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Chinese Journal of Materials Research  2021, Vol. 35 Issue (10): 741-751    DOI: 10.11901/1005.3093.2020.536
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A Novel Ti-4.13Al-9.36V Alloy of High Ductility Designed on Base of α''-Microstructure for Laser Solid Forming
LIU Tianyu1, ZHU Zhihao1, ZHANG Shuang2, DONG Chuang1,2(), MIN Xiaohua3, WANG Qing1
1.Key Laboratory of Materials Modification by Laser, Ion and Electron Beams (Ministry of Education), School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
2.School of Materials Science and Engineering, Dalian Jiaotong University, Dalian 116028, China
3.School of Materials Science and Engineering, Dalian University of Technology, Dalian 116024, China
Cite this article: 

LIU Tianyu, ZHU Zhihao, ZHANG Shuang, DONG Chuang, MIN Xiaohua, WANG Qing. A Novel Ti-4.13Al-9.36V Alloy of High Ductility Designed on Base of α''-Microstructure for Laser Solid Forming. Chinese Journal of Materials Research, 2021, 35(10): 741-751.

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Abstract  

Ti-6Al-4V alloy is widely used in laser solid forming, however, low work-hardening ability and ductility limit its industrial applications. In this paper, a novel Ti-4.13Al-9.36V (%) alloy with cluster composition of 4[Al-Ti12](AlTi2)+12[Al-Ti14](V2Ti) was designed based on the cluster composition formula 12[Al-Ti12](AlTi2)+5[Al-Ti14](V2Ti) of Ti-6Al-4V. Samples of two alloys Ti-4.13Al-9.36V and Ti-6.05Al-3.94V (set as contrast alloy) were prepared by laser solid forming and followed by heat treatment. Then the microstructure and mechanical properties of the as-deposited and solution treated alloys were investigated. The results show that the microstructure of the as-deposited alloys Ti-4.13Al-9.36V and Ti-6.05Al-3.94V consists of columnar prior-β grains, which grow epitaxial from the substrate along the deposition direction. A basket-weave α-laths existed in the inner prior-β grains. The width of prior-β grains and the width of α-laths of Ti-4.13Al-9.36V alloy are ca 606 μm and 0.48 μm, in the contrast, those of Ti-6.05Al-3.94V alloy are ca 770 μm and 0.71 μm, respectively. Further, after the Ti-6.05Al-3.94V subjected to post solution treatment at 920°C for 2 h followed by water cooling, its microstructure consists of phases α'+α, and the corresponding yield strength, ultimate tensile strength and ductility to failure were ca 893 MPa, 1071 MPa and 3%, respectively. However, when the Ti-4.13Al-9.36V subjected to post solution treatment at 750°C for 2 h followed by water cooling, its microstructure consists of phases α''+α, and the related yield strength, ultimate tensile strength and ductility to failure were ca 383 MPa, 989 MPa and 17%, respectively. This may be ascribed to that the stress-induced α''-phase could significantly improve the work-hardening ability compared with α'-phase. The work-hardening ability and ductility of the Ti-alloy used for laser solid forming could be significantly improved by adjusting the microstructure with phases α''+αvia cluster-plus-glue atom model.

Key words:  metallic materials      composition design      cluster-plus-glue atom model      laser solid forming      work-hardening     
Received:  17 December 2020     
ZTFLH:  TG166.5  
Fund: National Key Research and Development Program of China(2016YFB1100103);Key Discipline and Major Project of Dalian Science and Technology Innovation Foundation(2020JJ25CY004)
About author:  DONG Chuang, Tel: (0411)84708389, E-mail: dong@dlut.edu.cn

URL: 

https://www.cjmr.org/EN/10.11901/1005.3093.2020.536     OR     https://www.cjmr.org/EN/Y2021/V35/I10/741

Alloy

Cluster formulas

/(atom fraction, %)

Composition

/(mass fraction, %)

[Mo]eq
112[Al-Ti12](AlTi2)+5[Al-Ti14](V2Ti)Ti-6.05Al-3.94V2.64
24[Al-Ti12](AlTi2)+12[Al-Ti14](V2Ti)Ti-4.13Al-9.36V6.27
Table 1  Cluster formulas of designed Ti-Al-V alloys and their compositions
Fig.1  SEM image of Ti, Al and V powders mixture for Ti-6.05Al-3.94V (a) and scanning strategy for laser additive manufacturing (b)
Fig.2  Measurement locations of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V
Fig.3  XRD spectra of the laser solid formed Ti-6.05Al-3.94V and Ti-4.13Al-9.36V samples (a) XRD spectra of the as-deposited samples, and (b) XRD spectra of the different solution temperature, wherein Ti-4.13Al-9.36V alloy solution temperature subjected to 700℃, 750℃ and 800℃, and is Ti-6.05Al-3.94V subjected to 920℃, respectively
Fig.4  As-deposited microstructure of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V (a, b) OM images of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V, (c, d) SEM images of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V
Fig.5  SEM images of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V (a) SEM image of Ti-6.05Al-3.94V after solution treatment at 920℃, and (b)(c)(d) SEM images of Ti-4.13Al-9.36V after solution treatment at 700℃, 750℃ and 800℃, respectively
Temperature/℃The α laths width / μm
Ti-6.05Al-3.94VTi-4.13Al-9.36V
700-0.52±0.05
750-0.56±0.03
800-0.63±0.09
9201.03±0.09-
Table 2  Changes of α laths width in Ti-6.05Al-3.94V and Ti-4.13Al-9.36V with different solution temperature
Fig.6  TEM morphological images and diffraction pattern of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V (a~c) TEM morphological images and diffraction pattern of Ti-6.05Al-3.94V after solution treatment at 920℃, (d~f) TEM morphological images and diffraction pattern of Ti-4.13Al-9.36V after solution treatment at 800℃
Temperature/℃Vickers hardness / HV
Ti-6.05Al-3.94VTi-4.13Al-9.36V
Room temperature331±10337±7
700-348±5
750-298±6
800-289±4
920374±6-
Table 3  Vickers hardness of the as-deposited and solution heat treatment in Ti-6.05Al-3.94V and Ti-4.13Al-9.36V
Fig.7  Engineering stress-strain curves of the as-deposited and solution heat treatment Ti-6.05Al-3.94V and Ti-4.13Al-9.36V (a) stress-strain curves of the as-deposited Ti-6.05Al-3.94V and Ti-4.13Al-9.36V, (b) stress-strain curves of Ti-6.05Al-3.94V and Ti-4.13Al-9.36V subjected to different solution-treatment temperature
AlloyσYS / MPaσUTS / MPaδ / %
As-deposited (Ti-6.05Al-3.94V)924±9977±1010±1
As-deposited (Ti-4.13Al-9.36V)950±11989±510±0.5
700℃ (Ti-4.13Al-9.36V)900±9986±810±1
750℃ (Ti-4.13Al-9.36V)383±12989±1117±0.7
800℃ (Ti-4.13Al-9.36V)424±7895±810±0.6
920℃ (Ti-6.05Al-3.94V)893±101071±73±1
Table 4  Yield strength (σYS), tensile strength (σUTS) and elongation (δ) of the as-deposited and solution- treatment Ti-6.05Al-3.94V and Ti-4.13Al-9.36V alloy
Fig.8  Curve of work hardening rate
Fig.9  SEM fracture morphologies of the as-deposited Ti-6.05Al-3.94V and Ti-4.13Al-9.36V, (a) Ti-6.05Al-3.94V, (b) Ti-4.13Al-9.36V
Fig.10  SEM fracture morphologies of the solution-treatment Ti-6.05Al-3.94V and Ti-4.13Al-9.36V (a) Ti-6.05Al-3.94V after solution treatment at 920℃, (b, c, d) Ti-4.13Al-9.36V after solution treatment at 700℃, 750℃ and 800℃
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