• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A fuel channel according to example embodiments for a nuclear reactor may have an elongated and hollow body with a multi-layer structure. The multi-layer structure may include a core layer and at least one cladding layer metallurgically-bonded to the core layer. The core layer and the at least one cladding layer may be alloys having different compositions. For instance, the core layer may be significantly more resistant to irradiation growth and/or irradiation creep than the at least one cladding layer, and the at least one cladding layer may have an increased resistance to hydrogen absorption and/or corrosion relative to the core layer. Accordingly, the distortion of the fuel channel may be reduced or prevented, thus reducing or preventing the interference with the movement of the control blade.
    公开号:SE534730C2
    申请号:SE0950337
    申请日:2009-05-13
    公开日:2011-12-06
    发明作者:Paul Everett Cantonwine；David William White
    申请人:Global Nuclear Fuel Americas；
    IPC主号:
    专利说明:

    40,534,730 different functions. For example, the core layer may be significantly more resistant to radiation growth and / or radiation creep than the at least single plating layer, and the at least single plating layer may have an increased resistance to hydrogen absorption and / or corrosion relative to the core layer.
    A fuel channel according to exemplary embodiments of a nuclear reactor may have a longitudinal and hollow body with a superficial structure. The layered structure may include a core layer and at least one plating layer metallurgically bonded to the core layer. The core layer and the at least one plating layer may be alloys of different composition that provide different functions.
    For example, the core layer may be significantly more resistant to radiation growth and / or radiation creep than the at least single plating layer, and the at least one plating layer may have an increased strength against hydrogen absorption and / or corrosion relative to the core layer.
    A method according to exemplary desiccation modes for manufacturing the fuel channels for a nuclear reactor may include joining nuclear material with plating material. The core material and the plating material may be alloys of different composition that provide different functions. For example, the core material may be significantly more resistant to radiation growth and / or creep than the plating material, and the plating material may have an increased strength against hydrogen absorption and / or corrosion relative to the core material. The joined core and cladding material can be rolled, and the rolled core and cladding material can be formed to form the fuel channel.
    Brief Description of the Drawings Features and advantages of exemplary embodiments may become more apparent upon review of the detailed description taken in conjunction with the accompanying drawings. The accompanying drawings are intended to illustrate exemplary embodiments and are not to be construed as limiting the intended scope of the claims. The accompanying drawings are not to be construed as being drawn to scale unless otherwise noted. For the sake of clarity, varying dimensions in the drawings may have been exaggerated.
    FIG. 1 is a cross-sectional view of a layered material according to exemplary embodiments of the present invention.
    FIG. 2 is a cross-sectional view of a reinforced multilayer material according to exemplary embodiments of the present invention.
    FIG. 3 is a perspective view of a fuel duct according to exemplary embodiments of the present invention.
    FIG. 4 is a perspective view of another fuel channel according to exemplary embodiments of the present invention.
    FIG. 5 is a perspective view of the contours of a fuel duct according to exemplary embodiments of the present invention. 40 534 730 FIG. 6 is a perspective view of another contour of a fuel duct according to exemplary embodiments of the present invention.
    FIG. 7 is a sectional view of a method of manufacturing a duct strip for a fuel duct according to exemplary embodiments of the present invention.
    FIG. 8 is a flow chart of another method of manufacturing a duct strip for a fuel duct according to exemplary embodiments of the present invention.
    FIG. 9 is a flow chart of another method of making a duct strip for a fuel duct according to exemplary embodiments of the present invention.
    Detailed Description of the Invention It is to be understood that when an element or layer is referred to as being "on", "connected to", "connected to", or "covering" another element or layer, it may be directly on, connected to, connected to to, or covering the other element or layer, or intervening elements or layers may be present.
    However, when an element is referred to as being "directly on", "directly connected to", or "directly connected to" another element or layer, there are no intervening elements or layers present.
    The same number refers to the same element throughout the description. As used herein, the term "and / or" may include any and all combinations of one or more of the associated listed objects.
    It is to be understood that, although the terms first, second, third, and so on. may be used herein to describe various elements, components, areas, layers and / or sections, these elements, components, areas, layers, and / or sections shall not be limited to these terms. These terms are used only ß: to distinguish an element, component, area, layer, or section from another area, layer, or section. Thus, a first element, component, area, layer, or section discussed below may be termed a second element, component, area, layer, or section without departing from the exemplary embodiments.
