Al6061/TA2异种金属冷金属过渡焊接性分析

以AlSi₅ 焊丝对6061铝合金和TA2纯钛进行CMT熔钎焊,采用SEM,EDS分析焊接接头的微观组织特征,并通过拉伸试验对接头进行力学性能评定.结果表明,焊接过程稳定,焊缝成形美观.所得到的焊接接头具有熔焊和钎焊两部分,其中局部熔化的铝母材与熔融的焊丝混合后形成焊缝,焊缝金属与微熔的钛母材形成三个钎焊界面.钎焊界面主要成分为TiAl₃金属间化合物,其厚度较薄.此外,界面附近还有一些随机分布的棒状的TiAl₃金属间化合物.焊接过程中,随着焊丝偏移量的增加,焊缝力学性能提高.参数优化后的接头抗拉强度较高,且断裂在铝热影响区.     

La2O3含量对Al2O3/Cu基复合材料组织与性能的影响

以La₂O₃粉、Al粉、CuO粉为反应物原料、纯铜为基体,采用原位合成技术和近熔点铸造法制备颗粒增强Cu基复合材料,研究La₂O₃对Al-CuO体系制备的Cu基复合材料组织及性能的影响。结果表明：添加La₂O₃可获得纳米Al₂O₃颗粒,且弥散分布于Cu基体中,制备的材料组织更加细小、均匀,其材料的电导率及摩擦磨损性能明显提高。当添加0.6%wtLa₂O₃,复合材料的电导率达到90.2%IACS,磨损量达到最小,相比未添加La₂O₃,其导电率提高10.1%,磨损量减小36.6%。     

La2O3含量对搅拌摩擦加工制备Ni /Al复合材料组织和性能的影响

采用搅拌摩擦加工方法在Al基体中添加不同La₂O₃含量的混合粉末(Ni+La₂O₃),制备 (Ni+La₂O₃)/Al复合材料。采用SEM、EDS、 EPMA及XRD对复合区微观结构及相组成进行分析,采用室温拉伸试验对 (Ni+La₂O₃)/Al复合材料力学性能进行了测试。结果表明,随着La₂O₃含量的增加,(Ni+La₂O₃)/Al复合材料的组织和性能先变好后变差。当La₂O₃添加量达到5%时,复合材料中Al₃Ni增强颗粒分布均匀、颗粒数量最多,块状的Ni粉团聚减少,其抗拉强度达到最大值215MPa,相比Ni/Al复合材料(抗拉强度176MPa),其抗拉强度提高了22%;当La₂O₃的添加量为7%时,复合材料中Al₃Ni增强颗粒含量减少,块状Ni粉团聚重新出现,抗拉强度下降至201MPa。     

Ti活度对Al2O3/AgCuTi/Fe-Ni-Co钎焊接头机械性能和微观组织结构的影响

采用AgCuTi钎料实现了Al₂O₃陶瓷与Fe-Co-Ni合金的钎焊连接,并调查了不同钛含量的钎料对Al₂O₃/AgCuTi/Fe-Ni-Co钎焊接头机械性能和微观组织结构的影响。扫描电子显微镜(SEM), X射线能量色散光谱仪(EDS), X射线衍射仪(XRD)及电子万能试验机用于分析钎焊接头的机械性能和微观组织结构,结果表明:钛含量的增加明显提高AgCuTi钎料与Al₂O₃陶瓷的相互作用,在Al₂O₃/Ag-Cu-Ti界面生成一层由Ti-Al 和 Ti-O化合物组成的反应层。Al₂O₃/AgCuTi/Fe-Ni-Co钎焊接头的抗拉强度随钛含量的增加而增加,当钛含量提高到8wt.%时,抗拉强度达到最大值78Mpa。通过微观组织结构分析发现,采用AgCu4Ti在890℃保温5min的条件下可以获得较好的钎焊接头,典型接头的微观组织结构为Al₂O₃/TiAl+Ti₃O₅/NiTi+Cu₃Ti+Ag(s,s)/Ag(s,s)+Cu(s,s)+(Cu,Ni)/Fe-Ni-Co。采用AgCu8Ti获得的钎焊接头的界面反应层与AgCu4Ti差异不大,但反应层稍微增厚,并伴有TiO和Ti3Al在Al₂O₃/Ag-Cu-Ti界面生成。     

