CONTROL ROD FOR NUCLEAR REACTOR AND METHOD OF MANUFACTURING CONTROL ROD
    1.
    发明申请
    CONTROL ROD FOR NUCLEAR REACTOR AND METHOD OF MANUFACTURING CONTROL ROD 有权
    核反应堆的控制杆和制造控制杆的方法

    公开(公告)号:US20080205574A1

    公开(公告)日:2008-08-28

    申请号:US12034966

    申请日:2008-02-21

    IPC分类号: G21C7/08

    摘要: A control rod for nuclear reactors includes four wings including neutron absorbers containing hafnium, a front end structural member which has a cross shape in cross section and includes brackets bonded to the leading ends of the wings, and a terminal end structural member which has a cross shape in cross section and includes brackets bonded to the tailing ends of the wings. The four wings are bonded to a wing-bonding member including a cross-shaped center shaft so as to form a cross shape. The front end structural member and the wing-bonding member are made of a zirconium alloy. The wings include neutron-absorbing plates having neutron-absorbing portions and each have an outer surface which is opposed to a fuel assembly and at which a hafnium-zircaloy composite member covered with zircaloy is disposed. The neutron-absorbing plates are opposed to each other with trap spaces disposed therebetween.

    摘要翻译: 用于核反应堆的控制棒包括四个翼,包括含有铪的中子吸收体,前端结构构件的横截面为十字形,并且包括结合到翼的前端的托架,以及具有十字形的末端结构构件 并且包括结合到翼的尾端的支架。 四个翼结合到包括十字形中心轴的翼接合构件以形成十字形状。 前端结构构件和翼缘接合构件由锆合金制成。 机翼包括具有中子吸收部分的中子吸收板,并且每个都具有与燃料组件相对的外表面,并且设置有用锆石覆盖的铪 - 氧化锆复合材料构件。 中子吸收板彼此相对,在它们之间设置有捕获空间。

    Control rod for nuclear reactor and method of manufacturing control rod
    3.
    发明授权
    Control rod for nuclear reactor and method of manufacturing control rod 有权
    核反应堆控制棒及制造控制棒的方法

    公开(公告)号:US08699652B2

    公开(公告)日:2014-04-15

    申请号:US12034966

    申请日:2008-02-21

    IPC分类号: G21C7/06

    摘要: A control rod for nuclear reactors includes four wings including neutron absorbers containing hafnium, a front end structural member which has a cross shape in cross section and includes brackets bonded to the leading ends of the wings, and a terminal end structural member which has a cross shape in cross section and includes brackets bonded to the tailing ends of the wings. The four wings are bonded to a wing-bonding member including a cross-shaped center shaft so as to form a cross shape. The front end structural member and the wing-bonding member are made of a zirconium alloy. The wings include neutron-absorbing plates having neutron-absorbing portions and each have an outer surface which is opposed to a fuel assembly and at which a hafnium-zircaloy composite member covered with zircaloy is disposed. The neutron-absorbing plates are opposed to each other with trap spaces disposed therebetween.

    摘要翻译: 用于核反应堆的控制棒包括四个翼,包括含有铪的中子吸收体,前端结构构件的截面十字形,并且包括结合到翼的前端的支架,以及具有十字形的末端结构构件 并且包括结合到翼的尾端的支架。 四个翼结合到包括十字形中心轴的翼接合构件以形成十字形状。 前端结构构件和翼缘接合构件由锆合金制成。 机翼包括具有中子吸收部分的中子吸收板,并且每个都具有与燃料组件相对的外表面,并且设置有用锆石覆盖的铪 - 氧化锆复合材料构件。 中子吸收板彼此相对,在它们之间设置有捕获空间。

    Jet pump beam and method for producing the same
    4.
    发明授权
    Jet pump beam and method for producing the same 有权
    喷射泵梁及其制造方法