    Spatial relative terns (eg "below", "below", "lower", "above", "upper", and the like) can be used to facilitate the description of describing an element or feature relation to another / other elements or features as shown in the figures. It is to be understood that the spatial relative terms are intended to encompass different orientations of the device in use or in operation in addition to the orientation shown in the figures. For example, if the device in the figures is turned over, elements described as "below" or "below" other elements or features will then be oriented "above" the other elements or gurus. Thus, the tin "below" can enclose both an orientation above and below. The device may be differently oriented (rotated 90 degrees or other orientation) and the spatial relative descriptors used herein are interpreted therein.
    The terminology used herein is for the sole purpose of describing various embodiments and is not intended to be limited to the exemplary embodiments. As used herein, the singular form "a", "an", and "it / it" is intended to include plural forms as well, unless the content clearly indicates otherwise. It will further be appreciated that the terms "include" and / or "including" 534,730 when used in this specification specify the presence of specified features, integers, steps, maneuvers, elements, and / or components, but not exclusively the presence or addition of a or fl your features, integers, steps, maneuvers, elements, components, and / or groups thereof.
    Exemplary embodiments are described herein with reference to cross-sectional illustrations which are schematic illustrations of idealized embodiments (and intermediate structures) of exemplified embodiments. As such, variations from the form of the illustrations as a result, for example, of manufacturing techniques and / or tolerances, are expected. Thus, exemplary embodiments are not to be construed as limited in the form of areas illustrated herein but are inclusive of deviations in form as a result, for example, from manufacture. For example, an implanted area illustrating a rectangle will typically have rounded or curved features and / or a gradient of implant concentration at its edges rather than a binary change from implanted to non-implanted area. Likewise, a buried area and the surface through which the implantation takes place. Thus, the areas illustrated in the figure are schematic in nature and their shape is not intended to illustrate the actual shape of an area or device and is not intended to limit the scope of exemplary embodiments.
    Unless otherwise defined, all terms (including technical and scientific terms) have the same meaning as commonly understood by one of ordinary skill in the art to which the exemplary embodiments belong. It will further be understood that the terms, including those defined in commonly used encyclopedias, shall be construed as having a meaning which is in line with their meaning in the context of relevant technology and will not be construed as an idealized or overly formal sentence unless expressly so defined here in.
    A reactor component according to exemplary embodiments of a boiling water reactor (BWR) can be formed from a composite material with a multilayer structure. With reference to FIG. 1, the layered structure of a composite material 100 may include a plating layer 102 disposed on a core layer 104. The core layer 104 may be formed of a first alloy, and the plating layer 102 may be formed of a second alloy. The first and second alloys may have different compositions.
    In addition, the plating layer 102 may be metallurgically bonded to the core 104. Furthermore, the core layer 104 and the plating layer 102 may have different physical properties (eg, resistance to radiation growth, hydrogen absorption, corrosion, and / or radiation creep).
    Thus, the core layer 104 and the plating layer 102 may be combined in a manner to obtain a composite material which advantageously utilizes the advantageous properties of both the core layer 104 and the plating layer 102. For example, the core layer 104 may have a greater strength against radiation growth and / or radiation creep relative to the plating layer 102. and the plating layer 102 may have a greater strength against corrosion and / or hydrogen absorption relative to the core layer 104. It may be advantageous for the vessel layer 104 to be significantly more resistant to radiation growth and / or radiation creep than the plating layer 102. The core layer 104 may be considered significantly more durable is approximately fifty percent more resistant to radiation growth and / or radiation creep than the plating layer l02. Conversely, it may be advantageous for the plating layer 102 to be at least 50 percent more resistant to corrosion and / or hydrogen absorption than the core layer 104. As a result, the core layer 104 may be less prone to fluent gradient arc and / or creep expansion, while the plating layer 102 may be less prone to shadow corrosion-induced arc.
    The first alloy may be a zirconium (Zr) alloy containing niobium (Nb). For example, the first alloy may be an MSF alloy. The NSF alloy may have a composition (in weight percent) of about 0.6 - 1.4% niobium (Nb), about 0.2-05% iron, and about 0.5-1 .0% tin (Sn), with the balance being essential zirconium ( Zr). For example, the NSF alloy may have a composition (in weight percent) of about 1.0% niobium, about 035% iron, and about 1.0% tin, with the balance being essential zirconium.
