w(Co)对CB2钢显微组织和力学性能的影响

为研究w(Co)对CB2钢微观组织和力学性能的影响，调整CB2钢中w(Co)为0.5%，1.0%，1.5%，2.0%和3.0%.利用光学显微镜(OM)、扫描电镜(SEM)、室温拉伸等检测方法研究w(Co)对试验钢微观组织和力学性能的影响规律，结合Thermo-Calc和JMatpro-7.0模拟结果解释其影响机理.研究发现:w(Co)增加提高铬当量的值，使试验钢中δ铁素体含量减少，当w(Co)增加到1.5%时，δ铁素体基本消失;材料的抗拉强度随w(Co)的增加而增加，而延长率则先增加后降低;结果表明，w(Co)为1.5%时综合性能较好，即抗拉强度达到805.13MPa，延长率达到20.4%，布氏硬度为260.     

单原子Co修饰TiO2(101)面的结构和析氢性能的第一性原理研究

通过基于密度泛函理论（DFT）+U的第一性原理方法研究了单原子Co在TiO₂（101）面的掺杂位置和方式、几何结构和整体能量以及掺杂后产物的制氢反应机制，得到了稳定且易出现的单原子修饰结构，即单原子Co吸附在4个O组成的表面空隙的中心位，记为Co/TiO₂（101）。进一步对Co/TiO₂（101）的析氢反应过程和性能进行研究，确定了当且仅当TiO₂（101）面完成表面羟基化反应后，H原子全覆盖的TiO₂（101）表面才能进行后续的析氢反应；此时单原子Co是唯一的反应位点，整体的制氢反应自由能ΔG_H*比Co（111）面更加趋近于0，显示出其具有远优于金属Co的催化性能。此外，Co和TiO₂间的电荷转移和相互作用使TiO₂带隙出现新的掺杂能级，可带来作为光催化基材的TiO₂光吸收性能的改善。     

多主元FeNiMnCr0.75Alx高熵合金微观结构和力学性能的研究

研究了合金中Al含量的增加对铸态FeNiMnCr_0.75Al_x（x=0.25，0.5，0.75，原子分数）高熵合金晶体结构及力学性能的影响。采用X射线衍射仪（XRD）和透射电子显微镜（TEM）对合金的微观结构及形貌进行分析，采用维氏硬度计和MTS万能试验机测试合金的硬度和室温压缩性能。试验结果表明，铸态下，FeNiMnCr_0.75Al_x高熵合金均由bcc和fcc两种晶体结构的相构成。随着Al含量的增加，合金中bcc结构的相的相对含量逐渐增加，导致硬度和压缩屈服强度也随之升高，应变量降低；且Al含量的增加最终也促使合金中无序bcc结构的相逐渐转变为Ni：（Mn+Al）=1：1（原子分数比）型有序bcc结构的相。     

Al涂层/AZ91镁合金复合铸造界面的研究

对型芯预喷涂一层Al涂层,将AZ91镁合金液浇注到铸型中实现基体和涂层的结合,对凝固后的结合界面组织和相组成进行分析。结果表明,AZ91镁合金液和Al涂层表面的氧化物发生反应,实现了界面间的润湿,形成冶金结合界面。该界面包含3个扩散层:镁合金基体一侧为(Al₁₂Mg₁₇+δ_Mg)共晶组织;中间层为Al₁₂Mg₁₇金属间化合物;Al涂层一侧为Al₃Mg₂金属间化合物,并弥散分布着一些氧化物。试验结果证明,通过复合铸造的方法可以实现Al涂层和镁合金基体的冶金结合。     

Ti-1300钛合金挤压管材组织性能研究

通过室温拉伸测试和显微组织观察，研究了挤压温度和热处理工艺对Ti-1300钛合金挤压管材显微组织和力学性能的影响，讨论了热加工工艺、显微组织和力学性能之间的关系。结果表明：Ti-1300钛合金在两相区挤压后的横向组织均匀细小，纵向组织沿挤压加工流线破碎均匀；其拉伸强度高达1 445 MPa。管材在相变点以上的高温固溶组织主要由等轴β相晶粒组成，具有较好的塑性。合金两相区挤压后具有较好的强度和塑性的匹配，两相区挤压的塑性明显优于β单相区挤压，尤其面缩。试样经过固溶时效处理后显微组织明显细化，强度大幅度提高，可达1 300 MPa以上。     

Effect of heat treatment on microstructures and properties of a novel Al-Zn-Mg-Cu alloy for oil drilling

