature of 800°C-1100°C.
S4、将坯料进行β淬火。S4, the blank is subjected to beta quenching.
其中,β淬火的温度为950℃-1100℃,并保温足够长时间使坯料整体到达淬火温度。Among them, the temperature of β quenching is 950℃-1100℃, and the temperature is kept for a long enough time to make the whole billet reach the quenching temperature.
S5、将经过β淬火后的坯料进行多次冷轧,冷轧之间进行中间退火。S5. The billet after β quenching is subjected to multiple cold rolling, and intermediate annealing is performed between cold rolling.
其中,根据所要形成的锆合金形态(如管材等)在冷轧之前,将坯料进行 挤压或热轧,再将坯料进行至少4道次冷轧。中间退火的温度为550℃-600℃。Wherein, according to the shape of the zirconium alloy to be formed (such as pipes, etc.), before cold rolling, the billet is extruded or hot rolled, and then the billet is subjected to at least 4 passes of cold rolling. The temperature of the intermediate annealing is 550°C-600°C.
S6、将经过冷轧后的坯料在440℃-600℃下进行最终退火,制得锆合金。S6. Final annealing is performed on the cold-rolled billet at 440° C.-600° C. to obtain a zirconium alloy.
当锆合金作为包壳管材料时,优选去应力退火或再结晶退火,退火温度为440-600℃,制得的包壳有优异的耐腐蚀性能和足够的抗蠕变性能。When zirconium alloy is used as the cladding tube material, stress relief annealing or recrystallization annealing is preferred, and the annealing temperature is 440-600°C, and the prepared cladding has excellent corrosion resistance and sufficient creep resistance.
当锆合金作为导向管材料时,优选再结晶退火,退火温度为540-600℃,制得的导向管有优异的抗蠕变性能和足够的耐腐蚀性能。When zirconium alloy is used as the guide tube material, recrystallization annealing is preferred, and the annealing temperature is 540-600° C. The prepared guide tube has excellent creep resistance and sufficient corrosion resistance.
当锆合金作为格架带材使用时,优选再结晶退火,退火温度为540-600℃制得的格架带材有优异的抗蠕变性能、抗辐照生长性能和足够的耐腐蚀性能。When a zirconium alloy is used as a lattice strip, recrystallization annealing is preferred. The lattice strip prepared at an annealing temperature of 540-600°C has excellent creep resistance, radiation growth resistance and sufficient corrosion resistance.
为便于将锆合金加工形成包壳管、导向管或格架带材等,通过上述步骤S1-S6,制得锆合金型材。In order to facilitate the processing of zirconium alloys into cladding tubes, guide tubes or grid strips, etc., the zirconium alloy profiles are prepared through the above steps S1-S6.
锆合金还可根据应用产品需要制成板材或管材。Zirconium alloys can also be made into sheets or tubes according to the needs of the application.
进一步地,本发明的制备方法还可包括以下步骤:Further, the preparation method of the present invention may further comprise the following steps:
S7、将步骤S6制得的锆合金加工成包壳管、格架或者导向管,以用于燃料组件。S7. The zirconium alloy obtained in step S6 is processed into a cladding tube, a grid or a guide tube for use in a fuel assembly.
在一应用实施方式中,将上述的锆合金制成燃料组件的包壳管。In an application embodiment, the above-mentioned zirconium alloy is made into a cladding tube of a fuel assembly.
对于燃料组件,包括上述的锆合金制成的包壳管,还包括密封在包壳管内的燃料芯块。由于包壳管由上述的锆合金制成,较于常规Zr-4合金制成的包壳管具有更优异的耐腐蚀能性能和抗蠕变性能,进而提高燃料组件的服役性能和安全性。The fuel assembly includes the above-mentioned cladding tube made of zirconium alloy, and also includes fuel pellets sealed in the cladding tube. Since the cladding tube is made of the above-mentioned zirconium alloy, the cladding tube has better corrosion resistance and creep resistance than the cladding tube made of the conventional Zr-4 alloy, thereby improving the service performance and safety of the fuel assembly.
以下通过具体实施例对本发明作进一步说明。The present invention will be further described below through specific embodiments.
根据本发明的制备方法制得实施例1-实施例4的锆合金,实施例1-实施例4及比较例1的锆合金中各成分含量如表1所示。According to the preparation method of the present invention, the zirconium alloys of Examples 1 to 4 were prepared. Table 1 shows the content of each component in the zirconium alloys of Examples 1 to 4 and Comparative Example 1.