    The second alloy may be zirconium (Zr) alloy containing tin (Sn), iron (Fe), and lo-om (Cr). The second alloy may have a composition (in weight percent) of about 0.4-2.0% tin (Sn), about 0.1-0.6% iron (Fe), and about 0.01-1.2% chromium (Cr), with the balance being essentially zirconium (Zr).
    The second alloy may be a Zircaloy-4 alloy. The zircaloy-4 alloy may have a composition (in weight percent) of about 1.2-1 .7% tin (Sn), about 0.12-0.21% iron (Fe), and about 0.05-0.5% chromium (Cr). , with the balance being essential zirconium (Zr). For example, the Zircaloy-4 alloy may have a composition (in weight percent) of about 1.45% tin, about 0.2% iron, and about 0.1% chromium, with the balance being essential zirconium.
    The other alloy can also be a VB alloy. The VB alloy may have a composition (in weight percent) of about 0.4-0.6% tin (Sn), about 0.4-0.6% Fe, and about 0.8-1 .2% chromium (Cr), with the balance being essential zirconium (Zr ). For example, the VB alloy may have a composition (in weight percent) of about 0.5% term, about 0.5% iron, and about 1.0% chromium, with the balance being essential zirconium.
    Referring to FIG. 2, the bearing structure of another composite material 200 may include a core layer 104 disposed between two plating layers 102. The core layer 104 may be formed of a first alloy, and the plating layers 102 may be formed of a second alloy. The first and second alloys may have different compositions. In addition, the plating layers 102 may be metallurgically bonded to the core layer 104. Furthermore, the core layer 104 and the plating layer 102 may have different physical properties (eg, resistance to radiation growth, hydrogen absorption, and / or radiation creep).
    Thus, the core layer 104 and the plating layers 102 may be combined in such a manner to obtain a composite material which has advantageously utilized the advantageous properties of both the core layer 104 and the plating layers 102. For example, the core layer 104 may have a greater strength against radiation growth and / or radiation creep 102 relative to the plating layer 102. , and the plating layers 102 may have a higher strength against corrosion and hydrogen absorption relative to the core layer 104. It may be advantageous for the core layer 104 to be significantly more resistant to radiation growth and / or radiation creep than the plating layers 102. The core layer 104 may be considered significantly more strong if it is approximately fifty percent more resistant to radiation growth and / or radiation creep than the plating layer 102. Conversely, it may be advantageous for the plating layers 102 to be at least fifty percent more resistant to corrosion and / or hydrogen absorption than the core layer 104. As a result, ultat 534 730, the core layer 104 may be less prone to uneven gradient arc and / or creep expansion, while the plating layers 102 may be less prone to shadow corrosion-induced arc.
    The first alloy may be a zirconium (Zr) alloy containing niobium (Nb). For example, the first alloy may be an NSF alloy. The NSF alloy may have a composition (in weight percent) of about 0.6-1 .4% niobium (Nb), about 0.2-0.5% iron, and about 0.5-l .0% tin (Sn), with the balance being essentially Zirconium. For example, the NSF alloy may have a composition (in weight percent) of about 1.0% niobium, about 035% iron, and about 1.0% tin, with the balance being essential zirconium.
    The second alloy may be a zirconium (Zr) alloy containing tin (Sn), iron (Fe), and chromium (Cr). The second alloy may have a composition (in weight percent) of about 0.4-2.0% tin (Sn), about 0.1 -0.6% iron (F e), and about 0.01-1 .2% chromium (Cr), with the balance being essentially Zirconium.
    The second alloy may be a Zirkaloy-4 alloy. The Zirkaloy-4 alloy may have a composition (in weight percent) of about 1.2-1 .7% tin (Sn), about 0.12-0.2l% iron (Fe), and about 0.05-0.1 5% chromium (Cr). with the balance being essential zirconium (Zr). For example, the Zirkaloy-4 alloy may have a composition (in weight percent) of about 1.45% term (sn), about 0.2l% iron, and about 0. 1% chromium, with the balance being essential zirconium.
    The other alloy can also be a VB alloy. The VB alloy may have a composition (in weight percent) of about 0.4-0.6% tin (Sn), about 0.4-0.6% Fe, and about 0.8-I .2% chromium (Cr), with the balance being essential zirconium.
    Thus, one or more of the surfaces of the first alloy may be plated with a second alloy. For example, the first alloy may be plated on one side of one or andra your other alloy layers.
