氚在锆合金包壳材料中的扩散行为模拟

基于氚扩散基本模型建立了氚扩散行为一维模拟程序,对模拟程序进行了典型实验验证,模拟结果与实验结果符合较好。分析了不同氚浓度、温度分布对锆合金包壳材料中氚的扩散行为的影响。分析结果表明:包壳-芯块间隙内氚浓度的升高会导致进出包壳的氚扩散通量提高,渗透通量增大;由于包壳氧化层相对较低的扩散系数,包壳氧化层的存在对氚渗透有较大的限制作用;温度对氚扩散速率的影响很显著,温度越高,扩散速度越快;锆合金外表面氧化层的相对低温限制了氚渗透出包壳管的速率,温度梯度导致的热致扩散有利于氚向包壳冷测扩散。     

Nb-Al合金高温氧化机理

通过自编软件建立了铝氧化膜与基体铌界面的原子集团模型,用递归法计算了合金的原子埋置能、原子结合能等电子参数,从电子层面分析铌合金高温氧化机理.研究表明:铝通过晶界扩散偏聚在合金表面,并与氧结合生成致密的Al2O3氧化膜,阻挡氧向铌基体扩散.晶界和稀土元素能提高氧化膜与基体间的原子结合能,增加其界面的结合强度,加强氧化膜与基体铌间的黏附性.因此,通过在合金中添加稀土元素或细化合金晶粒均能提高铌合金的抗高温氧化性能.     

溶胶-凝胶法制备Fe-Al_2O_3巨磁旋光薄膜

用溶胶-凝胶法制备了Fe-Al2O3铁磁金属-非磁绝缘体基体薄膜。实验结果表明,当Fe与Al2O3的质量比为1∶1,热处理温度为420℃时,所制备的薄膜具有最大的磁致旋光(Faraday)效应,测得的费尔德(Verdet)常数V=(6.8×104)°/(T.cm)。通过分析,得出了Fe-Al2O3薄膜巨磁Faraday旋光效应主要是由光、磁场与薄膜相互作用产生剧烈塞曼(Zeeman)分裂引起的。对影响薄膜Faraday旋光效应的各种主要因素进行了讨论。     

溶胶-凝胶法制备Fe-Al_2O_3巨磁旋光薄膜北大核心

用溶胶-凝胶法制备了Fe-Al2O3铁磁金属-非磁绝缘体基体薄膜。实验结果表明,当Fe与Al2O3的质量比为1∶1,热处理温度为420℃时,所制备的薄膜具有最大的磁致旋光(Faraday)效应,测得的费尔德(Verdet)常数V=(6.8×104)°/(T.cm)。通过分析,得出了Fe-Al2O3薄膜巨磁Faraday旋光效应主要是由光、磁场与薄膜相互作用产生剧烈塞曼(Zeeman)分裂引起的。对影响薄膜Faraday旋光效应的各种主要因素进行了讨论。     

Fe-Cr-Al合金高温氧化行为电子理论研究

从电子层面系统研究Fe-Cr-Al合金氧化膜的形成机理,杂质硫对氧化膜黏附性的影响,稀土元素在改善氧化膜黏附性方面的作用,揭示合金氧化的物理本质.研究表明氧使Al在合金表层的环境敏感镶嵌能最低,促使Al原子从合金内部向合金表面扩散,最终在合金表面偏聚.由于氧与Al间的亲和力较大,氧原子易与Al结合生成Al2O3保护膜.杂质S在基体/氧化膜界面的环境敏感镶嵌能较低,可通过扩散偏聚在基体/氧化膜界面,削弱氧化膜与合金基体的结合力.当合金中加入Y后,Y易与S结合形成稳定的硫化物,阻碍S向基体/氧化膜界面的偏聚,显著提高氧化膜的黏附性,提高合金抗高温氧化能力.     

Fe-Cr-Al合金氧化膜形成机理电子理论研究

通过自编软件建立了Fe-Cr-Al合金表面、氧化膜/基体界面模型,采用递归法计算了合金元素在Fe-Cr-Al合金表面、氧化膜/基体界面的环境敏感镶嵌能、亲和能、结合能、态密度等电子结构参数.从电子层次系统研究了Fe-Cr-Al合金氧化膜的形成机理、稀土元素和杂质硫对氧化膜形成过程及黏附性的影响机理.研究表明Fe-Cr-Al合金中Al的偏聚驱动力远大于Y,Cr.氧化初期氧从合金表面向合金内部扩散,合金内部Al向合金表面扩散,使合金形成富铝、氧表面层;氧与Al间的亲和力较大（亲和能低）,氧原子容易与Al结合生成Al₂O₃保护膜;合金中加入Y后,Y在合金表面偏聚,抑制Al向合金表面扩散,氧化膜的横向生长得到有效控制,从而避免氧化膜皱褶形貌的发生,提高氧化膜的黏附性;合金内部的S通过扩散汇集在基体/氧化膜界面,S使界面区原子的总能增高,总态密度降低,减小了界面的稳定性,进而削弱氧化膜与合金基体的结合力. 关键词： 电子结构 高温氧化 Fe-Cr-Al合金     