表1Table 1
Figure PCTCN2021117835-appb-000001
Figure PCTCN2021117835-appb-000001
将实施例1-实施例4及比较例1制得的锆合金及Zr-4合金(Zr-1.30Sn-0.20Fe-0.10Cr-0.12O)作为比较例2进行腐蚀试验。腐蚀试验在高压釜上开展,腐蚀条件为360℃/18.6MPa/去离子水,试验时间为130天。结果如下表2所示。The zirconium alloys and Zr-4 alloys (Zr-1.30Sn-0.20Fe-0.10Cr-0.12O) prepared in Examples 1 to 4 and Comparative Example 1 were used as Comparative Example 2 to conduct corrosion tests. The corrosion test was carried out in an autoclave, the corrosion conditions were 360°C/18.6MPa/deionized water, and the test time was 130 days. The results are shown in Table 2 below.
表2Table 2
实施例Example 腐蚀量(mg/dm 2) Corrosion amount (mg/dm 2 )
11 45.8845.88
22 42.2942.29
33 44.1244.12
44 45.4245.42
比较例1Comparative Example 1 44.7544.75
比较例2Comparative Example 2 63.3063.30
从表2所示数据可知,实施例1-4及比较例1的锆合金均较于比较例2的Zr-4合金具有较高的耐腐蚀性能(更少的增重)。From the data shown in Table 2, it can be seen that the zirconium alloys of Examples 1-4 and Comparative Example 1 have higher corrosion resistance (less weight gain) than the Zr-4 alloy of Comparative Example 2.
将实施例1-实施例4及比较例1制得的锆合金及作为比较例2的Zr-4合金(Zr-1.30Sn-0.20Fe-0.10Cr-0.12O)进行内压蠕变试验。蠕变试验在专业的蠕变机上开展,温度为400℃,环向应力为130MPa,试验时间为240小时。结果如下表3所示。The zirconium alloys prepared in Examples 1 to 4 and Comparative Example 1 and the Zr-4 alloy (Zr-1.30Sn-0.20Fe-0.10Cr-0.12O) as Comparative Example 2 were subjected to internal pressure creep tests. The creep test was carried out on a professional creep machine, the temperature was 400°C, the hoop stress was 130MPa, and the test time was 240 hours. The results are shown in Table 3 below.
表3table 3
实施例Example 应变量(mm/mm)Strain (mm/mm)
11 0.700.70
22 0.440.44
33 0.810.81
44 0.510.51
比较例1Comparative Example 1 0.910.91
比较例2Comparative Example 2 1.791.79
从表3所示数据可知,实施例1-4的锆合金,由于其中满足(Nb-0.45%)≥Fe+V,较于比较例1的(Nb-0.45%)<Fe+V及比较例2的Zr-4合金显示出了较高的抗蠕变性能(更少的蠕变变形)。From the data shown in Table 3, it can be seen that the zirconium alloys of Examples 1-4 satisfy (Nb-0.45%)≥Fe+V, which is lower than that of Comparative Example 1 (Nb-0.45%)<Fe+V and Comparative Example The Zr-4 alloy of 2 shows higher creep resistance (less creep deformation).
可以理解地,本发明除了上述各实施例外,在本发明各成分含量范围内及满足含量关系式的锆合金,均具有优异的耐腐蚀能性能和抗蠕变性能,适用做核电站反应堆包壳材料、格架材料以及导向管材料。It can be understood that, in the present invention, except for the above-mentioned embodiments, the zirconium alloys within the content range of each component of the present invention and satisfying the content relationship have excellent corrosion resistance performance and creep resistance performance, and are suitable for use as nuclear power plant reactor cladding materials. , lattice material and guide tube material.
以上所述仅为本发明的实施例,并非因此限制本发明的专利范围,凡是利用本发明说明书内容所作的等效结构或等效流程变换,或直接或间接运用在其他相关的技术领域,均同理包括在本发明的专利保护范围内。The above descriptions are only the embodiments of the present invention, and do not limit the scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the description of the present invention, or directly or indirectly applied in other related technical fields, will not limit the scope of the invention. Similarly, it is included in the scope of patent protection of the present invention.

