激光熔化沉积Ti5Si3/NiTi双相金属间化合物合金耐磨性能

采用激光熔化沉积工艺制备出以块状Ti5Si3过渡金属硅化物为初生相、以Ti5Si3/NiTi共晶为基体的双相金属间化合物耐磨合金,在室温干滑动磨损条件下测试了Ti5Si3/NiTi合金的耐磨性能并讨论了其磨损机制。结果表明,由于Ti5Si3/NiTi合金良好的强韧性配合以及在磨损过程中磨损表面上形成了“无组织特征”的表面高硬度层,对合金有保护作用,合金在室温干滑动磨损条件下具有优异的耐磨性能和很低的载荷敏感性     

激光熔炼Ti5Si3／NiTi金属间化合物合金的组织及耐磨性

设计并利用激光熔炼技术制备出了以Ti5Si3为增强相、以NiTi为基体的金属间化合物新型耐磨合金，研究了增强相Ti5Si3的含量对合金显微组织、显微硬度及耐磨性能的影响。结果表明，随Ti5Si3含量的增加，合金显微组织由亚共晶向共晶、过共晶转化，增强相Ti5Si3由细层片状共晶相向块状初生相转变，合金显微硬度随之显著提高；在室温干滑动磨损条件下，Ti5Si3／NiTi金属间化合物合金具有优异的耐磨性，并随Ti5Si3增强相的增加而显著提高。Ti5Si3增强相的高硬度和NiTi基体的高韧性及伪弹性效应是该合金具有优异耐磨性能的主要原因。     

激光熔敷NiTi/Ni3Ti金属间化合物复合材料涂层组织及耐磨性

以Ni79Ti21（wt％）合金粉末为原料，采用同步送粉激光熔敷技术在BT20钛合金表面制备出NiTi／Ni3Ti金属间化合物复合材料涂层，分析了该涂层的显微组织，测试了该涂层的室温干滑动磨损性能。结果表明，激光熔敷涂层组织均匀致密，与基材呈良好的冶金结合，具有优良的抗滑动磨损性能。     

激光熔炼TiCo／Ti5Si3双相金属间化合物合金组织及耐磨性

利用激光熔炼技术制备出以金属硅化物Ti5Si3为耐磨增强相、以金属间化合物TiCo为增韧相的双相金属间化合物新型耐磨合金。用OM，SEM，XRD与EDS等方法分析了合金的显微组织、相组成及成分。在室温干滑动磨损条件下测试了合金的耐磨性能，研究了合金组织中TiCo含量对合金显微组织、硬度及耐磨性能的影响。结果表明，合金的显微组织均由块状Ti5Si3初生相及TiCo／Ti5Si3共晶基体组成并具有优异的室温干滑动耐磨损性能。随TiCo含量的增加，初生相Ti5Si3的体积分数与合金的显微硬度下降，合金的韧性与耐磨性能随之显著提高。Ti5Si3的高硬度和TiCo的高韧性是该合金具有优异耐磨性能的主要原因。     

激光熔敷Ti5Si3／NiTi金属间化合物复合材料涂层组织与耐磨性

以Ti14Si6Ni80合金粉末为原料，利用激光熔敷技术在BT9钛合金表面制得以金属硅化物Ti5Si3为增强相、以金属间化合物NiTi为基体的快速凝固金属间化合物复合材料涂层，分析了该涂层的显微组织，在室温干滑动磨损条件下测试了其耐磨性。研究结果表明，涂层硬度高、组织致密、与基材之间为完全冶金结合，在干滑动磨损试验条件下具有较好的耐磨性。涂层具有优异耐磨性的主要原因是作为耐磨增强相的金属硅化物Ti5Si3具有高硬高耐磨的特性，在涂层中起到了抗磨骨干作用，同时作为涂层基体的金属间化合物NiTi由于具有极强的原子结合键及应力诱发马氏体相变特性，本身具有优异的耐磨性，在摩擦过程中对耐磨增强相Ti5Si3起到了强力支撑作用。     