    Alternatively, the second alloy may be alternated between two or more other alloy layers. Where several other alloy layers are used, the other alloy may have an identical or different composition. The first and second alloys may be zirconium (Zr) alloy. The use of zirconium in nuclear reactor components can be beneficial because zirconium has a relatively small cross-section for neutron absorption and poor corrosion resistance in a water environment with a relatively high pressure / temperature.
    The thickness of the first alloy layer can determine a majority of the thickness of the composite material. For example, the thickness of the first alloy layer may be about 50-100 mils (about 0.050-0.00 inches). On the other hand, the second alloy may be relatively thin. For example, the thickness of the second alloy layer may be about 3-4 miles (about 0.003-0.004 inches).
    However, it should be noted that other dimensions are possible depending on the application. The first and second alloy layers may be metallurgically bonded.
    A reactor component according to exemplary embodiments may include a fuel channel for a boiling water reactor. The fuel duct according to exemplary exhaust modes can reduce or prevent duct disturbance caused by different radiation growth, different hydrogen absorption, and / or radiation creep. 40 534 730 The fuel channel can be manufactured with a first alloy which is relatively strong against different radiation growth and / or radiation penetration. As a result, the first alloy may reduce or prevent the formation of a non-gradient arc and / or creep expansion. The first alloy can be plated with a second alloy which is relatively resistant to hydrogen absorption and / or corrosion. As a result, the second alloy may reduce or prevent the appearance of shadow corrosion-induced arc.
    Referring to FIG. 3 shows a fuel channel 300 can be formed of the material 100 iFIG. Thus, the fuel channel 300 may include a plating layer 102 on the outer surface of the core layer 104. Alternatively, the outer surface of the core layer 104 may be plated with a plurality of plating layers (not shown).
    Referring to FIG. 4, a fuel channel 400 may be formed of the material 200 in FIG. Thus, the fuel channel 400 may include both a plating layer 102 on the inner surface of the core layer 104 and a plating layer 102 on the outer surface of the core layer 104. Alternatively, the inner and / or outer surfaces of the core layer 104 may be plated with a plating layer (not shown).
    Referring to FIG. 5 shows a contour (thick / thin) of a fuel channel 500 which can be formed of the material 100 according to FIG. Thus, the fire play channel 500 may include a plating layer 102 on the outer surface of the core layer 104. Alternatively, the outer surface of the core layer 104 may be plated with a plurality of plating layers (not shown).
    Referring to FIG. 6 shows a contour (thick / thin) of a fuel channel 600 which may be formed of the material 200 in FIG. Thus, the fuel channel 600 may include both a plating layer 102 on the inner surface of the core layer 104 and a plating layer 102 on the outer surface of the core layer 104. Alternatively, the inner and / or outer surfaces of the core layer 104 may be plated with a plurality of plating layers (not shown).
    Next, exemplary embodiments of a method of manufacturing a fuel duct will be described. Fig. 7 is a view of a method for manufacturing a duct strip for a fuel duct according to exemplary embodiments. As shown in step S70, a core material of a first alloy is joined to a plating material formed of a second alloy. For example, a plate formed of a first alloy and a cladding formed of a second alloy may be provided, the first and second alloys having different compositions. The plate may be an alloy which is relatively strong against radiation growth and / or radiation absorption, since the cladding may be an alloy which is relatively strong against corrosion and / or hydrogen absorption. For example, the alloys can be described as above with reference to FIG. 1-2. The plate can be inserted into the cladding, and a vacuum can be drawn to seal the plate in the cladding. Alternatively, it may be noted that the second alloy may also be in the form of a plate which is joined to the plate formed by the first alloy. For example, the first alloy plate may be electron beam welded to the second alloy plate under vacuum.
    The joined alloy materials may be subjected to a first hot rolling process to obtain a first thickness (eg about 1 inch) in step 72. The first hot rolling process may be any well known hot rolling process. Referring to step S74, the hot rolled alloy materials can be beta hardened to increase the corrosion resistance. The beta curing can be obtained by any well known beta curing process. For example, the hot rolled alloy materials may be beta hardened at a temperature higher than about 900 degrees Celsius due to a beta hardening.
