CN115810434A - Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof - Google Patents
Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof Download PDFInfo
- Publication number
- CN115810434A CN115810434A CN202211723006.2A CN202211723006A CN115810434A CN 115810434 A CN115810434 A CN 115810434A CN 202211723006 A CN202211723006 A CN 202211723006A CN 115810434 A CN115810434 A CN 115810434A
- Authority
- CN
- China
- Prior art keywords
- tungsten mesh
- tungsten
- mesh
- aluminum
- shielding material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 title claims abstract description 103
- 229910052721 tungsten Inorganic materials 0.000 title claims abstract description 102
- 239000010937 tungsten Substances 0.000 title claims abstract description 102
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 54
- 239000002131 composite material Substances 0.000 title claims abstract description 48
- 239000000463 material Substances 0.000 title claims abstract description 43
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 34
- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 30
- 229910052796 boron Inorganic materials 0.000 claims abstract description 25
- 239000002245 particle Substances 0.000 claims abstract description 24
- 229910052688 Gadolinium Inorganic materials 0.000 claims abstract description 17
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims abstract description 17
- 238000000034 method Methods 0.000 claims abstract description 15
- 239000000725 suspension Substances 0.000 claims abstract description 13
- 239000011159 matrix material Substances 0.000 claims abstract description 12
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 9
- 239000010959 steel Substances 0.000 claims abstract description 9
- 239000006096 absorbing agent Substances 0.000 claims abstract description 8
- 238000001035 drying Methods 0.000 claims abstract description 7
- 239000000843 powder Substances 0.000 claims description 16
- 230000005251 gamma ray Effects 0.000 claims description 8
- 238000010521 absorption reaction Methods 0.000 claims description 5
- 229910052580 B4C Inorganic materials 0.000 claims description 4
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 4
- INAHAJYZKVIDIZ-UHFFFAOYSA-N boron carbide Chemical compound B12B3B4C32B41 INAHAJYZKVIDIZ-UHFFFAOYSA-N 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000012459 cleaning agent Substances 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 2
- 239000012535 impurity Substances 0.000 claims description 2
- 238000002844 melting Methods 0.000 claims 2
- 230000008018 melting Effects 0.000 claims 2
- 230000001680 brushing effect Effects 0.000 claims 1
- 238000004140 cleaning Methods 0.000 claims 1
- 238000005520 cutting process Methods 0.000 claims 1
- 229940075613 gadolinium oxide Drugs 0.000 claims 1
- 229910001938 gadolinium oxide Inorganic materials 0.000 claims 1
- CMIHHWBVHJVIGI-UHFFFAOYSA-N gadolinium(iii) oxide Chemical compound [O-2].[O-2].[O-2].[Gd+3].[Gd+3] CMIHHWBVHJVIGI-UHFFFAOYSA-N 0.000 claims 1
- 238000010030 laminating Methods 0.000 claims 1
- 238000003825 pressing Methods 0.000 claims 1
- 230000005855 radiation Effects 0.000 abstract description 4
- 238000009417 prefabrication Methods 0.000 abstract 2
- 239000007788 liquid Substances 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 description 4
- 230000010354 integration Effects 0.000 description 4
- 229910000712 Boron steel Inorganic materials 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 239000003513 alkali Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 229910002804 graphite Inorganic materials 0.000 description 3
- 239000010439 graphite Substances 0.000 description 3
- -1 polyethylene Polymers 0.000 description 3
- 239000004698 Polyethylene Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229920000573 polyethylene Polymers 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 238000009715 pressure infiltration Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000000498 ball milling Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- JEEHQNXCPARQJS-UHFFFAOYSA-N boranylidynetungsten Chemical compound [W]#B JEEHQNXCPARQJS-UHFFFAOYSA-N 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000011824 nuclear material Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000002490 spark plasma sintering Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
Images
Classifications
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/30—Nuclear fission reactors