硬质合金表面Ti系涂层退除后的界面性能研究

采用电弧离子镀技术(AIP)在YW2合金基体表面制备了TiAlN涂层,通过化学方法退除基体上的涂层,分析了硬质合金表面退除涂层后和镀覆涂层前成分和元素存在形态的变化。发现当样品在30%H₂O₂、草酸钾COOK(1.5mol·L-1)、缓蚀剂葡萄糖酸钠GA和NaOH,V_NaOH溶液∶V_30%H2O2∶V_COOK溶液=1∶1∶1,45 ℃时,45 min可以退除涂层,肉眼未观察到基体表面受腐蚀。涂层退除后样品表面光亮,呈现合金未镀覆涂层前颜色。通过对退镀后YW2基体和基体镀覆涂层前的表面XPS定性及定量分析发现,退除涂层后,基体表面W元素结合能和N元素主峰结合能与XPS结合能与参照表上对应结合能变化很小,元素的价态没有发生变化;镀覆TiAlN涂层时扩散到合金浅表层的Al,Ti,N元素,造成表面Al,Ti,N元素含量较镀覆涂层前增加,结合能位置偏移,形成AlN和TiN,有利于重新镀覆的涂层与合金基体的结合。     

T91钢和SIMP钢表面AlOx涂层在600℃静态液态铅铋共晶中的稳定性和腐蚀行为

铁素体/马氏体钢,如T91钢和SIMP钢,被选为第4代铅冷快堆和加速器驱动系统(ADS)的主要候选结构材料.但容器钢与液态铅铋共晶(LBE)在高温下的相容性限制了它们的应用.铁素体/马氏体钢在600℃的LBE中腐蚀严重.为了保护铁素体/马氏体钢免受高温LBE腐蚀,在钢表面制备AlO_x (x <1.5)涂层.本文采用磁控溅射法在T91钢和SIMP钢表面制备了AlO_x涂层.对表面有涂层的T91钢和SIMP钢以及表面无涂层的T91钢和SIMP钢在600℃的饱和氧浓度的LBE中腐蚀300 h和700 h的结果进行比较.结果表明,涂层钢表面的氧化层比无涂层钢表面的氧化层薄,这表明AlO_x涂层可以有效防止铁、铬和氧元素的快速扩散.然而,在LBE中腐蚀700 h后, AlO_x涂层出现裂纹,表面有涂层的T91钢和SIMP钢均遭受到明显的氧化腐蚀,说明该涂层在600℃的LBE中可以在短时间内保护基体免受高温腐蚀.但是涂层在600℃的LBE中不能长时间保持稳定.这可能是由于此次实验条件制备的AlO_x     

热处理对青铜法制作的多芯Nb_3Sn超导体的影响

本文研究了热处理对实用多芯Nb,Sn超导体的影响.在(650—750℃热处理时,Nb_3Sn层厚度Y与时间t可用Y∞t~(72)关系表示,这里0.130≤n≤0.195.多芯复合材料在热处理过程中,Cu-Sn基体中Sn量消耗显著地影响Nb_3Sn生长速率,考虑了这一因素的Nb_3Sn生长动力学修正公式能对实验结果进行解释.700℃热处理10—100小时,Nb_3Sn品粒尺寸是热处理时间的一个函数。晶粒大小随热处理时间增长而增大,并且∞t~m,m=0.205.对于锡青铜基体与铌比值分别为1.84和3.05的两种导体,在700℃热处理时,其临界电流是热处理时间的一个函数.I_c(t)中最大值取决于Nb_3Sn层增厚和晶粒度长大的综合效果.T_c随热处理时间增长和温度升高而峪有提高.这大概与Nb_3Sn层化学计量比有关.     