In view of the special requirements for strength, heat resistance and corrosion resistance of Al-Zn-Mg-Cu alloy for oil drilling, the Al-6.2 Zn-2.5 Mg-1.6 Cu alloy was prepared by increasing Cu content on basis of Russian Series 1953 alloy. The effect of heat treatment on the microstructures and properties of the alloy was characterized by optical microscope(OM), scanning electron microscope(SEM) and transmission electron microscope(TEM), and investigated by tensile test at room temperature, thermal exposure test and corrosion test. The results show that the strength after T6 aging treatment exhibit a decrease trend as an increase of the solution temperature from465 °C to 480 °C. After the solution treated by the rate of 470 °C/1 h, second phases dissolve into the matrix very well and the strength property reaches optimum. The alloy has better comprehensive properties treated by a solution treatment of 470 °C/1 h and then followed by an aging treatment of 120 °C/24 h + 170 °C/1 h + 120 °C/24 h. Under the aging state, the precipitated phases inside the grains are suitable in size, while on the grain boundary distribute discontinuously and the precipitate-free zone is obvious. Besides, the alloy still maintain high tensile properties. The yield strength, tensile strength and elongation are 650 MPa, 686 MPa,12.0%, respectively. The yield strength retention after heat exposure is 92%. The alloy has good corrosion resistance and the exfoliation corrosion degree. The average corrosion rate in the H_2S and CO_2 environment is 0.0024 mm/a, which is far less than the required 0.12 mm/a. It is insensitive to H_2S and CO_2 environments.     

团簇Co3FeP异构化反应的热力学与动力学研究

为了寻找团簇Co₃FeP的稳定性、结构和内部作用力等规律，利用密度泛函理论，在B3LYP/Lanl2dz的量化水平下对团簇Co₃FeP进行理论计算，得到5种优化构型，并从化学反应热力学与动力学的角度对其异构化反应中的反应物、过渡态和生成物进行了讨论分析。结果表明，所有构型均为C1对称且构型的空间结构对其熵值有影响；构型的稳定性主要由金属原子与非金属原子所决定，并且在常温常压下构型1^（3）、2^（3）和3^（3）可以稳定存在，是大部分异构化反应的最终产物。因此，在实际材料的开发中，不仅需要注意金属原子与非金属原子之间的作用力以确保构型的稳定性，还应首先考虑对稳定构型1^（3）、2^（3）和3^（3）进行相关研究。     

基于40Cr高温动态力学性能的磨削表面动态再结晶行为

通过分离式霍普金森压杆(SHPB)实验得到了40Cr合金钢在高温高应变率下真应力-真应变曲线，据此确定了材料发生动态再结晶的临界条件.采用解析法和实验法分别求解了磨削强化层的温度场和塑性应变场分布.结果表明，磨削强化层在磨削深度方向具有较大的温度和塑性应变梯度;150μm强化层内会发生奥氏体转变;磨削表面最高温度可达1060℃.在磨削亚表面60μm内会产生剧烈的塑性变形，达到了再结晶的临界条件.较大的磨削深度使磨削强化层塑性应变增大，再结晶现象越充分，微观组织细化程度越高.     

Superior corrosion resistance-dependent laser energy density in(CoCrFeNi)95Nb5 high entropy alloy coating fabricated by laser cladding

(CoCrFeNi)95Nb5 high entropy alloy(HEA)coatings were successfully fabricated on a substrate of Q235 steel by laser cladding technology.These(CoCrFeNi)95Nb5 HEA coatings possess excellent properties,particularly corrosion resistance,which is clearly superior to that of some typical bulk HEA and common engineering alloys.In order to obtain appropriate laser cladding preparation process parameters,the effects of laser energy density on the microstructure,microhardness,and corrosion resistance of(CoCrFeNi)95Nb5 HEA coating were closely studied.Results showed that as the laser energy density increases,precipitation of the Laves phase in(CoCrFeNi)95Nb5 HEA coating gradually decreases,and diffusion of the Fe element in the substrate intensifies,affecting the integrity of the(CoCrFeNi)95Nb5 HEA.This decreases the microhardness of(CoCrFeNi)95Nb5 HEA coatings.Moreover,the relative content of Cr2O3,Cr(OH)3,and Nb2O5 in the surface passive film of the coating decreases with increasing energy density,causing corrosion resistance to decrease.This study demonstrates the controllability of a high-performance HEA coating using laser cladding technology,which has significance for the laser cladding preparation of other CoCrFeNi-system HEA coatings.     

Effect of thermo-mechanical treatment on Ti–Ta-Hf high temperature shape memory alloy

The microstructure, martensitic transformation and mechanical/functional properties of Ti–Ta-Hf alloys with various thermo-mechanical treatments were investigated. The results reveal that the hot-rolling could refine the grain size and introduce a certain number of defects, resulting in the disappearance of martensitic transformation. The as-casted and solution treated Ti–Ta-Hf alloys were composed of α'' martensite phase and smaller volume of β phase. In contrast, the grain size of solution treated Ti–Ta-Hf alloy was slightly less than that of as-casted Ti–Ta-Hf alloy. This should be responsible to the higher yield stress and superior strain recovery characteristics for solution treated Ti–Ta-Hf alloy. The yield stress for the dislocation slip and the maximum recoverable strain of solution treated Ti–Ta-Hf alloy were 723 ​MPa and 5.06%, respectively.