Ti3Al—Nb合金的组织结构分析

用透射电子显微术和X射线能谱术分析了Ti_3Al-Nb合金在不同热处理状态下的组织结构。结果表明。添加铌使Ti_3A1基合金的铸态组织中的α_2相晶粒中的有序畴细化。Ti_3Al-11Nb合金从高温缓冷到室温的组织由粗大的α_2相晶粒和晶间的β相晶粒组成。Ti_3Al-10Nb合金从1200℃空冷、油淬和水淬到室温后,组织(主要或全部)分别为α_2相、马氏体相+B2相,B2相组成。油淬样品在750℃时效时沿晶界和晶内析出不同形态的α_2相。α_2相晶粒及其内部的有序畴在时效过程中长大。     

Ti—241Al—14Nb—3V—0.5Mo合金拉伸变形显微组织的研究

用透射电子显微镜研究了Ｔｉ３Ａｌ－Ｎｂ（Ｔｉ－２４Ａｌ－１４Ｎｂ－３Ｖ－０．５Ｍｏ）合金拉伸变形显微组织，利用双倾技术和双束条件下ｇ．ｂ＝０不可见判据，分析了合金中具有Ｄ０１９结构的α２相在拉伸过程中的变形机制。     

粉末冶金Nb—Ti—Al合金的研制

研究采用粉末冶金法制备铌基耐蚀仪表结构材料(Nb-40Ti-4Al-(0.2～0.3)O合金)。结果表明:采用Nb-Al中间合金粉和Ti粉,经混合、压制成形后,于1700℃真空烧结,保温4h,可制得致密且成分均匀的单相固溶体(氧含量0.2％～0.3％)。该合金易于加工成材,并且具有优良的综合性能,是理想的耐蚀仪表结构材料。使用效果良好。     

氢对Ti3Al-Nb合金微观组织和超塑变形行为的影响

研究了氢对Ti-24Al-14Nb-3V-0.5Mo合金微观组织和超塑变形的影响。结果表明：氢可增加合金中B2相的体积分数,促进变形过程中条状相晶粒的细化。氢的存在可降低合金在超塑变形过程中的流变应力,并在较低的温度下获得合金的最大m值。     

Ti—3Al—2.5V合金的热稳定性研究

Ｔｉ—３Ａ１—２．５Ｖ合金是美国６０年代研制的一种近α的α＋β型钛合金,最初是作为焊接管材和无缝管材而研制的．７０年代末该合金管材已在Ｆ１４、Ｆ１５、Ｂ１、波音７４７等飞机上应用．关于 Ｔｉ—３Ａ１—２．５Ｖ合金热稳定性研究,未见国外报道．为了了解该合金的热稳定性能,以Ｔｉ—３Ａ１—２．５Ｖ合金管、棒材为试验原料,研究了该合金在 １２５℃～ ５００℃温度区间,无应力作用时,分别热暴露４００ｈ～２０００ｈ后材料的热稳定性能．ｌ试验材料及方法１．１试验材料 试验材料选用经真空退火的１２ｍｍ×０．９ｍｍ、…     

粉末冶金Ti—14Al—21Nb合金的HIP成形

本文讨论了Ti-14Al-21Nb合金粉末热等静压(HIP)成形方法和工艺参数对合金室温拉伸性能的影响。用钛作包套并以电子束封焊是用于Ti_3Al基合金粉末HIP成形的有效方法。HIP成形的合金均可得到α_2+β结构,但是初生α_2相的含量随HIP温度的提高而减少,合金经1100℃HIP可以获得较好的强度和延伸率。     

Ti3Al—10Nb—3V—1Mo合金力学性能的研究

研究了 Ti_3Al-10Nb-3V-1Mo 合金的机械性能、拉伸断口和变形行为。结果表明:合金两相区淬火组织中。随淬火温度降低,初生α_2 相的数量逐渐增加,拉伸强度呈下降趋势。室温延伸率在初生α_2相含量为50%时,存在最大值。两相区淬火组织在700～850℃时效处理后 B2相发生分解。与淬火性能比较,合金经时效处理后塑性明显下降,室温拉伸断口及变形行为的研究表明:随淬火温度降低,断口形貌及变形行为呈现出一定的规律性。     