La2O3掺杂氧化铝气凝胶的制备与耐温性能研究

以仲丁醇铝为前驱体,采用溶胶-凝胶法结合丙酮-苯胺原位生成水技术,通过乙醇超临界干燥,制备出不同含量(1.5 mol%~12 mol%)La₂O₃掺杂的氧化铝气凝胶。采用电子扫描电镜(SEM)、透射电子显微镜(TEM)、X线衍射仪(XRD)、N₂吸附分析仪等仪器表征了La₂O₃掺杂对氧化铝气凝胶的微结构和耐温性能的影响。结果表明：La₂O₃的引入使氧化铝气凝胶的形貌由球状颗粒向大的片状结构转变。适量的La₂O₃掺杂能提高氧化铝气凝胶的比表面积,9 mol% La₂O₃掺杂的氧化铝气凝胶比表面积最大。通过La₂O₃掺杂,能够抑制氧化铝晶粒在高温下的生长和α-Al₂O₃的相变,提高氧化铝气凝胶的耐温性能。1200℃热处理后,La₂O₃掺杂的氧化铝气凝胶仍维持在θ-Al₂O₃,比表面积为86.5 m₂/g,高于未掺杂的氧化铝气凝胶(46 m₂/g)。     

基于Ti中间层的SiCp/6061-T6Al MMCs低功率激光-TIG复合焊组织与性能

以0.1mm厚的Ti箔做中间夹层,使用低功率激光-TIG复合焊的方式对SiCp/6061-T6Al MMCs 进行焊接,并对接头的宏观形貌、显微组织、物相、电阻率、抗拉强度及断口形貌进行分析。结果表明：激光功率对焊缝的成形有着较大影响;Ti箔的加入基本抑制了焊缝中针状Al₄C₃生成,并生成TiC增强相以及条状TiAl₃;焊缝区为等轴晶组织,熔合区为柱状晶组织,热影响区组织变化不明显;随着激光功率的增加接头的电阻率呈现出增加的趋势,并明显高于母材;在554W时接头的抗拉强度可达196.98MPa,是母材强度的54.71%。接头断口中几乎没有气孔,韧窝中的第二相粒子以TiC为主,接头呈现出以脆性断裂为主的脆-韧性混合断裂特征。     

原位颗粒对近液相线铸造6063铝合金微观组织和耐磨性的影响机理

以CuO-Al作为反应体系,在6063铝合金中原位反应生成Al₂O₃颗粒,采用近液线相铸造的方法制备6063Al-XAl₂O₃(X=0,2,4,6)复合材料。研究原位反应颗粒Al₂O₃与6063铝合金自带的原位结晶颗粒Mg₂Si的形状、尺寸、数量、分布、界面特征等对合金微观组织和耐磨性的影响机理。结果表明,在6063铝合金中原位反应生成尺寸在亚微米级的近球形θ-Al₂O₃颗粒;其(311)晶面与6063铝合金基体(111)晶面成共格界面;6063铝合金中Mg₂Si尺寸大约为100nm,呈条带状,其(02-2)与Al基体(111)晶面属于共格界面。随着Al₂O₃颗粒含量的增加,6063铝基复合材料的晶粒组织形貌由蔷薇状逐渐向等轴晶转变,晶粒尺寸逐渐减小。当Al₂O₃的质量分数为6%时,复合材料组织由等轴晶和细小的柱状晶组成。载荷为50N时,6063铝合金的磨损量为6.72mg,6063-6Al₂O₃复合材料的磨损量为1.63mg,相对于6063铝合金降低75.7%。原位颗粒(Al₂O₃+Mg₂Si)与铝基体都成共格界面,界面之间无污染,界面结合强度高,在磨损过程中,不易从基体中脱落,承当磨损过程中的大部分载荷。原位生成高硬度的Al₂O₃颗粒与原位结晶颗粒Mg₂Si协同作用共同提高复合材料的耐磨性。外加载荷为40N时,随着增强相质量分数的增加,复合材料的磨损机制由粘着磨损转变为磨粒磨损。6063铝合金磨损机制以严重的粘着磨损为主。6063-2Al₂O₃复合材料磨损机制主要以粘着磨损为主,6063-4 Al₂O₃和6063-6Al₂O₃复合材料主要表现为磨粒磨损。     

