Abstract

The isothermal compression tests of Ti-25.5Al-13.5Nb-2.8Mo-1.8Fe (at.%) alloys were executed under the deformation temperature ranges of 950-1100 C with the strain rate ranges of 0.001-1 s-1, for total height reduction of 0.5. The isothermal compression deformation behavior was investigated based on flow stress curves, dynamic model analysis. The processing map of Ti-25.5Al-13.5Nb-2.8Mo-1.8Fe alloy was obtained for the optimum hot process parameters. The calculated value of Q (activation energy) was 634.5 kJ/mol. The constitutive model of the alloy was constructed. Based on DMM and the Prasad flow instability criteria, the hot processing map was established with strain of 0.7. The deformation mechanisms were interpreted by microstructural observation within both stable and instability zones. Processing map showed a stable region under the deformation temperature ranges of 950-1100 C with the strain rate ranges of 0.001-1 s-1. One certain maximum power dissipation efficiency value was approximately 43 % occurred at 950 C/0.001 s-1. Another peak power dissipation efficiency value was about 58 % at 1050 C/0.001 s-1. Both areas were the optimum processing regions. Furthermore, while the strain rate value exceeded 1 s-1, the alloy sustained deformation instability phenomenon, such as shearing band or flow localization.

Highlights

  • The Ti2AlNb-based alloy (Banerjee et al, 1988; Khadzhieva et al, 2014) combines low density, an improved oxidation resistance, and higher fracture toughness compared with the traditional TiAl and NiAl intermetallics (Feng et al, 2002; Yang et al, 2004; Lin et al, 2012)

  • The isothermal compression tests of Ti-25.5Al-13.5Nb-2.8Mo1.8Fe alloys were executed under the deformation temperature range of 950–1,100◦C with the strain rate range of 0.001–1 s−1 for a total height reduction of 0.5

  • The isothermal compression deformation behavior was investigated based on flow stress curves and dynamic model analysis

Read more

Summary

Introduction

The Ti2AlNb-based alloy (Banerjee et al, 1988; Khadzhieva et al, 2014) combines low density, an improved oxidation resistance, and higher fracture toughness compared with the traditional TiAl and NiAl intermetallics (Feng et al, 2002; Yang et al, 2004; Lin et al, 2012). Ti2AlNb intermetallics have been regarded as promising structural metals to be applied to aircraft engine components (Banerjee, 1997; Germann et al, 2005). Nb is an expensive and high-density additional beta-stabilizer element in Ti2AlNb alloys. Efforts have been made to reduce the Nb content of Ti2AlNb alloys by substituting Nb with other low-cost beta-stabilizer elements (Feng et al, 2002; Cao et al, 2006; Mao et al, 2007).

Objectives
Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call