Ti6Al4V合金显微组织对超声声速的影响

通过对Ti6Al4V合金棒材在β相区、α+β两相区热处理后的显微组织观察和纵向超声声速值测量、分析,研究了合金显微组织对超声声速的影响。结果表明,Ti6Al4V合金在相变点以上加热,随着冷速的降低,次生α析出长大为粗大片层状,声速值也随之提高;在相变点以下加热,组织中的初生α相含量对超声声速值的影响不明显,次生相的形貌对超声波声速起决定作用,其中规则片层次生α 相的析出有利于超声声速值的提高。     

Ti6Al4V合金激光熔覆Ni基自润滑涂层的组织和性能

利用光纤激光器在Ti6Al4V合金基体表面制备了Ni25为基体和Ni包MoS2为润滑剂的Ni基自润滑涂层,通过FESEM、XRD、硬度测试仪和摩擦磨损试验机研究了熔覆层的显微组织、物相组成和摩擦性能.结果表明,熔覆层表面主要以花瓣状组织以及少量的树枝晶组成,界面处的组织主要是以树枝晶为主,还有少量的等轴晶粒.熔覆层...     

铝含量对高铬合金堆焊层组织与性能的影响

采用焊丝和合金粉块氮气保护明弧堆焊方法制备了不同Al含量的Fe-Cr-C-Al合金堆焊层,利用扫描电镜、能谱仪、洛氏硬度计等分析不同Al含量堆焊层的组织和性能。结果表明,堆焊层焊态组织主要由马氏体、奥氏体和M7C3型碳化物组成,铝含量为2.11%和3.06%的堆焊层中有Al2O3硬质相的存在;随着Al含量的增加,Fe-Cr-C-Al堆焊层的洛氏硬度逐渐增加而磨损量呈依次递减趋势,含3.06%Al堆焊层耐磨性是基体耐磨性的4.2倍,堆焊层硬度值达到45 HRC,磨损量最小。     

真空热处理对Ti6Al4V基体/NiCrAlY涂层体系组织结构及元素扩散行为的影响

采用电弧离子镀(AIP)技术在Ti6Al4V基体表面沉积制备了NiCrAlY涂层. 通过金相观察(OM)、扫描电镜(SEM)与能谱(EDS)分析、 X射线衍射(XRD)分析以及显微硬度测试, 研究了真空热处理对NiCrAlY涂层组织性能的影响, 讨论了Ti6Al4V基体/NiCrAlY涂层界面元素扩散规律. 结果表明: 700.℃真空热处理后, NiCrAlY涂层中开始析出γ′-Ni3Al相, 这提高了涂层的表面硬度; 在700.℃温度下, Ti6Al4V基体/NiCrAlY涂层界面由外至内出现Ni3(Al,Ti)、 TiNi和Ti2Ni中间化合物层, 并随着温度提高, 界面处中间化合物层增厚; 700.℃时, 主要发生了镍、钛元素的扩散, 铬元素在870.℃开始发生扩散. 当温度提高到950.℃后, 由于镍元素大量向Ti6Al4V基体扩散引起涂层的退化失效.     

Fe含量对Ti-6Al-4V钛合金力学性能的影响

研究不同Fe含量(0.04wt％ ～0.26wt％)对Ti-6Al-4V钛合金力学性能的影响.结果表明,随Fe含量增加,Ti-6Al-4V钛合金室温抗拉强度、屈服强度、硬度及弹性模量增加,塑性无明显变化.进一步分析发现,Fe含量与屈强比σ0.2/σb呈线性关系,铁含量0.26wt％时屈强比σ0.2/σb高达0.97.高Fe含量时Ti-6Al-4V钛合金塑性变形是滑移为主、孪生为辅的复合变形机制.     

Ti6Al4V合金表面热浸镀Ti-Al镀层相组成

采用热浸镀方法在Ti6Al4V合金表面制备Ti-Al镀层,并在1100 ℃高温下进行热扩散处理。结果表明,TC4合金热浸镀铝后在1100 ℃保温,形成了表面氧化层、过渡层及基体,表面氧化层和过渡层厚度随扩散时间延长而增加,表面氧化层主要由Al₂O₃和TiO₂构成,过渡层主要相为TiAl₃、Ti₂Al₅和Ti₁₉Al₆金属间化合物。     

