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

Article Preview

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.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

208-216

Citation:

Online since:

May 2020

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2020 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[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).

Google Scholar

[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).

DOI: 10.1016/j.matdes.2010.09.011

Google Scholar

[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.

Google Scholar

[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.

DOI: 10.1177/146442070121500201

Google Scholar

[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).

Google Scholar

[6] J.M. Cai, G.B. Mi, F. Gao, Research and Development of Some Advanced High Temperature Titanium Alloys for Aero-engine, J. Journal of Materials Engineering, 2016, 44(8): 1-10.

Google Scholar

[7] C. Suryanarayana, F.H. Froes, Mechanical Alloying of Titanium-Base Alloys, J. Advanced Materials, 2010, 5(2): 96-106.

DOI: 10.1002/adma.19930050205

Google Scholar

[8] N. Singh, V. Singh, Effect of temperature on tensile properties of near-α alloy Timetal 834, J. Materials Science & Engineering A, 2008, 485(1): 130-139.

DOI: 10.1016/j.msea.2007.07.064

Google Scholar

[9] M.Y. Hao, J.M. Cai, J. Du, The effect of heat treatment on microstructure and properties of BT36 high temperature alloy, J. Journal of Aeronautical Materials, 2003, 23(2): 14-17.

Google Scholar

[10] P.L. Narayana, S.W. Kim, J.K. Hong, Tensile properties of a newly developed high-temperature titanium alloy at room temperature and 650 °C, J. Materials Science and Engineering: A, 2018:S0921509318301540.

DOI: 10.1016/j.msea.2018.01.113

Google Scholar

[11] W.Y. Liu, Y. Lin, Y. Chen, et al, The Effect of Different Heat Treatments on Microstructure and Mechanical Properties of Ti6Al4V Titanium Alloy, J. Rare Metal Materials & Engineering, 2017, 46(3): 634-639.

DOI: 10.1016/s1875-5372(17)30109-1

Google Scholar

[12] S. Zhu, H. Yang, L.G. Guo, et al, Effect of cooling rate on microstructure evolution during α/β heat treatment of TA15 titanium alloy, J. Materials Characterization, 2012, 70(none): 101-110.

DOI: 10.1016/j.matchar.2012.05.009

Google Scholar

[13] Y.G. Zhou, W.D. Zeng, H.Q. Yu, An investigation of a new near-beta forging process for titanium alloys and its application in aviation components, J. Materials Science & Engineering A, 2005, 393(1): 204-212.

DOI: 10.1016/j.msea.2004.10.016

Google Scholar

[14] R. Duan, J.M. Cai, Z.X. Li, Effect of Primary α Phase Volume Fraction on Tensile Property and Thermal Stability of Near-Alpha TG6 Titanium Alloy, J. Journal of Aeronautical Materials, 2007, 27(3): 17-22.

Google Scholar

[15] T.R. Bieler, M.A. Crimp, Y. Yang, et al, Strain heterogeneity and damage nucleation at grain boundaries during monotonic deformation in commercial purity titanium, J. JOM, 2009, 61(12): 45-52.

DOI: 10.1007/s11837-009-0180-x

Google Scholar

[16] V.M. Imayev, R.A. Gaisin, R.M. Imayev, Microstructure and mechanical properties of near α titanium alloy based composites prepared in situ by casting and subjected to multiple hot forging, J. Journal of Alloys & Compounds, 2018, 762: 555-564.

DOI: 10.1016/j.jallcom.2018.05.273

Google Scholar

[17] Y.W. Sui, A.H. Liu, B.S. Li, et al, Relationship between Thickness of Lamellar α+β Phase and Mechanical Properties of Titanium Alloy, J. Advanced Materials Research, 2011, 311-313: 1916-1919.

DOI: 10.4028/www.scientific.net/amr.311-313.1916

Google Scholar

[18] K. Wang, M.Q. Li, Morphology and crystallographic orientation of the secondary α phase in a compressed α/β titanium alloy, J. Scripta Materialia, 2013, 68(12): 964-967.

DOI: 10.1016/j.scriptamat.2013.02.048

Google Scholar

[19] Q.J. Wang, J.R. Li, R. Yang, High temperature titanium alloys: status and perspective, Journal of Aeronautical Materials, 34 (2014) 1-26.

Google Scholar