    Referring to step S76, the cured alloy materials may also be subjected to a second hot rolling process to obtain a second thickness (eg less than 1 inch). The second hot rolling process can be any well known hot rolling process. The second hot rolling process can be followed by any well known annealing process (eg recrystallization annealing). Referring to step S78, the hot rolled material may additionally be subjected to any well known cold rolling process to obtain a third thickness (eg about 0.050-0.110 inches). The cold rolling process can be followed by any well known annealing process. It may be advantageous for the process following beta curing to be performed at a temperature below about 900 degrees Celsius (eg about 500-800 degrees Celsius).
    The final layer of material can have a relatively homogeneous thickness. The final bearing material can be deformed and welded to form a fuel channel. For example, two layers of the final material can be bent along a longitudinal direction to an approximately 90 degree angle.
    The curved plates can then be welded together to form a longitudinal fuel channel with a square shaped cross section.
    FIG. 8 is a flow chart of another method of manufacturing a duct strip for a fuel duct according to exemplary embodiments. As shown in step S80, a core material formed of a first alloy is joined to a plating material formed of a second alloy. For example, a plate formed of a first alloy and a roll cladding formed of a second alloy may be provided, the first and second alloys may have different compositions. The plate may be an alloy which is relatively strong against radiation growth and / or radiation creep, since the cladding may be an alloy which is relatively resistant to corrosion and hydrogen absorption. For example, the alloys may be as described above with respect to FIG. 1-2. The plate can be in the liner, and a vacuum can be drawn to seal the plate in the liner. Alternatively, it may be noted that the second alloy may also be in the form of a plate which is joined to the plate formed by the first alloy. For example, the first alloy may be electron beam welded to the second alloy plate under vacuum.
    The joined alloy materials may be subjected to a first hot rolling process to obtain a first thickness (eg about 1 inch) in step S82. The first hot rolling process can be any well known hot rolling process. Referring to step S84, the hot rolled materials can be beta hardened to increase the corrosion resistance. Beta curing can be obtained by any well known beta curing process. For example, the hot rolled materials can be beta heat treated at a temperature higher than 900 degrees Celsius followed by a beta cure.
    Referring to step S86, the cured alloy materials may also be subjected to a second hot rolling process to obtain a second thickness (eg, less than 1 inch). The second hot rolling process can be any well known hot rolling process. The second hot rolling process can be followed by any well known recrystallization (RX) annealing process. Referring to step S88, the hot rolled materials may additionally be subjected to any well known cold rolling process to obtain a third thickness (eg about 0.060-0.120 inches). The cold rolling process can be followed by any well known process of recrystallization annealing. It may be advantageous for the post-cure process to be carried out at a temperature below about 900 degrees Celsius (eg about 500-800 degrees Celsius).
    Referring to step S89, the cold rolled materials can be pressed to obtain a thick / thin dimension.
    The pressed alloy material can be the subject of any well-known restoration (eg stress relief) annealing process. Alternatively, thick and thin pieces can be manufactured separately (eg rolling the alloyed material to form a thick part and a thin part) and welded together to obtain a welded material with a thick / thin dimension. A thick / thin dimension can be advantageous in order to reduce or minimize the amount of material constituting a reactor component, since residual material can contribute to the absorption of neutrons. Pressing the cold-rolled liner and plate to obtain a thick / thin dimension can provide a better result compared to machining to obtain a thick / thin dimension, which can remove the plating formed by the second alloy.
    The final multilayer material can be deformed and welded to form a fuel channel. For example, two sheets of the final material can be bent in the longitudinal direction to an angle of approximately 90 degrees. The curved discs can then be welded together to form a longitudinal fire play channel with a square cross-section. Due to the thick / thin dimension of the material, the central part of the side walls of the channel can be relatively thin, while the parts of the side wall that are at the corner can be relatively thick.
    FIG. 9 is a flow chart of an amian method of making a duct strip for a fuel duct according to exemplary embodiments. As shown in step S90, a core material of a first alloy is joined to a cladding rig material formed of a second alloy. For example, a plate formed of the first alloy and a cladding formed of the second alloy may be provided, the first and second alloys may have different compositions. The plate may be an alloy which is relatively strong against radiation growth and / or radiation absorption, since the cladding may be an alloy which is relatively strong against hydrogen absorption and / or corrosion. For example, the alloys as described above with reference to FIG. 1-2. The plate can be inserted into the cladding row, and a ballot box can be drawn to close the plate in the cladding. Alternatively, it may be noted that the second alloy may also be in the form of a plate which is joined to the plate formed by the first alloy. For example, the first alloy plate may be electron beam welded to a second alloy plate under vacuum.