激光熔炼Ti5Si3-TiCo-Ti2Co多相金属间化合物合金的组织与耐磨性

利用激光熔炼技术制备出Ti5Si3-TiCo-Ti2Co多相金属间化合物新型耐磨合金，分析了合金的显微组织并测试了合金的室温干滑动磨损性能。结果表明，Ti5Si3-TiCo—Ti2Co多相金属间化合物耐磨合金组织均匀、致密，在室温干滑动磨损条件下具有优异的耐磨性能。Ti5Si3-TiCo—Ti2Co多相金属间化合物耐磨合金的磨损量随磨损时间的延长缓慢增加，磨损率先增加后降低；难熔金属硅化物Ti5Si3的高硬度及金属间化合物的反常屈服强度一温度关系及磨损过程中表面粘附转移保护层的形成，是Ti5Si3-TiCo—Ti2Co多相金属间化合物耐磨合金在室温干滑动磨损试验条件下具有较好耐磨性能的原因。     

钛合金表面激光熔敷Ti2Ni3Si/NiTi耐磨涂层组织与耐磨性能

以Ti-50Ni-10Si合金粉末为原料，利用激光熔敷技术在钛合金BT9基材表面制得由Ti2Ni3Si初生树枝晶和枝晶间Ti2Ni3Si／NiTi共晶组织组成的耐磨材料涂层，研究了涂层的显微组织及室温耐磨性能。结果表明，该涂层在室温干滑动磨损条件下具有优异的耐磨性能和良好的载荷特性。     

激光熔覆TiFe/β-Ti复合涂层组织及耐磨性

以Ti85-Fe15合金粉末为原料,利用激光熔覆技术在TA15钛合金表面制得了由β-Ti初生树枝晶和枝晶间TiFe金属间化合物组成的复合涂层,研究了涂层的显微组织及室温耐磨性能.结果表明,该涂层在室温干滑动磨损条件下具有优异的耐磨性能.     

Ni含量对镍钛合金的力学和摩擦学性能的影响

本文通过机械合金化和放电等离子烧结法(SPS)在1000 ℃制备具有不同Ni含量的镍钛合金,采用显微硬度仪研究不同Ni含量NiTi合金的显微硬度变化规律,通过摩擦磨损试验机和万能试验机研究NiTi合金室温摩擦学性能和力学性能,采用三维白光轮廓仪扫描磨痕形貌并计算NiTi合金的磨损体积和磨损率,采用扫描电子显微镜研究磨损表面形貌。结果表明：通过球磨和SPS制备的NiTi合金组织均匀,在镍含量低于50 wt. %时,显微组织中只有NiTi相和NiTi₂相,镍含量高于50 wt. %时,显微组织中只有NiTi相和Ni₃Ti相。Ni含量为50 wt. %时可以显著提高NiTi合金的显微硬度,随着镍含量增加NiTi合金的抗压强度降低,Ni含量为55 wt. %时可以显著改善NiTi合金的摩擦学性能,其主要磨损机理是磨粒磨损和疲劳磨损。     

等离子熔敷TiC/γ-(Fe,Ni)复合涂层组织与耐磨性

为了提高奥氏体不锈钢的耐磨性能,扩大其应用范围,以Ti-C-Fe-Ni混合合金粉末为原料,利用等离子熔敷技术在1Cr18Ni9Ti奥氏体不锈钢表面原位合成了TiC增强耐磨复合涂层。分析了涂层的显微组织结构,测试了涂层沿层深方向的硬度分布,评价了涂层在室温干滑动磨损试验条件下的摩擦磨损性能,结果表明:等离子熔敷TiC金属陶瓷增强复合涂层显微组织细小均匀,由花瓣状和少量颗粒状TiC初生相均匀分布在TiC/γ-(Fe,Ni)共晶基体上组成,涂层与不锈钢基材之间形成了完全冶金结合,涂层平均显微硬度约790 HV,涂层在室温干滑动磨损试验条件下表现出良好的耐磨性及较低的摩擦系数。     

Microstructure and tribological properties of laser clad Ti2Ni3Si/NiTi intermetallic coatings