纳米铝热剂Al/SiO_2层状结构铝热反应的分子动力学模拟

利用分子动力学模拟方法和反应力场势函数研究了Al/SiO_2层状纳米体系的铝热反应,模拟了在不同初始温度下(600,700,800,900,1000和1100 K)绝热反应的结构变化和能量性质,发现Al/SiO_2体系的铝热反应是自加热的氧化还原反应,当初始温度为900和1000 K时,Al经历了熔化前的一个临界状态,与SiO_2的铝热反应比较活跃,系统温度随着反应时间的增加不断升高,当初始温度为600,700,800和1100 K时,初始温度越高,在Al和SiO_2界面形成的Al-O层越薄,系统发生铝热反应达到的最终绝热温度越高,所用的时间(有效反应时间τ)越短,即界面扩散阻挡层的厚度对铝热反应的自加热速率产生了影响,初始温度为600,700,800,1100K时的自加热速率分别为3.4,3.5,4.7和5.4K/p8.A1/SiO_2体系的铝热反应析出了Si单质,与实验结果相符合。     

Effect of heat treatment on the microstructure and microhardness of cold-sprayed tin bronze coating

Tin bronze (TB) powder was deposited on a stainless steel substrate by cold spraying. Post-deposition heat treatment was conducted in an electrical resistance furnace under nitrogen atmosphere at a temperature of 850 °C for 3 h. The effect of heat treatment on the microstructure and microhardness of cold-sprayed TB coating was investigated. It was found that the as-sprayed TB coating presented a dense microstructure. Heat treatment significantly influenced the microstructure and microhardness of cold-sprayed TB coating. A distinguishable diffusion layer of about 150 μm was formed in the coating near the coating/substrate interface. A compound was precipitated in the diffusion layer. The microhardness in the coating was changed gradually along the coating from the interface to the coating surface after heat treatment. The microhardness in the diffusion layer was high owing to the precipitation of hard phase, while it was much low in other area due to the obvious grain growth during annealing.     

Heat treatment induced intermetallic phase transition of arc-sprayed coating prepared by the wires combination of aluminum-cathode and steel-anode

A method to prepare intermetallic composite coatings employing the cost-efficient electric arc spraying twin wires assistant with suitable heat treatment was developed. In this study, a Fe-Al composite coating was produced by spraying twin wires, i.e. a carbon steel wire as the anode and an aluminum wire as the cathode. The inter-deposited Fe-Al coating was transformed in-situ to Fe-Al intermetallic composite coating after a post annealing treatment. The effect of annealing treatment conditions on phase composition, microstructure and mechanical properties of the coating was investigated by using XRD, SEM, EDS and OM as well as microhardness tester. The results show that the desirable intermetallic phases such as Fe₂Al₅, FeAl and Fe₃Al are obtained under the annealing condition. The main oxide in the coating is FeO which can partially transform to Fe₃O₄ up to the annealing condition.     

Al–Cu intermetallic coatings processed by sequential metalorganic chemical vapour deposition and post-deposition annealing

Sequential processing of aluminum and copper followed by reactive diffusion annealing is used as a paradigm for the metalorganic chemical vapour deposition (MOCVD) of coatings containing intermetallic alloys. Dimethylethylamine alane and copper N,N′-di-isopropylacetamidinate are used as aluminum and copper precursors, respectively. Deposition is performed on steel and silica substrates at 1.33 kPa and 493–513 K. Different overall compositions in the entire range of the Al–Cu phase diagram are obtained by varying the relative thickness of the two elemental layers while maintaining the overall thickness of the coating close to 1 μm. As-deposited films present a rough morphology attributed to the difficulty of copper to nucleate on aluminum. Post-deposition annealing is monitored by in situ X-ray diffraction, and allows smoothening the microstructure and identifying conditions leading to several Al–Cu phases. Our results establish a proof of principle following which MOCVD of metallic alloys is feasible, and are expected to extend the materials pool for numerous applications, with innovative thin film processing on, and surface properties of complex in shape parts.     

One way of surface alloying treatment on iron surface based on surface mechanical attrition treatment and heat treatment

A method of surface alloying treatment has been developed: Ni powders were welded into the surface of iron plates by Surface Mechanical Attrition Treatment (SMAT), followed by annealing at certain temperature for 30 min. A Ni-Fe alloy layer with thickness about 100 μm in the sample surface was fabricated on pure iron plate. Scanning electron microscope (SEM), glow discharge spectrum (GDS), and X-ray diffraction (XRD) methods were used to analyze the microstructure, the composition and the phases of the alloy layer. Studies on the interface microstructure indicated that there was significant atomic diffusion and formation of multilayer of intermetallic compound and solid solution in SMAT process. Subsequent annealing accelerates the alloying process. The corrosion test shows the sample by SMAT treated with Ni powders exhibit the best corrosion resistance.     