Landscapes
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
本发明涉及核辐射防护复合材料技术领域,更具体的说是一种钨网增韧铝基复合核屏蔽材料及其制备方法,步骤一:选取处理钨网:步骤二:配置中子吸收剂悬浊液;步骤三:钨网剪成后层叠,中子吸收剂悬浊液刷在每一层钨网表面,干燥后形成钨网预制件;步骤四:钨网预制件压入到钢模中;步骤五:预热钨网预制件,熔化铝金属;步骤六:熔化铝金属浇铸在预热后的钨网预制件上;步骤七:加压使得熔化铝金属浸渗到预热的钨网预制体内;步骤八:保持压力并自然冷却,制成钨网增韧铝基复合核屏蔽材料;该复合材料以含硼和/或含钆颗粒为中子吸收组元,以钨网为伽马射线吸收组元,以铝金属为基体,具有综合屏蔽能力,同时兼顾良好力学性能。
The present invention relates to the technical field of nuclear radiation protection composite materials, more specifically a tungsten mesh toughened aluminum-based composite nuclear shielding material and a preparation method thereof. Step 1: select and process tungsten mesh; Turbid liquid; step 3: tungsten mesh is cut and stacked, neutron absorber suspension is brushed on the surface of each layer of tungsten mesh, and after drying, tungsten mesh prefabrication is formed; step 4: tungsten mesh prefabrication is pressed into the steel mold ;Step 5: Preheat the tungsten mesh preform and melt the aluminum metal; Step 6: Cast the molten aluminum metal on the preheated tungsten mesh preform; Step 7: Pressurize the molten aluminum metal to impregnate the preheated tungsten mesh Prefabricated body; Step 8: Maintain pressure and cool naturally to make a tungsten mesh toughened aluminum matrix composite nuclear shielding material; the composite material uses boron and/or gadolinium-containing particles as neutron absorbing components, and tungsten mesh as gamma The ray-absorbing component is based on aluminum metal, which has comprehensive shielding ability and good mechanical properties.
Description
技术领域technical field
本发明涉及核辐射防护复合材料技术领域,更具体地说是一种钨网增韧铝基复合核屏蔽材料及其制备方法。The invention relates to the technical field of nuclear radiation protection composite materials, in particular to a tungsten mesh toughened aluminum-based composite nuclear shielding material and a preparation method thereof.
背景技术Background technique
核屏蔽材料对核能的安全应用有着至关重要的作用。对于要求轻量化和小型化的核反应堆动力装置,核屏蔽材料需要具备更优良的力学性能和更低的比重。Nuclear shielding materials play a vital role in the safe application of nuclear energy. For nuclear reactor power plants that require lightweight and miniaturization, nuclear shielding materials need to have better mechanical properties and lower specific gravity.
为了满足核屏蔽材料结构功能一体化的需求,国内外开展了大量的研究,设计开发了屏蔽混凝土、硼钢、铅硼聚乙烯等一系列高效的金属基和聚合物基综合屏蔽复合材料。In order to meet the needs of structural and functional integration of nuclear shielding materials, a lot of research has been carried out at home and abroad, and a series of high-efficiency metal-based and polymer-based comprehensive shielding composite materials such as shielding concrete, boron steel, and lead-boron polyethylene have been designed and developed.
例如专利CN105014075制备了具有优异的屏蔽性能和力学性能的铅铝硼复合屏蔽材料,但其制备工艺比较复杂,且屏蔽混凝土易受环境腐蚀的严重,影响材料对屏蔽粒子的吸收效果。For example, patent CN105014075 has prepared a lead-aluminum-boron composite shielding material with excellent shielding performance and mechanical properties, but its preparation process is relatively complicated, and the shielding concrete is easily corroded by the environment, which affects the absorption effect of the material on shielding particles.
例如专利CN110774512A制备了高含钨量的钨硼聚乙烯屏蔽体,具有高的核辐射屏蔽效率,但这种材料中含有聚合物,其耐热性能较差,仅为80~100℃。而硼钢和高硼钢会反应生成共晶硼化物Fe2B,且易在晶界形核,弱化材料的力学性能,同时此类合金的屏蔽性能受固溶度影响也不出众。然而,高效稳定的核屏蔽材料不仅要具有高的γ射线和中子屏蔽性能,还要求具有良好的强韧性。采用铝基复合材料的形式,不仅具有添加屏蔽组元介观形态可控、含量可调范围大的特点,同时还能够保持较好的力学性能和耐热性能,以及较之传统屏蔽材料更低的比重,这在后期材料成型和工程使用上具有较大优势。For example, patent CN110774512A has prepared a tungsten-boron polyethylene shielding body with high tungsten content, which has high nuclear radiation shielding efficiency, but this material contains polymer, and its heat resistance is poor, only 80-100 ° C. However, boron steel and high boron steel will react to form eutectic boride Fe 2 B, which is easy to nucleate at the grain boundary and weaken the mechanical properties of the material. At the same time, the shielding performance of this type of alloy is not affected by the solid solubility. However, efficient and stable nuclear shielding materials should not only have high γ-ray and neutron shielding performance, but also require good toughness. The form of aluminum-based composite materials not only has the characteristics of controllable mesoscopic shape and large content adjustable range of added shielding components, but also can maintain good mechanical properties and heat resistance, and is lower than traditional shielding materials. The specific gravity, which has great advantages in later material molding and engineering use.