Ti—10V—2Fe—3Al合金的热变形行为

本文测试了Ti-10V-2Fe-3Al合金在700～950℃温度范围内,5×10~(-3)s~(-1)～10s~(-1)七个应变速率下的真应力-应变(σε)曲线,分析了变形组织,并对β区动态再结晶的形核机制进行了探讨。结果表明,在β区850～950℃下,应变速率ε=1s~(-1)～10s~(-1)范围内变形时,动态回复是主要软化机制,经计算得:应力指数n=4.1,激活能Q=195kJ/mol;当 ε≤10~(-1)s~(-1)时,有动态回复和动态再结晶两种软化机制,此时n=3.9,Q=157kJ/mol。α+β区变形时,有动态回复和动态再结晶两种软化机制。     

Creep behavior of Ti-25Al-10Nb-3V-1Mo

A study has been made of the role of microstracture in room-temperature tensile properties as well as elevated-temperature creep behavior of an advanced Ti₃Al-base alloy, Ti-25Al-10Nb-3V-lMo (atomic percent). Creep studies have been performed on this alloy as a function of stress and temperature between 650 °C and 870 °C, since the use of conventional titanium alloys has generally been restricted to temperatures below 600 °C. A pronounced influence of microstructure on creep resistance was found. Generally, the β solution-treated colony-type (slow-cooled or SC) microstructure showed superior creep resistance. This improved creep resistance in β/SC is accompanied by lower room-temperature tensile strength and ductility. Study of the stress dependence of steady-state creep rate indicates that increasing temperature caused a gradual decrease in the stress exponentn and a transition in creep mechanism at 870 °C, depending on applied stress level. Transmission electron microscopy observations of deformed dislocation structures developed during steady-state creep and room-temperature tensile tests, as well as the corresponding fracture modes, were used to interpret properties as a function of temperature. Finally, creep behavior of the present Ti₃Al alloy was found to be superior to that of conventional near-α titanium alloys. WONSUK CHO, formerly with Carnegie Mellon University, is Senior Research Staff Member, Kia Technical Center, Yeoeuido, P.O. Box 560, Seoul, Korea. JAMES WILLIAMS, formerly Dean of Engineering, Carnegie Mellon University.     

冷却速度对Ti3Al-10Nb-3V-1Mo合金组织的影响

用秀射龟镜研究了Ｔｉ３Ａｌ－１０Ｎｂ－３Ｖ－１Ｍｏ合金在１１７０℃加热１ｈ，以不同速度冷却后的显微组织结构。结果表明，Ｗ，Ｑ．组织由单一Ｂ２相组成，Ａ．Ｃ．组织由Ｂ２相基体组成，Ｂ２相晶粒内开始第二相的析出。     

退火温度对Ti-3Al-4.5V-5Mo钛合金显微组织和织构的影响

研究了退火温度对Ti-3Al-4.5V-5Mo钛合金丝材显微组织和织构的影响. 结果表明, 随着退火温度的提高, 初生α相的形态逐渐由条状α和球状α的混合组织向球状组织过渡, 晶粒尺寸逐渐增加. 当退火温度达到880 ℃时, 转变成粗晶片状组织. 两相区退火时,α相出现(φ1,～0°,φ2)织构组分, 其强度随着退火温度的升高而略有增加,β相(φ1,～0°,φ2)织构组分随着退火温度的升高逐渐增强. Β区退火后织构依然明显,α和β相织构分别主要为(φ1,～0°,φ2)和(φ1,～45°,0°).两相区退火加热时,α和β相发生了原位再结晶和形核长大再结晶, 在随后的炉冷过程中, β相向α相的转变主要是以在原有α相颗粒上的长大机制进行.     

A comparison study of microstructure and mechanical properties of Ti-24Al-14Nb-3V-0.5Mo with and without Si

A comparative study has been made of the room- and elevated-temperature properties, room-temperature fracture toughness, fatigue-crack propagation rates, and 650 °C creep properties of Ti-24Al-14Nb-3V-0.5Mo with and without 0.9 at. pct Si. Both alloys have microstructures consisting of the α ₂, B2, and the orthorhombic O phase, with different proportions of the α ₂ phase relative to the (O + B2) mixtures, depending on solution-treatment temperature. The alloy with a Si addition contains additional primary ζ-Ti₅Si₃ particles distributed in the (O + B2) matrix. Tests of mechanical properties showed that the incorporation of a small fraction (about 0.03 by volume) of the Ti₅Si₃ phase leads to greater room-temperature and elevated-temperature strengths, but lower room-temperature elongations and fracture toughness as compared with the base alloy. Alloys containing greater volume fractions of the α ₂ phase exhibited better tensile ductility, and this was attributed to the concurrent stabilization of the B2 phase. Examination of tensile-tested and fatigued specimens indicates that the primary failure mode of the alloys, regardless of Si addition, was due to the brittleness of the α ₂ phase; the silicide particles that debonded from the matrix also contribute to cracking in the monotonic loading mode. Up to a 20 pct improvement in creep-rupture life was observed in the Si-containing alloys, and this was interpreted in terms of the solute-strengthening effect of Si. While the incorporated Ti₅Si₃ phase has an unfavorable effect on ductility and room-temperature fracture toughness, the difference in fatigue-crack propagation rates between the alloys with and without Si is minimal. It is concluded that the controlling factor for the fatigue failure in orthorhombic alloys is related to the (α ₂ + O + B2) microstructure, instead of the Ti₅Si₃ particles.     

退火温度对Ti-6Al-3Nb-2Zr-1Mo合金组织及力学性能的影响

研究了退火温度对Ti-6Al-3Nb-2Zr-1Mo合金组织和力学性能的影响。结果表明:随着退火温度升高,初生α相含量降低,2°～15°小角度晶界逐渐减少;退火温度较高时,退火过程中发生了α相→β相→α相的相变,<0001>//横向织构消失。随着退火温度升高,Ti-6Al-3Nb-2Zr-1Mo合金屈服强度逐渐降低,抗拉强度、延伸率先升高后降低。退火温度升高后,片层组织比例升高,裂纹扩展功占冲击吸收功的比例增大,材料韧性提升。     

TiAl基合金超塑性变形中的位错运动

研究了结晶Ｔｉ－３３Ａｌ－３Ｃｒ－０．５Ｍｏ合金在超塑性变形过程中的位错运动。透射电镜分析结果表明，超塑性变形时，合金中存在大量位错运动，在晶界附近和晶粒内形成了位错网，并在晶界上出现位错塞积。大多数位错是从晶界及α２相粒子处发射出来的。     

The Influence of Induction Sintering on Microstructure and Deformation Behavior of Ti-5Al-5Mo-5V-3Cr Alloy

The influence of the induction sintering process at different temperatures on the behavior of the powder metallurgy Ti-5Al-5Mo-5V-3Cr alloy was investigated. Material for the research was produced by elemental powder blending, followed by the uniaxial cold compacting process. Powder compacts were induction heated and sintered within the temperature range of 1000 °C to 1300 °C. The influences of process parameters on the material behavior during sintering and its properties were studied. The microstructure examination was performed with particular attention to the pore size and distribution as well as the homogenization of the microstructure. The sintering temperature of 1200 °C proved to be critical for the dissolution of most alloying powder particles. Hot compression tests were performed to determine the formability of the obtained material. Significant differences in flow stress behavior between samples sintered at temperatures below and above 1200 °C were observed. The mechanical properties of the material before and after deformation were compared. The evolution of the microstructure of sintered Ti-5Al-5Mo-5V-3Cr alloy after hot deformation was analyzed with an emphasis on its influence on the material properties. Based on the conducted research, it was found that the adequate homogenization of the chemical composition and microstructure was achieved at the temperature of 1250 °C, and a further increase did not reflect in a significant improvement.

     

热处理对Ti-5Mo-5V-2Cr-3Al合金组织和性能影响

通过扫描电镜(SEM), 光学显微镜(OM)和X射线衍射分析(XRD)等对Ti-5Mo-5V-2Cr-3Al(Ti5523)合金棒材分别经固溶和固溶时效处理后得到的微观组织, 相含量等进行分析, 结合性能数据, 分析了微观结构对性能的影响. 研究发现, 在720 ℃固溶0.5 h, 并在540 ℃时效6 h后, 获得了一种规则的垂直有序排列的亚结构, 这种网篮状亚结构起到了组织细化的作用, 从而使得断面收缩率非常高. 研究还发现, 两相区固溶后析出相不仅使得强度提高, 对材料的塑性也有贡献.