退火工艺对激光选区熔化成形Ti6Al4V合金组织及室温力学性能的影响

以Ti6Al4V球形粉末为原料,利用激光选区熔化成形方法制备了Ti6Al4V合金试样,采用光学显微镜、扫描电镜及力学性能测试等手段,研究了退火工艺对Ti6Al4V合金室温力学性能及组织的影响规律。结果表明: SLM成形沉积态Ti6Al4V合金室温抗拉强度超过1200 MPa,而平均断后伸长率仅为4.0%;在650 ℃下进行真空退火处理,合金的抗拉强度仍保持在1200 MPa左右,规定塑性延伸强度R_p0.2高于1150 MPa,但试样的断后伸长率<10%;而在750及800 ℃下进行真空退火处理,合金试样的抗拉强度降至1100 MPa左右,规定塑性延伸强度高于1050 MPa,伸长率达到甚至超过10%,材料的综合强韧性得到明显提升。随着真空退火加热温度和保温时间的增加,SLM成形Ti6Al4V合金原始β晶界逐渐变模糊,晶粒趋向于等轴化。与此同时,快速冷却转变的α′针状马氏体未出现明显地粗化。     

Surface characterization of plasma sprayed pure and reinforced hydroxyapatite coating on Ti6Al4V alloy

Hydroxyapatite coatings suffer from poor mechanical properties like fretting fatigue, toughness and abrasive wear resistance. These properties can be enhanced by incorporation of secondary ceramic and metallic reinforcements in HA. An attempt has been made to deposit HA and HA reinforced with 10 wt.% (80Al₂O₃-20TiO₂) by plasma spray process on Ti6Al4V substrate. These coatings have been characterized using SEM/EDAX, XRD and FTIR spectroscopy. Corrosion studies have been done in SBF solution. Bio compatibility study is not included in this work. Reinforcement has enhanced the tensile strength. There is marginal improvement in microhardness and surface roughness with reinforcement. Both pure and reinforced coatings show superior resistance against corrosion in simulated body fluid.     

Ti6Al4V合金表面离子注入N+C,Ti+N和Ti+C性能研究

采用等离子体基离子注入的方法在Ti6Al4V合金表面分别注入N+C、Ti+N和Ti+C元素,注入剂量均为2×1017 ions/cm2,N+C和Ti+N元素的注入负脉冲偏压为-50 kV,Ti+C元素的注入电压分别为-20 kV、-35 kV和-50 kV。通过X射线光电子能谱仪（XPS）和X射线衍射仪（XRD）对注入层进行了微观结构分析,结果表明：Ti+C注入层中存在TiC和Ti-O,Ti+N注入层中存在TiN和Ti-O键。采用纳米压痕仪和球盘磨损试验机对注入层的硬度和摩擦学性能进行了研究。结果表明：在相同注入电压下,Ti+C注入层的硬度最高,其次是Ti+N注入层,N+C注入层的硬度最低;Ti+C 注入层的硬度随着注入电压的增大而增大,最大硬度为11.2GPa。50kV注入层Ti+C具有最低的比磨损率,其值为6.7×10-5mm3/N.m,比磨损率较未处理Ti6Al4V基体下降了1 个数量级以上,表现出优异的耐磨损性能。     

氟化物ATIG焊接Ti6Al4V的焊缝成形和组织

试验选用MF型氟盐(LiF,NaF,KF)、MF2型氟盐(MgF2,CaF2,BaF2)和KN型钾盐(KF,KCl,KBr)对Ti6Al4V进行ATIG焊接,焊后研究了焊缝的成形、熔深和组织.结果表明,除MgF2焊道成形稍有曲折外,其它活性剂ATIG焊接接头均成形良好、无缺陷;氟化物能起到阻止熔池金属氧化的作用;KF和MF2型氟盐可显著减小焊缝熔宽;同阳离子的氟化物相比其氯化物和溴化物可显著增加Ti6Al4V焊缝熔深;MF型氟盐中KF活性剂获得的焊缝熔深最大,MF2型氟盐中MgF2活性剂获得的焊缝熔深最大,且熔深MgF2>KF;TIG和ATIG的焊缝组织均为粗大的柱状晶,活性剂ATIG焊可细化焊缝晶粒尺寸,但不会对焊缝的相结构组成造成影响.     