脉冲宽度对超薄TiNi/不锈钢激光焊接头TiNi侧界面的影响

添加Ni做为填充材料是抑制TiNi/不锈钢异种材料激光焊接头裂纹从而实现其良好连接的方法之一,但填充金属Ni与母材TiNi合金的成分差异会形成界面区,焊接热输入对界面区的组织形貌有很大的影响,进而会影响整个接头的力学行为。本文在厚度为0.2mm的TiNi合金/321不锈钢异种材料激光微焊接时,预置Ni做为填充材料,获得了TiNi合金/Ni/321不锈钢激光焊接头,研究了激光脉冲宽度对焊接接头TiNi侧界面的影响。结果表明,不同脉冲宽度下,TiNi合金侧界面区均由宽度不等的TiNi共晶层和TiNi₃金属间化合物层组成;随着脉冲宽度的增加,TiNi共晶层平均宽度逐渐减小,TiNi₃金属间化合物层平均宽度逐渐增加;界面区显微硬度随脉冲宽度的增加逐渐升高。TiNi母材熔化量和Marangoni流动的改变是影响接头该侧界面区宽度及显微硬度的主要原因。     

在线去应力退火对线性摩擦焊TiAl合金接头微结构与力学性能的影响机制

采用在线去应力退火工艺对线性摩擦焊TiAl合金接头进行处理,避免了焊后裂纹的产生。显微组织分析表明,接头焊缝区与热力影响区界限明显,焊缝区主要由等轴γ晶组成,并含有少量的α₂相。靠近焊缝的热影响区内的层状γ晶具有明显的流线特征,其方向与焊接界面热塑性金属的流动方向一致。接头的显微硬度从母材区到焊缝区呈逐渐增加的趋势,焊缝区显微硬度相较于母材区增加了约1700 MPa;接头的室温抗拉强度与母材相当,在683 MPa到717 MPa之间。焊缝区的细晶强化效应是接头强度较高的主要原因。     

酸刻蚀处理对IrO2-Ta2O5/Ti阳极寿命的影响

通过改变腐蚀方法,研究了使用H₂C₂O₄和H₂SO₄进行钛基体表面刻蚀对金属氧化物钛阳极电化学性能和表面形貌的影响。采用扫描电子显微镜、X射线衍射仪和光电子能谱等测试方法对样品进行了结构分析。然后利用电化学工作站测试了样品的电催化活性,利用加速寿命测试研究了样品的电化学稳定性。结果表明,通过H₂C₂O₄和H₂SO₄分步腐蚀可以获得更加均匀致密的表面形貌和更好的催化稳定性。在此基础上,进一步研究了预处理对钛阳极寿命的影响原因。IrO₂-Ta₂O₅/Ti阳极的催化活性和稳定性与酸刻蚀处理的先后顺序及表面结构密切相关,并建立了预处理方法与阳极性能之间的关系。分步腐蚀使钛表面具有合适的粗糙度,因而提升了涂层附着力。在热分解过程中,经分步腐蚀形成的氢化钛在不改变表面形貌的情况下转变为金红石结构的氧化钛,有利于电子输运,从而增强涂层附着力并延长加速寿命。     

原位合成TiC和TiB增强钛基复合材料的微观结构与力学性能

利用钛与Ｂ４Ｃ之间的自蔓延高温合成反应经普通的熔钐工艺原位合成制备了ＴｉＣ、ＴｉＢ增强的钛基复合材料。光学金相、ＥＰＭＡ、ＴＥＭ和Ｘ射线衍射的研究结果表明：存在匠两种不同形状的增强体,即短纤维状ＴｉＢ晶须和等轴、近似等轴状ＴｉＣ粒子。ＴｉＢ、Ｔｉ基体界面洁净,没有明显的界面反应,而ＴｉＣ、Ｔｉ基体界面有非化学配比的ＴｉＣ过度层存在。由于增强体承受载荷,基体合金晶粒细化以及高密度位错的存在,制备钛基     