鉴于铅元素的毒性危害,本发明使用重核元素钨作为γ射线屏蔽组元,并以含硼颗粒和/或含钆颗粒来实现良好的中子吸收效果。然而,现有的含钨核屏蔽复合材料中钨元素主要以颗粒形式添加,随钨颗粒含量的增加,复合材料的塑性将显著下降。In view of the toxicity hazard of lead element, the present invention uses heavy nuclear element tungsten as gamma ray shielding component, and uses boron-containing particles and/or gadolinium-containing particles to achieve good neutron absorption effect. However, the tungsten element in the existing tungsten-containing nuclear shielding composite materials is mainly added in the form of particles, and the plasticity of the composite material will decrease significantly with the increase of the content of tungsten particles.
例如专利CN110527887B是将钨和/或碳化钨以及硼、碳化硼和氮化硼中的一种或两种与铝合金粉球磨后放电等离子烧结得到复合材料。For example, in patent CN110527887B, tungsten and/or tungsten carbide and one or both of boron, boron carbide and boron nitride are ball-milled with aluminum alloy powder and then spark plasma sintered to obtain a composite material.
为提高复合材料的屏蔽性能,必然需要提高钨和/或碳化钨含量,必然带来复合材料力学性能的显著下降,难以满足结构功能一体化需求,且存在球磨时间长,放电等离子烧结制备样品尺寸小的问题。In order to improve the shielding performance of the composite material, it is necessary to increase the content of tungsten and/or tungsten carbide, which will inevitably lead to a significant decline in the mechanical properties of the composite material, and it is difficult to meet the needs of structural and functional integration, and there is a long ball milling time, and the size of the sample prepared by spark plasma sintering small problem.
因此,本发明将颗粒状增强体改为网状编织的钨丝,采用压力浸渗法制备钨网增韧铝基复合材料,以期降低增强体对复合材料脆性的贡献,在保证材料屏蔽性能的同时提高材料的强韧性。Therefore, in the present invention, the granular reinforcement is changed to a mesh-like braided tungsten wire, and the tungsten mesh toughened aluminum-based composite material is prepared by a pressure infiltration method, in order to reduce the contribution of the reinforcement to the brittleness of the composite material, while ensuring the shielding performance of the material. At the same time, the strength and toughness of the material are improved.
综上所诉,研发一种具有对γ射线和中子具有综合屏蔽能力,同时兼顾良好力学性能的结构功能一体化核屏蔽材料势在必行、前景广阔。In summary, it is imperative and promising to develop a structure-functional integrated nuclear shielding material that has comprehensive shielding capabilities against γ-rays and neutrons, and has good mechanical properties.
发明内容Contents of the invention
本发明的目的是提供一种钨网增韧铝基复合核屏蔽材料及其制备方法,可以制备一种具有对γ射线和中子具有综合屏蔽能力,同时兼顾良好力学性能的结构功能一体化核屏蔽材料。The purpose of the present invention is to provide a tungsten mesh toughened aluminum-based composite nuclear shielding material and its preparation method, which can prepare a structure-functional integrated nuclear material with comprehensive shielding ability for gamma rays and neutrons and good mechanical properties. shielding material.