    The joined materials may be subjected to a first hot rolling process to obtain a first thickness (eg about 1 inch) in stone S92. The first hot rolling process can be any well known hot rolling process. Referring to step 94, the hot rolled alloy materials may be beta hardened to increase corrosion resistance and radiation growth. The beta cure can be obtained by any well known beta cure process. For example, the hot-rolled alloy materials beta heat can be treated at a temperature higher than about 900 degrees Celsius followed by a beta hardening. 534 730 Referring to step S96, the cured alloy materials may also be subjected to a second hot rolling process to obtain a second thickness (eg less than one inch). The second hot rolling process can be any well known hot rolling process. The second hot rolling process can be followed by any well known recrystallization (RX) annealing process. Referring to step S98, the hot rolled materials may be subjected to a cold rolling process to obtain a third thickness having a thick / thin dimension. For example, the cold rolling process can be performed with a grooved roller to apply the thick / thin dimension into the material. The cold rolling process can be followed by any well known recrystallization process.
    Alternatively, thick and thin parts can be manufactured separately (eg, roll the alloy material to obtain a thick and a thin part) and welded together to obtain a welded material with a thick / thin dimension. It may be advantageous for the post-cure process to be carried out at a temperature below about 900 degrees Celsius (eg about 500-800 degrees Celsius).
    The final multilayer material can be deformed and welded to form a fuel channel. For example, two plates of the final material can be bent along the longitudinal direction to an approximately 90 degree angle. The curved plates can then be welded together to form a longitudinal fuel channel with a square cross-section. Due to the thick / thin dimensions of the material, the central part of the side walls of the channel can be relatively tumi, while the parts of the side walls that are at the corners can be relatively thick.
    Since exemplary embodiments have been shown herein, it is to be understood that other variations are possible. Such variations are not to be construed as a departure from the core of exemplary embodiments of the present invention, and all such modifications as would be apparent to those skilled in the art are intended to be included within the scope of the following claims.
    权利要求:
    Claims (6)
    [1]
    1. A multilayer material (200) for a reactor component, comprising: a core layer (10 4); and at least one plating layer (102) metallurgically bonded to the core layer (104), the core layer (104) and the at least one plating layer (102) having different compositions, the core layer (104) being significantly more resistant to radiation growth than the at least one plating layer (102). ) and the at least one plating layer (102) has an increased strength against hydrogen absorption relative to the core layer (104), the core layer (104) being formed of a first zirconium alloy containing niobium and the at least one plating layer (102) being formed of a second zirconium alloy containing tin , iron, and about 0.8% - 1.2% Within.
    [2]
    The material of claim 1, wherein the at least one plating layer (102) includes two plating layers (102), the core layer (104) being interspersed between the two plating layers (102).
    [3]
    A fuel channel (400) for a nuclear reactor, comprising: a longitudinal and hollow body having a multilayer structure, including the fl-bearing structure, a core layer (104); and at least one plating layer (102) metallurgically bonded to the core layer (104), the core layer (104) and the at least one plating layer (102) having different compositions, the core layer (104) being significantly more resistant to radiation growth than the at least one plating layer (102). ), and the at least one plating layer (102) has an increased strength against hydrogen absorption relative to the core layer (104), the core layer (104) being formed of a first zirconium alloy containing niobium and the at least one plating layer (102) being formed of a second zirconium alloy. tin, iron, and about 0.8% - 1.2% chromium.
    [4]
    A method of manufacturing a fuel channel for a nuclear reactor, comprising: joining a core material with a plating material (S70), the core material and the plating material having different compositions, the core material being formed of a first zirconium alloy containing niobium and a zinc alloy material. term, iron, and about 0.8% - 1.2% chromium, the core material is significantly more resistant to radiation growth than the plating material, and the plating material has an increased resistance to hydrogen absorption relative to the core material; rolling the joined core and cladding materials; and deforming the rolled core and plating materials to form a fuel channel.
    [5]
    The method of claim 4, wherein the rolling of the joined core and plating material comprises. performing a first hot rolling process on the comb and plating materials (S72); performing a beta curing process (S74); performing a second hot rolling process followed by annealing (S76); perform a cold rolling process followed by annealing (S78).