Phase evolution of an aluminized steel by oxidation treatment

Effects of temperature and time on the microstructure and phase evolution for different thermal treatments were investigated with respect to the measurement of intermetallic layer thickness, phase identification and microhardness distribution in the aluminized zone of a steel substrate. The intermetallic phases present in the aluminized region after hot dip aluminizing is mainly Fe₂Al₅. The thickness of the intermetallic layers increases with increasing oxidation temperature and time. In the oxidation treatments of the aluminized steel in air, the initial Fe₂Al₅ phase remains at the temperature below 950 °C in 2-h, and the Fe₂Al₅ phase is completely transformed into low iron content Fe-Al intermetallics due to oxidation at 950 °C for 4 h. However, the Fe₂Al₅ phase remains in the outer layer of the aluminized samples diffusion-treated in vacuum regardless of diffusion time. The microhardness values of the Al₂O₃ and the intermetallic Fe₂Al₅, FeAl₂, FeAl and Fe₃Al phases are HV1150, HV1010, HV810, HV650 and HV320, respectively. The oxide layer formed on the steel substrate has an extremely fast adherence to the steel substrate and excellent properties of thermal shock resistance, high temperature oxidation resistance and anti-liquid aluminum corrosion.     

Vanadium carbide coatings on die steel deposited by the thermo-reactive diffusion technique

Thermal reactive diffusion coating of vanadium carbide on DIN 1.2367 die steel substrate was performed in a powder mixture consisting of ferro-vanadium, ammonium chloride, alumina and naphthalene at 950, 1050 and 1150 °C for 1-5 h. The carbide layers were characterized by means of microstructure, microhardness, X-ray diffraction and chemical analysis. Depending on the coating process time and temperature, the thickness of the vanadium carbide layer formed on the substrate ranged from 2.3 to 23.2 μm. The hardness of vanadium carbide layers was about 2487 HV. Dry wear tests for uncoated and coated DIN 1.2367 die steel were carried out on pin-on-disk configuration and at a sliding speed of 0.13 m/s. The results showed superior wear properties of the coated samples. The kinetics of vanadium carbide coating by the pack method was also studied and the activation energy for the thermo-reactive diffusion process was estimated to be 173.2 kJ/mol.     

热处理对纳米金刚石涂层场发射性能的影响

用旋涂法在金属钛衬底上涂敷纳米金刚石,经过适当的热处理形成金刚石涂层与金属钛衬底的化学键合,即形成衬底与涂层之间的过渡层,从而为纳米金刚石颗粒提供电子,使其成为有效的发射体。用扫描电镜、原子力显微镜、X射线衍射和拉曼散射等手段分析了温度对键合效果以及场发射性能的影响,温度过高或过低都不利于提高纳米金刚石涂层的场发射性能,只有在700℃左右对样品进行热处理,才能得到较好的键合状态。改变涂膜时旋涂的次数以获得不同涂层厚度的样品,对其在700℃的相同温度下进行热处理,发现涂层过厚或过薄都不利于样品发射性能的提高。旋涂9次并于700℃热处理的样品具有较好的场发射性能,其发射阈值场强可达4.6V/μm,而15.3V/μm场强下的电流密度为59.7μA/cm2。     

碳化钛及其复合涂层材料抗氚渗透层的稳定性

研究了３１６Ｌ不锈钢表面镀ＴｉＣ和ＴｉＮ＋ＴｉＣ复合涂层材料的抗氚透层在聚变环境中的稳定性。研究结果表明,ＴｉＣ和ＴｉＮ＋ＴｉＣ复合涂层材料经化学热处理后在其表面层生成的抗氚渗透层能抗Ｈ＾＋离子辐照,能抗很大的温度梯度和热循环,经长时间实验证明这些涂层材料的抗氚渗透层性能稳定。     

Modeling of diffusion and absorption processes of tritium in beryllium membranes

The permeation of tritium produced in thermonuclear fusion through metallic membranes, which is a topical problem in radiation physics, is addressed. A physical model for the permeation of hydrogen through a beryllium membrane is proposed which takes into account the oxide layer on the surface of the membrane. The model is implemented in the form of a system of differential equations, which is solved by numerical methods. As a result of the computer modeling it is shown that as the temperature is raised, the oxide layer in a certain interval blocks the permeation of tritium in the membrane, and it is found that the tritium is distributed in a rather limited region of the membrane over its thickness. This circumstance will permit the use of special processing by etching or mechanical treatment. Zh. Tekh. Fiz. 69, 38–41 (July 1999) Deceased