Wear resistant Ti₂Ni₃Si/NiTi full intermetallic composite coatings with a microstructure consisting of ternary metal silicide Ti₂Ni₃Si primary dendrites and interdendritic Ti₂Ni₃Si/NiTi eutectic were fabricated on a substrate of 0.2%C low carbon steel by the laser cladding process using Ti-Ni-Si alloy powders as the precursor materials. Microstructure of the coatings was characterized by optical microscopy (OM), scanning electron microscopy (SEM), X-ray diffraction (XRD) and energy dispersive X-ray analysis (EDS). Wear resistance of the laser clad Ti₂Ni₃Si/NiTi intermetallic coatings was evaluated under dry sliding wear test conditions at room temperature. Results indicate that the Ti₂Ni₃Si/NiTi intermetallic coatings have excellent abrasive and adhesive wear resistance under dry sliding wear test conditions because of the unique combination of high yield strength and toughness of the intermetallic compound NiTi and the high hardness, strong covalent dominant atomic bonds and possible strong hardness anomaly of the ternary metal silicide Ti₂Ni₃Si with MgZn₂ type Laves crystal structure.     

Microstructure and dry sliding wear resistance of Moss-toughened Mo2Ni3Si metal silicide alloys

A wear resistant Mo₂Ni₃Si-based metal silicide alloy toughened by molybdenum-based solid solution (Mo_ss) was fabricated by the laser melting deposition (LMD) manufacturing process. Microstructure of the alloy is composed of Mo_ss primary dendrites and the matrix of the single phase Mo₂Ni₃Si. Wear resistance and friction coefficient of the alloys were evaluated under metallic dry sliding wear test conditions as a function of contact load. Results showed that the alloys have a low friction coefficient and outstanding wear resistance due to the high hardness of Mo₂Ni₃Si matrix and the high strength, ductility and toughness of Mo_ss dendrites. The wear rate and the friction coefficient of alloys are extremely insensitive to the contact load owing to the abnormal hardness–temperature relation of Mo₂Ni₃Si. The Mo_ss dendrite played the role of trapping micro-cracks and restraining brittle spalling of the Mo₂Ni₃Si matrix during wear process and improved the wear properties of Mo_ss-toughened Mo₂Ni₃Si alloy.     

Ti2Ni3Si/NiTi金属间化合物合金在H2SO4溶液中的腐蚀行为

利用激光熔炼材料制备技术,制得了由三元金属硅化物Ti2Ni3Si初生枝晶和枝晶间Ti2Ni3Si/Ti共晶组成的金属间化合物耐磨耐蚀合金;采用极化曲线、塔菲尔图(Tafel Plot)和交流阻抗(EIS)等技术,研究了合金在1 mol/L H2SO4溶液中的电化学腐蚀行为以及Ti含量对合金组织与耐蚀性的影响.结果表明:由于表面形成的稳定钝化膜及Ti2Ni3Si和NiTi的高化学稳定性,使合金在1 mol/L H2SO4溶液中具有优异的耐蚀性,且随着Ti含量的升高,合金的耐蚀性略有提高.     

Wear properties of nonhydrogenated,hydrogenated,and dehydrogenated Ti6A14V alloy

Wear properties of the nonhydrogenated,hydrogenated 0.5 wt% and dehydrogenated Ti6 A14 V alloys were studied through dry sliding wear tests using an M-200 type pin-on-disk wear testing machine in ambient air at room temperature to reveal the effects of hydrogen on wear properties of Ti6 A14 V alloy. Morphology and chemical element of worn surface were investigated by means of scanning electron microscope(SEM) and energy dispersive spectroscopy(EDS). Results show that hydrogen decreases the wear resistance of Ti6 A14 V alloy. Wear rate of the Ti6 A14 V alloy increases after hydrogenation. Wear rate increases by 244.3 % when 0.5 wt% hydrogen is introduced into a Ti6 A14 V alloy. Wear rate of the dehydrogenated Ti6 A14 V alloy recovers. Wear mechanisms of the nonhydrogenated, hydrogenated, and dehydrogenated Ti6 A14 V alloys are determined. The nonhydrogenated Ti6 A14 V alloy is controlled by oxidative wear. The hydrogenated Ti6 A14 V alloy is dominated by abrasive wear. Wear mechanism of the dehydrogenated Ti6 A14 V alloys is a mixture of oxidative wear and abrasive wear.