    [6]
    The method of claim 5, further comprising: pressing the cold-rolled core and plating materials to obtain a pressed material with a 534 'P30 II. first part with a first dimension and a second part with a second dimension, the first dimension is relatively thick compared to the second dimension, and the second dimension is relatively thin compared to the first dimension; and performing a restorative annealing process to release internal stress in the pressed material (S89).
    类似技术:
    公开号 | 公开日 | 专利标题
    You2015|Copper matrix composites as heat sink materials for water-cooled divertor target
    Bouiadjra et al.2008|Disbond effects on bonded boron/epoxy composite repair to aluminium plates
    Smith et al.2014|Measured and predicted residual stresses in thick section electron beam welded steels
    Tafreshi2006|Delamination buckling and postbuckling in composite cylindrical shells under combined axial compression and external pressure
    SE534730C2|2011-12-06|Multilayer fuel channel and method for manufacturing the same
    Sedighi et al.2012|Investigation of cold rolling influence on near surface residual stress distribution in explosive welded multilayer
    Comley2004|Lowering the heat-the development of reduced SPF temperature titanium alloys for aircraft production
    Salehi et al.2019|Residual stress measurement using the slitting method via a combination of eigenstrain, regularization and series truncation techniques
    Jiang et al.2021|Comparative study on the tensile cracking behavior of CrN and Cr coatings for accident-tolerant fuel claddings
    Bompa et al.2017|Numerical modelling and parametric assessment of hybrid flat slabs with steel shear heads
    CN110252807A|2019-09-20|Cladded sheet materials for heat exchanger
    Li et al.2018|Interfacial fracture behavior of double-ceramic-layer thermal barrier coating system with segmented structure
    SE510099C2|1999-04-19|Method of providing a fuel canister with an alloy zirconium barrier layer
    Yin et al.2012|Impact of residual stress on the adhesion and tensile fracture of TiN/CrN multi-layered coatings from first principles
    Kamaya2015|Elastic-plastic failure assessment of cold worked stainless steel pipes
    He et al.2013|Uncovering the critical factor in determining the residual stresses level in Si3N4–GM filler alloy–42CrMo joints by FEM analysis and experiments
    Su et al.2014|Microstructure and mechanical properties of AA5005/AA6061 laminated composite processed by accumulative roll bonding
    JP5207075B2|2013-06-12|Material property identification method of elasto-plastic material by indentation test
    Khalili et al.2020|Flexural properties of sandwich composite panels with glass laminate aluminum reinforced epoxy facesheets strengthened by SMA wires
    Khaledi et al.2019|A multiscale description of bond formation in cold roll bonding considering periodic cracking of thin surface films
    US2017757A|1935-10-15|Duplex metal article
    Ainsworth et al.2013|The treatment of secondary strains within a strain-based failure assessment diagram
    Nechaykina et al.2017|Structure and Properties of High-Temperature Multilayer Hybrid Material Based on Vanadium Alloy and Stainless Steel
    Sørensen et al.2012|Strength and failure modes of ceramic multilayers
    Zhang et al.2011|Delamination of layered structures on elastic foundation
    同族专利:
    公开号 | 公开日
    DE102009025838A1|2009-11-26|
    SE0950337L|2009-11-20|
    US20090285350A1|2009-11-19|
    JP2009282026A|2009-12-03|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4751044A|1985-08-15|1988-06-14|Westinghouse Electric Corp.|Composite nuclear fuel cladding tubing and other core internal structures with improved corrosion resistance|
    JP2580273B2|1988-08-02|1997-02-12|株式会社日立製作所|Nuclear reactor fuel assembly, method of manufacturing the same, and members thereof|
    US5524032A|1993-07-14|1996-06-04|General Electric Company|Nuclear fuel cladding having an alloyed zirconium barrier layer|
    US5805656A|1996-04-08|1998-09-08|General Electric Company|Fuel channel and fabrication method therefor|US9284629B2|2004-03-23|2016-03-15|Westinghouse Electric Company Llc|Zirconium alloys with improved corrosion/creep resistance due to final heat treatments|
    US10221475B2|2004-03-23|2019-03-05|Westinghouse Electric Company Llc|Zirconium alloys with improved corrosion/creep resistance|
    US9287012B2|2010-07-25|2016-03-15|Global Nuclear Fuel—Americas, LLC|Optimized fuel assembly channels and methods of creating the same|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    US12/153,415|US20090285350A1|2008-05-19|2008-05-19|Multi-layer fuel channel and method of fabricating the same|
    [返回顶部]