Improving the strength of brazed joints with in situ synthesized TiB whiskers

TiB whiskers have been in situ synthesized as reinforcements in 73Cu-27Ti (wt.%) active brazing filler alloy used for the joining of Al₂O₃ and Ti-6Al-4V alloy. The results show that TiB whiskers served as an effective reinforcement phase aid to decrease the residual stress and increase the shear strength of joints. The shear strength of the joint, containing 30 vol.% TiB whiskers was about 239% higher than that of the joint brazed without TiB whiskers.     

Microstructure and mechanical properties of (TiB+La2O3)/Ti composites heat treated at different temperatures

Near-α titanium matrix composites reinforced with TiB and La₂O₃ were synthesized by common casting and hot-working technology. The effects of β heat treatment temperature on the microstructure and the tensile properties of the in situ synthesized (TiB+La₂O₃)/Ti were studied. Microstructure was studied by OM and TEM, and tensile tests were carried out at room temperature and 923 K, respectively. Results show that with the increase of β heat treatment temperature, prior β phase grain size increases and α colony size decreases. Room temperature tensile strength increases with the increase of β heat treatment temperature, which can be attributed to the decrease of α colony size with the increase of β heat treatment temperature. However, high-temperature tensile strength decreases with the increase of β heat treatment temperature and the decrease of the high-temperature tensile strength is due to the increase of the prior β phase grain size.     

原位合成多元增强钛基复合材料(TiB+TiC+Y2O3)/Ti

利用钛与B2O3、B4C和稀土钇之间的化学反应,采用真空非自耗电弧炉熔炼工艺,原位合成多元、多尺度、不同形状增强体增强的钛基复合材料--(TiB TiC Y2O3)/Ti.利用热力学机理分析了制备该种材料的可行性,通过X射线衍射仪、光学显微镜、扫描电镜、电子探针和透射电镜分析了复合材料的物相组成、增强体的微观形貌和材料的显微组织.结果表明:复合材料的增强体为TiB、TiC和Y2O3;生成的增强体分布均匀;复合材料的晶粒非常细小;TiB为针状;TiC为等轴状和近似等轴状;Y2O3的形貌随着稀土Y含量的增加从近似等轴状粗化生长为树枝状;材料中存在较多纳米级的球状增强体;增强体TiB、TiC、Y2O3和钛基体界面干净,没有界面反应物存在.     

原位合成TiB/Ti基复合材料增强体的生长机制

利用Ｔｉ与Ｂ之间的自蔓延高温合成反应,经非自耗电弧熔炼工艺制备了ＴｉＢ增强的钛基复合材料,借助Ｘ射线衍射（ＸＲＤ）,扫描电镜和透射电镜分析了复合材料的物相和增强体的形态,结果表明：只存在ＴｉＢ增强体和α－Ｔｉ。原位合成增强体ＴｉＢ的形貌与其Ｂ２７晶体结构密切相关,ＴｉＢ增强体容易沿（０１０）方向生长而生成柱状短纤维,其柱面由（１００）,（１０１）和（１０１）组成。     

Thermal stability of in situ synthesized high temperature titanium matrix composites

TiB and La₂O₃ reinforced high temperature titanium matrix composites are in situ synthesized by common casting technology. Microstructure of the matrix alloys and composites before and after thermal exposure are characterized, tensile properties of the specimens are tested. Both the strength and ductility of the composites are enhanced by the reinforcements. Titanium matrix composites show better thermal stability than the matrix alloys because of the reduction of oxygen and microstructure refinement without Ti₃Al agglomeration.     