本发明的目的通过以下技术方案来实现:The purpose of the present invention is achieved through the following technical solutions:
一种钨网增韧铝基复合核屏蔽材料,该复合材料以含硼和/或含钆颗粒为中子吸收组元,以钨网为伽马射线吸收组元,以铝金属为基体;其中含硼和/或含钆颗粒体积分数为1%~20%,钨网体积分数为1%~50%,铝金属基体的体积分数为30%~98%;A tungsten mesh toughened aluminum-based composite nuclear shielding material, the composite material uses boron-containing and/or gadolinium-containing particles as neutron-absorbing components, tungsten mesh as gamma-ray-absorbing components, and aluminum metal as a matrix; wherein The volume fraction of boron and/or gadolinium-containing particles is 1% to 20%, the volume fraction of tungsten mesh is 1% to 50%, and the volume fraction of aluminum metal matrix is 30% to 98%;
所述铝金属基体为纯铝或者铝合金,所述含硼颗粒是纯硼粉和/或碳化硼粉,含硼粉的粒径为0.1~30μm,含钆颗粒是纯钆粉和/或氧化钆粉,含钆粉的粒径为0.1~50μm,钨网为10~500目,丝径为5μm~1mm;The aluminum metal matrix is pure aluminum or aluminum alloy, the boron-containing particles are pure boron powder and/or boron carbide powder, the particle size of the boron-containing powder is 0.1-30 μm, and the gadolinium-containing particles are pure gadolinium powder and/or boron carbide powder. Gadolinium powder, the particle size of the gadolinium-containing powder is 0.1-50 μm, the tungsten mesh is 10-500 mesh, and the wire diameter is 5 μm-1mm;
一种钨网增韧铝基复合核屏蔽材料制备方法,该方法包括以下步骤:A method for preparing a tungsten mesh toughened aluminum-based composite nuclear shielding material, the method comprising the following steps:
步骤一:选取处理钨网:按材料设计要求,选取目数为10目~500目,丝径为5μm~1mm的钨网,将钨网放入清洗剂中清洗,以去除表面的杂质和氧化层;清洗剂为为浓碱或浓酸溶液;Step 1: Select and process tungsten mesh: According to the material design requirements, select a tungsten mesh with a mesh number of 10 mesh to 500 mesh and a wire diameter of 5 μm to 1mm, and put the tungsten mesh in a cleaning agent to remove impurities and oxidation on the surface layer; the cleaning agent is concentrated alkali or concentrated acid solution;
步骤二:配置中子吸收剂悬浊液;中子吸收剂悬浊液为含硼粉和/或含钆粉与无水乙醇配置成的浓度为100%~700%的悬浊液;Step 2: preparing a neutron absorber suspension; the neutron absorber suspension is a suspension of boron-containing powder and/or gadolinium-containing powder and absolute ethanol with a concentration of 100% to 700%;
步骤三:将清洗过的钨网裁剪成一定形状、尺寸,按材料设计要求按照交错层叠与顺序层叠等铺层方式和0~90°的铺层角度进行层叠,每铺一层钨网,用毛刷将中子吸收剂悬浊液刷在钨网表面,称量以确定中子吸收剂添加量;将排布后的钨网用石墨垫片上下夹紧,并用螺栓固定;随后将其放入50℃~100℃的干燥箱中干燥5~20min;Step 3: Cut the cleaned tungsten mesh into a certain shape and size, and stack according to the material design requirements in accordance with the layering methods such as staggered layering and sequential layering and the layering angle of 0-90°. Each layer of tungsten mesh is laid with Brush the neutron absorber suspension on the surface of the tungsten mesh, weigh it to determine the amount of neutron absorber added; clamp the arranged tungsten mesh up and down with graphite gaskets, and fix it with bolts; then place it Dry in a drying oven at 50°C to 100°C for 5 to 20 minutes;
步骤四:钨网预制件用压力机压入压入到钢模中;Step 4: The tungsten mesh preform is pressed into the steel mold with a press;
步骤五:将钨网预制体连同钢模一同转移至加热炉中,将加热炉的温度从室温升温至500℃~700℃并保温10~120分钟,得到预热的钨网预制体;同时将铝金属在700℃~900℃加热至熔化;Step 5: Transfer the tungsten mesh preform together with the steel mold to the heating furnace, raise the temperature of the heating furnace from room temperature to 500°C-700°C and keep it warm for 10-120 minutes to obtain a preheated tungsten mesh preform; Aluminum metal is heated at 700°C to 900°C until it melts;
步骤六:得到预热的钨网预制体置于压力机台面上,将熔融的铝金属倒入钢模内预热的钨网预制体上;Step 6: Place the preheated tungsten mesh prefabricated body on the press table, and pour molten aluminum metal onto the preheated tungsten mesh prefabricated body in the steel mold;