Claims (11)

  1. 一种锆合金,其特征在于,包括以下质量百分比的成分:铌0.48%~0.95%、锡0.37%~0.75%、铁0.03%~0.15%、钒0~0.15%,还包括氧1100ppm-1600ppm,余量为锆;A zirconium alloy is characterized by comprising the following components by mass percentage: niobium 0.48%-0.95%, tin 0.37%-0.75%, iron 0.03%-0.15%, vanadium 0-0.15%, and oxygen 1100ppm-1600ppm, The balance is zirconium;
    其中,铌、铁和钒的含量满足以下关系:(Nb-0.45%)≥Fe+V、Fe+V≤0.2%。Wherein, the contents of niobium, iron and vanadium satisfy the following relationships: (Nb-0.45%)≥Fe+V, Fe+V≤0.2%.
  2. 根据权利要求1所述的锆合金,其特征在于,所述锆合金中,C≤100ppm,N≤45ppm。The zirconium alloy according to claim 1, wherein, in the zirconium alloy, C≤100ppm and N≤45ppm.
  3. 一种权利要求1或2所述的锆合金的制备方法,其特征在于,包括以下步骤:A preparation method of zirconium alloy described in claim 1 or 2, is characterized in that, comprises the following steps:
    S1、提供分别含有锆、铌、锡、铁和钒成分的原料,根据锆合金中各成分所占的质量百分比称取原料;S1. Provide raw materials containing zirconium, niobium, tin, iron and vanadium components respectively, and weigh the raw materials according to the mass percentage of each component in the zirconium alloy;
    S2、将所述原料进行熔炼,制得合金锭;S2, smelting the raw material to obtain an alloy ingot;
    S3、将所述合金锭锻造成坯料;S3, forging the alloy ingot into a billet;
    S4、将所述坯料进行β淬火;S4, the blank is subjected to beta quenching;
    S5、将经过β淬火后的坯料进行多次冷轧,冷轧之间进行中间退火;S5. The billet after β quenching is subjected to multiple cold rolling, and intermediate annealing is carried out between cold rolling;
    S6、将经过冷轧后的坯料进行最终退火,制得锆合金。S6. Final annealing is performed on the cold-rolled billet to obtain a zirconium alloy.
  4. 根据权利要求3所述的锆合金的制备方法,其特征在于,步骤S3中,所述锻造的温度为800℃-1100℃。The method for preparing a zirconium alloy according to claim 3, wherein in step S3, the temperature of the forging is 800°C-1100°C.
  5. 根据权利要求3所述的锆合金的制备方法,其特征在于,步骤S4中,所述β淬火的温度为950℃-1100℃。The method for preparing a zirconium alloy according to claim 3, wherein in step S4, the temperature of the beta quenching is 950°C-1100°C.
  6. 根据权利要求3所述的锆合金的制备方法,其特征在于,步骤S5中,所述中间退火的温度为550℃-600℃。The method for preparing a zirconium alloy according to claim 3, wherein in step S5, the temperature of the intermediate annealing is 550°C-600°C.
  7. 根据权利要求3所述的锆合金的制备方法,其特征在于,步骤S5中,进行冷轧之前将所述坯料进行挤压或热轧。The method for preparing a zirconium alloy according to claim 3, wherein in step S5, the billet is extruded or hot rolled before cold rolling.
  8. 根据权利要求3所述的锆合金的制备方法,其特征在于,步骤S6中,所述最终退火的温度为440℃-600℃。The method for preparing a zirconium alloy according to claim 3, wherein in step S6, the temperature of the final annealing is 440°C-600°C.
  9. 根据权利要求3-8任一项所述的锆合金的制备方法,其特征在于,还包括以下步骤:The preparation method of zirconium alloy according to any one of claims 3-8, is characterized in that, also comprises the following steps:
    S7、将所述锆合金加工成包壳管、格架或者导向管。S7, processing the zirconium alloy into a cladding tube, a lattice or a guide tube.
  10. 一种包壳管,其特征在于,采用权利要求1或2所述的锆合金制成。A cladding tube, characterized in that it is made of the zirconium alloy according to claim 1 or 2.
  11. 一种燃料组件,其特征在于,包括权利要求10所述的包壳管。A fuel assembly is characterized by comprising the cladding tube of claim 10 .
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32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 29/02/2024)