Improving tribological properties of Ti6Al4V alloy with duplex surface treatment

Ti-doped diamond like carbon films were deposited on both untreated and plasma nitrided Ti6Al4V alloy using Closed Field Unbalanced Magnetron Sputtering (CFUMBS) method and their tribological properties were evaluated by conducting sliding wear conditions. The influence of the nitrided layer on tribological behavior of Ti-DLC films was studied by means of XRD, SEM, scratch tester, microhardness tester and pin-on-disc tribotester. The microhardness results pointed out that the duplex treatment dramatically increased the surface hardness and reduced the plastic deformation of the alloy. Wear tests showed that Ti-DLC coatings on both untreated and nitrided surfaces caused a reduction in the coefficient of friction. The reason of the reduction in the coefficient of friction was found to be the formation of transfer film between the sliding surfaces. Wear rates demonstrated that wear resistance of duplex treated (Ti-DLC coating after nitriding) Ti6Al4V alloy was significantly improved.     

Effect of Zr addition on microstructures and mechanical properties of Ni-46Ti-4Al alloy

The microstructures and mechanical properties of Ni-(46-x)Ti-4Al-xZr (x = 0-8, at.%) alloys have been investigated by scanning electron microscopy (SEM), transmission electron microscopy (TEM), and mechanical tests. The results show that the Ni-Ti-Al-Zr alloys are composed of TiNi and (Ti, Al) 2 Ni with Zr as a solid solution element in both phases, and the third phase, (Zr, Ti, Al) 2 Ni, appears in Ni-40Ti-4Al-6Zr and Ni-38Ti-4Al-8Zr alloys. The compressive yield strength at room temperature increases with the increase of Zr content due to the solid-solution strengthening of Zr and precipitation strengthening of (Ti, Al, Zr) 2 Ni phase. However, the Ni-42Ti-4Al-4Zr alloy exhibits the maximum compressive yield strength at 873 and 973 K because of the softening of (Zr, Ti, Al) 2 Ni phase in the alloys with more Zr addition. The tensile stress-strain tests and the SEM fracture surface observations show that the brittle to ductile transition temperature of Ni-42Ti-4Al-4Zr alloy is between 873 and 923 K.     

Ti6Al4V合金吸氢行为研究

研究了Ti6Al4V合金在不同置氢温度、保温时间和氢压下的吸氢行为,利用光学显微镜研究了氢在钛合金中的分布规律。研究结果表明,Ti6Al4V合金的氢含量是由置氢温度、保温时间和氢压来控制的。随着置氢温度的升高,氢含量先增加后降低。随着氢压的增加,氢含量直线增加。钛合金的吸氢过程实质上是氢的扩散过程,随着保温时间的增加,合金中的氢分布逐渐趋于一致。     

Microstructure and mechanical properties of Ti6Al4V alloy prepared by selective laser melting combined with precision forging

To improve the mechanical properties of Ti6Al4V alloy prepared by selective laser melting (SLM) process, the precision forging was conducted at 950 °C and different strains and strain rates. The microstructure evolution of as-built samples and forged samples in both horizontal and vertical sections was visualized and analyzed by optical microscope and X-ray diffraction. The microstructure was improved by the precision forging and subsequent water quenching. The porosity in each section was accounted. It can be seen that high strain rate and large deformation result in low porosity, consequently contributing to a better fatigue performance. The micro-hardness was lowered after precision forging and water quenching, while the difference of microhardness between the horizontal and vertical sections became smaller, which illustrated that this process can improve the anisotropy of structural components fabricated by SLM.     

缺陷对选区激光熔化Ti6Al4V合金高周疲劳性能的影响

明确缺陷对选区激光熔化Ti6A14V合金的疲劳性能影响规律是突破该材料工程应用瓶颈的关键问题.在缺陷无法避免的工艺背景下,借助于金相显微镜、电子背散射衍射技术、X射线三维成像系统、疲劳试验机、扫描电子显微镜及激光共聚焦显微镜,对该材料的组织和缺陷表征,研究了高周疲劳性能及失效机制.结果 表明,该合金的微观组织表现出增材...     

Influence of hydrogenation on microstructures and microhardness of Ti6A14V alloy

The microstructures of Ti6A14V alloy after hydrogenation were investigated by optical microscopy（OM）, X-ray diffraction（XRD） and transmission electron microscopy（TEM）. The influence of hydrogenation on the hardness of α and β phases was analysed by microhardness testing. The influence of hydrogenation on alloying elements diffusion was studied by electron probe microanalysis（EPMA）. The microstructural observation reveals that hydride δ （FCC structure） as well as large number of dislocations precipitate in the specimens with 0.278% and 0.514% hydrogen, and a lot of twins are found in the specimen with 0.514% hydrogen, simultaneously. The result of microhardness testing shows that the hardness of a and β phases increases synchronously with the increase of hydrogen and the hardness increment of β is larger than that of a. According to analysis of EPMA, the diffusion ability of alloy elements Al and V increases after hydrogenation. It is considered that hydrogen solution strengthening and V element diffusion are the main factors causing the hardness of a phase increase with the increase of hydrogen, and the formation of δ hydrides, lattice defects, hydrogen solution strengthening and Al element diffusion jointly cause the hardness of β phase increase with the increasing hydrogen.     