步骤七:通过压力机施加压力,使熔融的铝金属浸渗到预热的钨网预制体中,压力为30~80MPa;Step 7: Apply pressure through a press to impregnate the molten aluminum metal into the preheated tungsten mesh prefabricated body, and the pressure is 30-80MPa;
步骤八:待熔融的铝金属完全浸渗到预热的钨网预制体中,保持压力1~5min并自然冷却;Step 8: The molten aluminum metal is completely impregnated into the preheated tungsten mesh prefabricated body, keeping the pressure for 1-5 minutes and cooling naturally;
步骤九:脱模,取出铸锭,即为钨网增韧铝基复合材料;Step 9: Demoulding, taking out the ingot, which is the tungsten mesh toughened aluminum matrix composite material;
本发明的有益效果为:The beneficial effects of the present invention are:
本发明以含硼颗粒和/或含钆颗粒作为中子吸收组元,以钨网作为γ射线吸收组元,采用压力浸渗工艺在含硼和/或钆的钨网预制体中渗入铝金属,制备出的复合材料具有致密度高、强韧性良好,γ射线和中子辐射综合屏蔽效果好的特点,满足核屏蔽材料结构功能一体化的要求。In the present invention, boron-containing particles and/or gadolinium-containing particles are used as neutron-absorbing components, tungsten mesh is used as gamma-ray-absorbing components, and aluminum metal is infiltrated into boron- and/or gadolinium-containing tungsten mesh prefabricated body by pressure infiltration process , the prepared composite material has the characteristics of high density, good strength and toughness, and good comprehensive shielding effect of γ-ray and neutron radiation, which meets the requirements of nuclear shielding material structure and function integration.
本发明制备的一种具有γ射线和中子屏蔽功能的钨网增韧铝基复合材料中含钨体积分数为1%~50%,致密度大于99%。复合材料的伽马射线屏蔽性能随钨含量增加而增加,当钨体积分数大于20%时,复合材料的伽马射线线吸收系数大于0.3cm-1;此时,若以钨颗粒形式添加,拉伸受力时复合材料呈脆性断裂,断裂延伸率小于0.5%;若以钨网形式添加,拉伸受力时复合材料的断裂延伸率可达2~5%,能更好的满足屏蔽材料结构功能一体化需求。本发明提供了一种具有γ射线和中子屏蔽功能的钨网增韧铝基复合材料制备方法,制备方法简单、易操作、工艺容易控制,制备出的复合材料致密性高、强韧性好、兼具中子和伽马射线屏蔽性能。The tungsten mesh toughened aluminum-based composite material prepared by the invention has the function of shielding gamma rays and neutrons. The volume fraction of tungsten is 1% to 50%, and the density is greater than 99%. The gamma ray shielding performance of the composite material increases with the increase of tungsten content. When the tungsten volume fraction is greater than 20%, the gamma ray absorption coefficient of the composite material is greater than 0.3cm-1; at this time, if it is added in the form of tungsten particles, the pull The composite material is brittle and fractured under tensile stress, and the elongation at break is less than 0.5%. If it is added in the form of tungsten mesh, the elongation at fracture of the composite material can reach 2-5% under tensile stress, which can better meet the structure of shielding materials. Functional integration requirements. The invention provides a method for preparing a tungsten mesh toughened aluminum-based composite material with gamma-ray and neutron shielding functions. The preparation method is simple, easy to operate, and the process is easy to control. The prepared composite material has high density, good toughness, and Combines neutron and gamma ray shielding properties.
附图说明Description of drawings
下面结合附图和具体实施方法对本发明做进一步详细的说明。The present invention will be described in further detail below in conjunction with the accompanying drawings and specific implementation methods.
图1是本发明的钨网增韧铝基复合核屏蔽材料微观组织示意图;Fig. 1 is the schematic diagram of the microstructure of the tungsten mesh toughened aluminum-based composite nuclear shielding material of the present invention;
图2是本发明的含钨颗粒体积分数为20%的钨硼铝复合材料与钨网体积分数为20%的钨网增韧铝基复合核屏蔽材料的拉伸应力应变曲线对比示意图。Fig. 2 is a schematic diagram comparing the tensile stress-strain curves of the tungsten-boron-aluminum composite material with a volume fraction of tungsten particles of 20% and the tungsten mesh toughened aluminum-based composite nuclear shielding material with a volume fraction of tungsten mesh of 20% according to the present invention.