    公开(公告)号:US08879683B2

    公开(公告)日:2014-11-04

    申请号:US13139835

    申请日:2009-12-01

    摘要: A jet pump beam is made of improved heat-treated precipitation-hardened nickel base alloy excellent in anti-stress corrosion cracking properties and high-temperature strength, and having high ductility and a high elastic modulus. A jet pump beam 27 made of improved heat-treated nickel base alloy is produced by preparing a precipitation-strengthened nickel base alloy material having a component composition containing by mass %, Ni: 50.0% to 55.0%, Cr: 17.0% to 21.0%, Nb+Ta: 4.75% to 5.50%, Mo: 2.8% to 3.3%, Ti: 0.65% to 1.15%, Al: 0.2% to 0.8%, C: 0.08% or less, Mn: 0.35% or less, Si: 0.35% or less, S: 0.015% or less, P: 0.03% or less, Cu: 0.30% or less, B: 0.006% or less, and Co: 1.0% or less, and Fe and inevitable impurities constituting a remaining part, subjecting the nickel base alloy material to solution heat treatment at a temperature of 1010° C. to 1090° C., and subjecting the nickel base alloy material to age-hardening heat treatment at a temperature of 694° C. to 714° C. for 5 to 7 hours after the solution heat treatment.

    摘要翻译: 喷射泵梁由改进的经热处理的沉淀硬化镍基合金制成,具有优异的抗应力腐蚀开裂性能和高温强度,并且具有高延展性和高弹性模量。 通过制备具有以质量%计含量的组分组成的沉淀强化镍基合金材料制备由改进的热处理镍基合金制成的喷射泵梁27,Ni:50.0%至55.0%,Cr:17.0%至21.0% ,Nb + Ta:4.75〜5.50%,Mo:2.8〜3.3%,Ti:0.65%〜1.15%,Al:0.2〜0.8%,C:0.08%以下,Mn:0.35% :0.35%以下,S:0.015%以下,P:0.03%以下,Cu:0.30%以下,B:0.006%以下,Co:1.0%以下,Fe和不可避免的杂质构成残留 将镍基合金材料在1010℃至1090℃的温度下进行固溶热处理,并将镍基合金材料在694℃至714℃的温度下进行老化硬化热处理 C.溶解热处理后5〜7小时。

    JET PUMP BEAM AND METHOD FOR PRODUCING THE SAME
    6.
    发明申请
    JET PUMP BEAM AND METHOD FOR PRODUCING THE SAME 有权
    喷射泵梁及其制造方法

    公开(公告)号:US20110255649A1

    公开(公告)日:2011-10-20

    申请号:US13139835

    申请日:2009-12-01

    IPC分类号: G21C15/25 C22F1/10

    摘要: A jet pump beam is made of improved heat-treated precipitation-hardened nickel base alloy excellent in anti-stress corrosion cracking properties and high-temperature strength, and having high ductility and a high elastic modulus. A jet pump beam 27 made of improved heat-treated nickel base alloy is produced by preparing a precipitation-strengthened nickel base alloy material having a component composition containing by mass %, Ni: 50.0% to 55.0%, Cr: 17.0% to 21.0%, Nb+Ta: 4.75% to 5.50%, Mo: 2.8% to 3.3%, Ti: 0.65% to 1.15%, Al: 0.2% to 0.8%, C: 0.08% or less, Mn: 0.35% or less, Si: 0.35% or less, S: 0.015% or less, P: 0.03% or less, Cu: 0.30% or less, B: 0.006% or less, and Co: 1.0% or less, and Fe and inevitable impurities constituting a remaining part, subjecting the nickel base alloy material to solution heat treatment at a temperature of 1010° C. to 1090° C., and subjecting the nickel base alloy material to age-hardening heat treatment at a temperature of 694° C. to 714° C. for 5 to 7 hours after the solution heat treatment.

    摘要翻译: 喷射泵梁由改进的经热处理的沉淀硬化镍基合金制成,具有优异的抗应力腐蚀开裂性能和高温强度,并且具有高延展性和高弹性模量。 通过制备具有以质量%计含量的组分组成的沉淀强化镍基合金材料制备由改进的热处理镍基合金制成的喷射泵梁27,Ni:50.0%至55.0%,Cr:17.0%至21.0% ,Nb + Ta:4.75〜5.50%,Mo:2.8〜3.3%,Ti:0.65%〜1.15%,Al:0.2〜0.8%,C:0.08%以下,Mn:0.35% :0.35%以下,S:0.015%以下,P:0.03%以下,Cu:0.30%以下,B:0.006%以下,Co:1.0%以下,Fe和不可避免的杂质构成残留 将镍基合金材料在1010℃至1090℃的温度下进行固溶热处理,并将镍基合金材料在694℃至714℃的温度下进行老化硬化热处理 C.溶解热处理后5〜7小时。