热处理工艺对Al0.5CoCrCuFeNi高熵合金显微组织与硬度的影响

采用水冷铜坩埚真空感应悬浮熔炼制备了多组元高熵合金Al_0.5CoCrCuFeNi,研究了不同热处理工艺对合金的显微组织和硬度的影响规律。结果表明,Al_0.5CoCrCuFeNi高熵合金相结构简单,在铸态下由两种不同成分的FCC相组成,枝晶处为贫Cu的FCC1相,枝晶间为富Cu的FCC2相,显微组织为树枝晶形貌,存在一定的枝晶偏析。合金制备态的硬度为255 HV0.5。合金具有良好的热稳定性,随着热处理温度的升高,合金的相结构和硬度均无太大的变化。冷却方式对合金的显微组织和相结构影响不大,但炉冷后合金的硬度比空冷和水冷时高。     

Ti6Al4V钛合金表面真空渗氧处理

目的在Ti6Al4V钛合金表层制备硬度高、耐磨性好的硬化层。方法结合真空技术,以高纯的O2为介质,在Ti6Al4V钛合金表面制备致密的渗氧硬化层,采用X衍射仪分析渗氧层的相组成,用金相显微镜观察渗氧层和磨痕组织,用显微硬度计测试渗氧层的显微硬度,用MM-U10A端面磨损试验机研究渗氧层的耐磨性。结果渗氧层物相主要由TiO_2、TiO、Ti_3Al及Al_2O_3组成,温度较低时,形成的渗氧层较薄,温度增加,渗氧层厚度迅速增加,硬度及耐磨性也随之增加。温度为760℃时,表面硬度为基体硬度的2.5倍以上,大于750HV,有效硬化层厚度达60μm以上,其磨损失重仅为未渗氧原样的1/4,表面磨痕细密,没有撕裂情况发生,渗氧层保持完整。温度继续增加,氧化物开始聚集长大,渗氧层组织开始变得疏松,硬度及耐磨性开始下降。结论 Ti6Al4V钛合金表面真空渗氧处理可显著提高其表面硬度,耐磨性改善明显。     

Effects of Sc, Zr and Ti on the microstructure and properties of Al alloys with high Mg content

The effects of trace Sc, Zr, and Ti on the microstructure and hardness of Al alloys with high Mg content (Al-6Mg, Al-8Mg, and Al-10Mg) were studied by optical microscope, scanning electron microscopy (SEM), transmission electron microscopy (TEM), and Brinell hardness. The grain size of the as-cast alloys was refined by the addition of Sc and Zr, and it was further refined by the addition of Ti. With the same contents of Sc, Zr, and Ti, an increase in Mg content was beneficial to the refinement due to the solution of Mg into α-Al. The refined micro-structures of the as-cast alloys were favorable for Brineil hardness. Addition of Sc, Zr, and Ti to the Al-10Mg alloy results in the improve-ment of peak hardness and it is about 45% higher than that of the Al-10Mg alloy, which is due to fine precipitations of Al_3(Sc_(1-x)Zr_x), Al_3(Sc_(1-x)Ti_x), and Al_3(Sc_(1-x-y)Zr_xTi_y).     

超音速激光沉积Ti6Al4V涂层的微观结构及耐蚀性能

超音速激光沉积技术是将激光加热与冷喷涂同步耦合的一种新型材料沉积技术。文中利用超音速激光沉积技术在中碳钢基体上制备Ti6Al4V涂层,并采用SEM、XRD、电化学腐蚀测试等手段对涂层厚度、显微组织、相成分以及耐蚀性能进行了表征分析。结果表明,在一定的激光辐照温度（即沉积区温度）范围内,涂层沉积效率、致密性以及涂层与基体之间的结合强度均随激光辐照温度的升高而增加,当激光辐照温度为800℃时,沉积效率是冷喷涂的4倍,涂层中的孔隙率仅为4.38%,涂层与基体的结合强度达75 MPa。由于低热输入的原因,涂层的物相组成与原始钛合金粉末基本一致。随着激光辐照温度的进一步提高,涂层中有TiN相的产生,不利于粉末的沉积,涂层的沉积效率、致密性以及结合强度均下降,但是在酸性腐蚀介质中,TiN的存在提高了涂层的耐蚀性能。