具体实施方式Detailed ways
下面结合附图对本发明做进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings.
为了制备一种具有对γ射线和中子具有综合屏蔽能力,同时兼顾良好力学性能的结构功能一体化核屏蔽材料,如图1所示,下面对一种钨网增韧铝基复合核屏蔽材料制备方法的步骤和功能进行详细的说明;In order to prepare a structure-functional integrated nuclear shielding material with comprehensive shielding ability for γ-rays and neutrons and good mechanical properties, as shown in Figure 1, a tungsten mesh toughened aluminum-based composite nuclear shielding material is The steps and functions of the material preparation method are described in detail;
实施例一:Embodiment one:
按体积分数称取24.1%的钨网,3%硼粉,其中钨网目数包括100目和150目两种,将称量硼粉与无水乙醇混合配置成浓度为500%的含硼悬浊液,同时将不同目数的钨网放入浓碱中清洗并裁切成所需的形状和尺寸;将含硼悬浊液用毛刷刷在钨网表面并放入50℃的干燥箱中干燥10min,后称量以确定硼颗粒附着到钨网上的含量,直到含量满足屏蔽性能要求。再将100目和150目含硼的钨网按照交错层叠方式和0°铺层角度进行层叠并用石墨垫片将层叠的钨网上下夹紧,用螺栓固定得到预制件;采用压力机将预制件压入钢模,后转移至650℃的加热炉中保温90分钟得到预热的钨网预制体;同时将铝基体在890℃加热至熔化并将其浇铸到钢模内的预热体上,通过压力机施加压力,使熔融的铝基体浸渗到预热的钨网预制件中,保持压力并自然冷却;最后脱模取出铸锭即得到硼/钨网/铝复合屏蔽材料;Weigh 24.1% tungsten mesh and 3% boron powder according to the volume fraction, wherein the tungsten mesh includes two types of 100 mesh and 150 mesh, and mix the weighed boron powder and absolute ethanol to form a boron-containing suspension with a concentration of 500%. At the same time, clean the tungsten mesh with different meshes in concentrated alkali and cut it into the desired shape and size; brush the boron-containing suspension on the surface of the tungsten mesh with a brush and put it in a drying oven at 50°C Dry in medium for 10 minutes, and then weigh to determine the content of boron particles attached to the tungsten mesh until the content meets the shielding performance requirements. Then stack 100 mesh and 150 mesh boron-containing tungsten mesh according to the staggered stacking method and 0° layering angle, clamp the stacked tungsten mesh up and down with graphite gaskets, and fix the prefabricated parts with bolts; Press into the steel mold, and then transfer to a heating furnace at 650°C for 90 minutes to obtain a preheated tungsten mesh preform; at the same time, heat the aluminum matrix at 890°C to melt and cast it on the preheated body in the steel mold, Apply pressure through a press to impregnate the molten aluminum matrix into the preheated tungsten mesh preform, keep the pressure and cool naturally; finally demoulding and taking out the ingot to obtain the boron/tungsten mesh/aluminum composite shielding material;
实施例二:Embodiment two:
按体积分数称取24.1%的钨网,3%硼粉,其中钨网目数包括100目和150目两种,将称量硼粉与无水乙醇混合配置成浓度为500%的含硼悬浊液,同时将不同目数的钨网放入浓碱中清洗并裁切成所需的形状和尺寸;将含硼悬浊液用毛刷刷在钨网表面并放入50℃的干燥箱中干燥10min,后称量以确定硼颗粒附着到钨网上的含量,直到含量满足屏蔽性能要求。再将100目和150目含硼的钨网按照交错层叠方式和45°铺层角度进行层叠并用石墨垫片将层叠的钨网上下夹紧,用螺栓固定得到预制件;采用压力机将预制件压入钢模,后转移至700℃的加热炉中保温90分钟得到预热的钨网预制体;同时将铝基体在890℃加热至熔化并将其浇铸到钢模内的预热体上,通过压力机施加压力,使熔融的铝基体浸渗到预热的钨网预制件中,保持压力并自然冷却;最后脱模取出铸锭即得到硼/钨网/铝复合屏蔽材料。Weigh 24.1% tungsten mesh and 3% boron powder according to the volume fraction, wherein the tungsten mesh includes two types of 100 mesh and 150 mesh, and mix the weighed boron powder and absolute ethanol to form a boron-containing suspension with a concentration of 500%. At the same time, clean the tungsten mesh with different meshes in concentrated alkali and cut it into the desired shape and size; brush the boron-containing suspension on the surface of the tungsten mesh with a brush and put it in a drying oven at 50°C Dry in medium for 10 minutes, and then weigh to determine the content of boron particles attached to the tungsten mesh until the content meets the shielding performance requirements. Then the 100 mesh and 150 mesh boron-containing tungsten meshes are stacked according to the staggered stacking method and the layering angle of 45°, and the stacked tungsten meshes are clamped up and down with graphite gaskets, and the prefabricated parts are obtained by fixing them with bolts; Press into the steel mold, and then transfer to a heating furnace at 700°C for 90 minutes to obtain a preheated tungsten mesh preform; at the same time, heat the aluminum matrix at 890°C to melt and cast it on the preheated body in the steel mold, Apply pressure through a press to impregnate the molten aluminum matrix into the preheated tungsten mesh preform, keep the pressure and cool naturally; finally demoulding and taking out the ingot to obtain the boron/tungsten mesh/aluminum composite shielding material.