Densification and compressive strength ofin-situ processed Ti/TiB composites by powder metallurgy

In the present study, the densification of Ti/TiB composites, the growth behavior ofin-situ formed TiB reinforcement, the effects of processing variables — such as reactant powder (TiB₂, B₄C), sintering temperature and time — on the microstructures and the mechanical properties ofin-situ processed Ti/TiB composites have been investigated. Mixtures of TiB₂ or B₄C powder with pure titanium powder were compacted and presintered at 700°C for 1 hr followed by sintering at 900, 1000, 1100, 1200, and 1300°C, respectively, for 3hrs. Some specimens were sintered at 1000°C for various times in order to study the formation behavior of TiB reinforcementin-situ formed within the pure Ti matrix. TiB reinforcements were formed through different mechanisms, such as the formation of fine TiB and the formation of coarse TiB by Ostwald ripening or the coalescence of fine TiB. There was no crystallographic relationship between TiB reinforcement and the matrix. There were voids at the interface between the TiB reinforcement and the Ti matrix due to the preferential growth of coarse TiB without a particular crystallographic relationship with pure Ti matrix and the surface energy between the Ti matrix and TiB reinforcements. Therefore, the densification of Ti/TiB₂ compacts was hindered by the preferential growth of coarse TiB reinforcements. The mechanical properties ofin-situ processed composites were evaluated by measuring the compressive yield strength at ambient and high temperatures. The compressive yield strength of thein situ processed composites was higher than that of the Ti-6A1-4V alloy. It was also found that the compressive yield strength of the composite made from TiB₂ reactant powder was higher than that of the composite made from B₄C at the same volume fraction of reinforcement. A crack path examination suggested that the bonding nature of interface between matrix and reinforcement made from TiB₂ reactant powder was better than that made from B₄C.     

Microstructure evolution during preparation of in-situ TiB reinforced titanium matrix composites

1　INTRODUCTIONTitaniummatrixcompositesarepromisingmate rialswhichcanbeusedextensivelyinaerospaceandautomotiveindustriesbecauseoftheirexcellentme chanicalpropertiesatroomtemperatureandelevatedtemperature[14 ] ,suchaslowdensity ,highstrength ,andcorrosion resistance .Amongthein situfabrica tionmethodsoftitaniummatrixcomposites[511] ,self propagatinghigh temperaturesynthesis (SHS )methodhasuniqueadvantage ,thatis ,thereinforce mentsarefineanddispersed .InSHS ,thereisanexothermicreactionac…     

Nanoscale TiB precipitates in laser deposited Ti-matrix composites

Metal-matrix composites based on boride reinforcements in a titanium base matrix have been deposited in situ from a powder feedstock consisting of a blend of Ti-alloy and elemental boron powders using the laser engineered net-shaping (LENS™) process. These composites exhibit a homogeneous multi-scale microstructure consisting of micron to sub-micron as well as nanometer scale TiB precipitates in a metal matrix. While the coarser precipitates result from rapid solidification of the liquid, the nanometer-scale precipitates are likely to form from the solid-state decomposition of a boron supersaturated Ti-base matrix. Such nanometer-scale TiB precipitates can play a prominent role in determining the mechanical properties of these composites.     

Mechanical properties of Ti-6Al-4V/TiB composites with randomly oriented and aligned TiB reinforcements

In situ Ti-6Al-4V/TiB discontinuously reinforced composites, containing 20 and 40% of TiB whiskers by volume, were produced by blending Ti, Al/V, and TiB₂ powders. The consolidated powder blends were annealed to transform the TiB₂ particles to TiB. The microstructural evolution of the composite was studied as a function of heat treatment duration at 1100, 1200, 1300 and 1400 °C. The mechanical properties of Ti-6Al-4V/TiB composites were established in tension and compression at room temperature and 300 °C, and by resonant ultrasound spectroscopy (RUS), for the two volume fractions of TiB, and for randomly oriented and aligned arrays of TiB whiskers. The average Young’s modulus of the composite with 20% of randomly oriented TiB whiskers was 153 GPa, compared to 109 GPa for unreinforced Ti-6Al-4V. The average Young’s modulus of composites with 20 and 40% of aligned TiB whiskers was measured along the extrusion axis as 169 and 205 GPa, respectively. The stiffness of TiB whiskers was determined from bulk measurements with the Halpin-Tsai equation to be 482 GPa. Yield and ultimate strengths near 1200 MPa were measured. The strength and ductility of the materials were limited in the present study by non-optimal matrix microstructure and inadequate particulate distribution, and approaches for properties improvements are provided.