Microstructures and Mechanical Properties of a New Type of High Temperature Titanium Alloy

Author:

Cui Ya Peng1,Chen Zi Yong1,Ma Xiao Zhao1,Liu Ying Ying1,Xiang Zhi Lei1,Chai Li Hua1

Affiliation:

1. Beijing University of Technology

Abstract

The microstructures and mechanical properties of a new type near α high temperature titanium alloy Ti-6.5Al-2.5Sn-9Zr-0.5Mo-0.25Si-1Nb-1W-0.3Re (wt. %) (denoted as TA6.5) were investigated. It was observed that the microstructure of forged TA6.5 mainly consisted of deformed lamellar α phase, small amount of equiaxed α phase, and residual β phase, exhibiting high strength and comparatively low elongation. Three different heat treatments processes were performed on forged TA6.5. The results showed that all heat treated alloys displayed high tensile strengths, and the values of strength parameters were almost unchanged with the increasing solution temperature, ascribing to the combination effects of decreasing primary α phase and increasing contents and widths of secondary α phase and lamellas. The tensile elongations of heat treated alloys tested at 650 °C decreased slightly with the increasing solution temperature, which is due to the increased width of secondary α lamellas and the generation of coarse grain boundary α phase. TA6.5 treated in the process of 990 °C/1 h/AC+700 °C/4 h/AC exhibited excellent comprehensive mechanical properties, i.e. the ultimate tensile strength of 829 MPa, yield strength of 707 MPa and elongation of 18.73% respectively.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference19 articles.

1. H.X. Jin, K.X. Wei, J.M. Li, J.Y. Zhou, W.J. Peng, Research development of titanium alloy in aerospace industry, J. The Chinese Journal of Nonferrous Metals, (2015).

2. C.X. Cui, B.M. Hu, L.C. Zhao, S.J. Liu, Titanium alloy production technology, market prospects and industry development, J. Materials and Design, 32(3) (2010).

3. X. Huang, Z.X. Li, H. Huang, Recent development of new high-temperature titanium alloys for high thrust-weight ratio aero-engines, J. Materials China, 30(6) (2011) 21-27.

4. M.R. Winstone, A. Partridge, J.W. Brooks, The contribution of advanced high-temperature materials to future aero-engines, J. Proceedings of the Institution of Mechanical Engineers Part L Journal of Materials Design & Applications, 2001, 215(2): 63.

5. J.M. Cai, Z.X. Li, J.M. Ma, Research and development of 600 °C high temperature titanium alloys for aeroengine, J. Materials Review, (2005).

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3