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211723006.2A CN115810434A (en) | 2022-12-30 | 2022-12-30 | Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211723006.2A CN115810434A (en) | 2022-12-30 | 2022-12-30 | Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN115810434A true CN115810434A (en) | 2023-03-17 |
Family
ID=85487129
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211723006.2A Pending CN115810434A (en) | 2022-12-30 | 2022-12-30 | Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115810434A (en) |
-
2022
- 2022-12-30 CN CN202211723006.2A patent/CN115810434A/en active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105200274B (en) | A kind of preparation method of neutron absorber material | |
CN104946911B (en) | Preparation method of high volume fraction B4C/Al composite material for spent fuel storage grid | |
CN107141004B (en) | Boron carbide composite material and preparation method thereof | |
CA2259448C (en) | Metal matrix compositions for neutron shielding applications | |
CN106756164A (en) | A kind of thermal structure function integration B4The preparation method of C/Al neutron absorber materials | |
CN108335760B (en) | Preparation method of high-uranium-loading-capacity dispersed fuel pellet | |
CN104926304B (en) | A kind of gadolinium oxide ceramics and preparation method thereof | |
CN111910113A (en) | Boron-containing particle reinforced tungsten aluminum alloy composite shielding material and preparation method thereof | |
WO2019114314A1 (en) | Max-phase ceramic tubing and preparation method therefor, and nuclear fuel cladding tube | |
CN108130438A (en) | A kind of preparation method of thermal structure function integration boron carbide enhancing aluminium base neutron absorber material | |
CN108504909A (en) | A kind of aluminum-base compound shielding material and preparation method thereof | |
CN104016680B (en) | A kind of B 4c base laminated ceramic composite and preparation method thereof | |
CN106756281B (en) | A kind of neutron absorbing material with high rare earth content and preparation method thereof | |
CN111892414A (en) | A kind of short carbon fiber reinforced boron carbide composite material and preparation method thereof | |
CN104130546A (en) | Preparation method for nuclear radiation shielding material | |
CN118162623B (en) | A three-level high entropy alloy particle reinforced aluminum-based composite material and preparation method thereof | |
CN115810434A (en) | Tungsten mesh toughened aluminum-based composite nuclear shielding material and preparation method thereof | |
CN101565786B (en) | Radiation protection aluminum-based composite material and vacuum hot-pressing preparation method thereof | |
CN113698206B (en) | A kind of preparation method of nuclear grade boron carbide pellet | |
CN107652509A (en) | A kind of lead-boron polythene composite material and preparation method thereof | |
CN1746324A (en) | High-energy ray shielding Pb-based composite material and preparation method thereof | |
CN115011839A (en) | A kind of titanium gadolinium alloy material for nuclear shielding, its preparation method and application | |
CN119144878B (en) | A neutron and gamma ray integrated aluminum-based nuclear shielding material and preparation method thereof | |
CN116543945A (en) | A low-cost aluminum-based composite shielding material and its preparation method | |
CN105316504B (en) | Material mixing method for preparing wolfram carbide particle (WCp)/2024Al composite radiation shield material |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |