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金属学报  2017, Vol. 53 Issue (9): 1055-1064    DOI: 10.11900/0412.1961.2016.00457
  本期目录 | 过刊浏览 |
Ti-43Al-4Nb-1.5Mo合金包套锻造与热处理过程的微观组织及高温拉伸性能
李天瑞1, 刘国怀1(), 徐莽1, 牛红志2, 付天亮1, 王昭东1, 王国栋1
1 东北大学轧制技术与连轧自动化国家重点实验室 沈阳 110819
2 东北大学材料科学与工程学院 沈阳 110819
Microstructures and High Temperature Tensile Properties of Ti-43Al-4Nb-1.5Mo Alloy in the Canned Forging andHeat Treatment Process
Tianrui LI1, Guohuai LIU1(), Mang XU1, Hongzhi NIU2, Tianliang FU1, Zhaodong WANG1, Guodong WANG1
1 State Key Laboratory of Rolling and Automation, Northeastern University, Shenyang 110819, China
2 School of Materials Science and Engineering, Northeastern University, Shenyang 110819, China
引用本文:

李天瑞, 刘国怀, 徐莽, 牛红志, 付天亮, 王昭东, 王国栋. Ti-43Al-4Nb-1.5Mo合金包套锻造与热处理过程的微观组织及高温拉伸性能[J]. 金属学报, 2017, 53(9): 1055-1064.
Tianrui LI, Guohuai LIU, Mang XU, Hongzhi NIU, Tianliang FU, Zhaodong WANG, Guodong WANG. Microstructures and High Temperature Tensile Properties of Ti-43Al-4Nb-1.5Mo Alloy in the Canned Forging andHeat Treatment Process[J]. Acta Metall Sin, 2017, 53(9): 1055-1064.

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摘要: 

对Ti-43Al-4Nb-1.5Mo合金进行包套锻造和后续热处理实验,考察了该过程TiAl合金的热变形行为、流变软化机制以及热处理参数对微观组织和力学性能的影响。结果表明,TiAl合金包套锻造过程的高温流变软化以β相协调变形、片层相变分解、γ相内位错滑移以及孪晶诱导的动态再结晶为主,最终组织为残余α2/γ层片和等轴α2γ、B2相的混合组织。随热处理温度的升高,热变形组织由残余α2/γ层片和多相混合组织转变为α2/γ层片+γ相组织,在较高的温度下(1300 ℃)转变为全层片组织。其中,B2相随着溶质扩散程度的增加逐渐消失,残余层片组织发生分解转变为等轴α2/γ层片团,同时发生γα转变,形成全层片组织。对热等静压、锻态和热处理试样的高温(800 ℃)拉伸性能进行比较,经热处理后获得的全片层组织具有最佳的综合性能,抗拉强度为663 MPa,延伸率达到26%。分析该样品的断裂行为可知,由于存在层片扭曲拉长、微孔钝化以及裂纹曲折延伸的断裂机制,全层片组织具有良好强度-塑性的综合力学性能。另外,热加工过程中(高温) bcc结构B2相能够协调变形,但服役条件下硬脆的B2相作为裂纹源容易引起裂纹萌生,对力学性能极其不利。因此,TiAl合金在热变形和服役过程中需要对组成相进行严格控制,从而获得良好的力学性能。

关键词 TiAl合金包套锻造热处理微观组织力学性能    
Abstract

TiAl alloys are highly promising for high temperature structural application due to their excellent mechanical properties. However, the widespread applications of TiAl alloys have been limited for their low temperature brittleness and poor workability. The further thermo-mechanical treatments is applied for fine microstructures and improved ductility to promote the commercial applications, during which the investigations of hot deformation behavior and microstructural evolution are necessary for the improved microstructure and mechanical properties. The canned forging and subsequent heat treatments of Ti-43Al-4Nb-1.5Mo alloy have been conducted, during which the hot deformation behavior, flow softening mechanism, microstructure evolution and mechanical properties were investigated. The results show that the flow softening process of the canned forging TiAl alloy can be attributed to the soft β phase, α2/γ lamellae decomposition and the dynamic recrystallization induced by dislocation slipping and twinning in γ phase, and the final microstructure is composed of remnant α2/γ lamellae and equiaxed α2, γ and B2 phases. With the increasing heat treatment temperature, the microstructure changes from the multi-phase structure (remnant α2/γ lamellar, equiaxed α2, γ and B2 phases) at 1250 ℃ to the α2/γ lamellar and γ phase at 1285 ℃, and then the fully α2/γ lamellar structure at 1300 ℃, during which the B2 phase is gradually dissolved due to the solution diffusion, and the remnant α2/γ lamellae change to equiaxed α2/γ colonies according to the α2/γγ+α2+B2 transition, and the final fully α2/γ lamellar structure is promoted by γα transition at high temperature. Moreover, the tensile tests of the hot isostatic pressed (HIPed) samples, canned forged and heat treated samples at 800 ℃ are conducted, in which the fully lamellar structure shows the high properties with the ultimate strength of 663 MPa and the elongation of 26%. The deformation process of the fully α2/γ lamellar can be strengthened by the lamellae twisting, microvoid inhibition and wavy growth of the cracks, leading to the optimal high temperature performance. Moreover, the disordered bcc β phase can promote the deformation during the hot working process at the high temperature (≥1200 ℃), while the hard-brittle B2 phase severely deteriorates the service properties, which should be controlled accurately for the high mechanical properties during the thermo-mechanical processing.

Key wordsTiAl alloy    canned forging    heat treatment    microstructure    mechanical property
收稿日期: 2016-10-17     
ZTFLH:  TG146  
基金资助:国家重点研发计划项目Nos.2016YFB0301200和2016YFB0300603,国家自然科学基金项目No.51504060,中央高校基本科研业务费项目No.N140703003及辽宁省科技项目博士启动基金项目No.201501150
作者简介:

作者简介 李天瑞,女,1992年生,博士生

图1  热等静压Ti-43Al-4Nb-1.5Mo合金的微观组织和相组成
图2  包套锻造Ti-43Al-4Nb-1.5Mo合金不同位置处的微观组织
图3  包套锻造Ti-43Al-4Nb-1.5Mo合金微观组织的EBSD表征
图4  包套锻造Ti-43Al-4Nb-1.5Mo合金的热变形组织以及局部流变软化机制示意图
图5  包套锻造Ti-43Al-4Nb-1.5Mo合金的相分解和再结晶过程
图6  包套锻造Ti-43Al-4Nb-1.5Mo合金不同温度热处理后的微观组织
图7  包套锻造Ti-43Al-4Nb-1.5Mo合金不同温度热处理后各组成相的体积分数变化
Specimen σ0.2 / MPa σb / MPa δ / %
HIP (1250 ℃, 120 MPa, 4 h, FC) 416 492 2.9
Canned forging 534 594 33.0
Canned forging +1250 ℃, 30 min, FC 506 576 36.0
Canned forging +1300 ℃, 30 min, FC 552 663 26.0
表1  Ti-43Al-4Nb-1.5Mo合金不同处理工艺下800 ℃的拉伸性能
图8  Ti-43Al-4Nb-1.5Mo合金不同组织高温拉伸后断口附近的裂纹扩展
图9  Ti-43Al-4Nb-1.5Mo合金经HIP和热处理后的高温拉伸断口形貌
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