Elsevier

Materials Science and Engineering: A

Volume 530, 15 December 2011, Pages 239-243
Materials Science and Engineering: A

The recrystallization behavior of surface deformation layer of (TiB + TiC)/Ti–6Al–4V composite during isothermal annealing

https://doi.org/10.1016/j.msea.2011.09.081Get rights and content

Abstract

The recrystallization behavior of surface deformation layer of (TiB + TiC)/Ti–6Al–4V and Ti–6Al–4V were both investigated during isothermal annealing using X-ray diffraction line profile analysis. The surface deformation layer was introduced by shot peening treatment. The results revealed that with increasing the time of isothermal annealing, the microstructure variations at shot peened layer were obvious. Based on the results of line profile analysis, the recrystallization activation energies were calculated by computer regression analysis, and it showed that the recrystallization activation energy of (TiB + TiC)/Ti–6Al–4V was larger than that of Ti–6Al–4V, which was ascribed to the effect of reinforcements hindering the movements of dislocations, grain and subgrain boundaries in the process of recrystallization. The hindrance effect of reinforcements as sink sources of dislocations gliding resulted that the decrease rate of dislocation density of the composite was slower than that of the matrix. In addition, the relaxation activation energies were obtained according to the analysis of microstrain relaxation, and after isothermal annealing, the depth distribution of domain sizes from the top surface was investigated and discussed in detail. According to above analysis, the results showed that the thermostability of the composite was higher than that of the matrix because of the effect of reinforcements.

Highlights

► The recrystallization activation energies are calculated by regression analysis. ► Larger activation energy of composite results from the effect of reinforcements. ► Reinforcements hinder grain and subgrain boundaries glide in recrystallization. ► The relaxation activation energies are obtained based on microstrain relaxation. ► SP treatment and thermal transfer direction are significant in recrystallization.

Introduction

At present, the research on titanium matrix composites becomes more and more significant and promising because of their excellent physical and mechanical properties [1], [2], [3], [4]. However, in order to improve their fatigue strength and life, crack initiation and growth at surface layers must be suppressed using surface treatments [5]. Shot peening (SP) is an effective surface mechanical treatment method widely used in industry which can improve surface properties, such as fatigue strength, stress corrosion resistance, surface hardness, etc. [6], [7]. However, the physical metallurgical processes such as recrystallization and grain growth, which happens at high temperatures can deteriorate the properties of shot peened components. Thus, the investigation on the thermostability of microstructure at elevated temperatures is important for retaining high properties of titanium matrix composites.

Till now, the researches on titanium matrix composites are mostly on the mechanical properties [3], [4], [8], [9], little investigation has been made on recrystallization behavior and thermostability of composite materials after SP together with heat treatment. And X-ray diffraction (XRD) line profile analysis is an important method for describing the microstructure variations of crystalline materials because XRD is reliability and non-destruction to materials [10], [11], [12], [13]. Therefore, the present investigation deals with the recrystallization behavior of deformation layer of in situ (TiB + TiC)/Ti–6Al–4V and Ti–6Al–4V during isothermal annealing using XRD line profile analysis.

Section snippets

Experimental

The shot peened deformation layers of (TiB + TiC)/Ti–6Al–4V (TiB:TiC = 1:1 (vol%)) and Ti–6Al–4V were investigated during isothermal annealing. The composite material was fabricated via in situ technology [14], [15], and the total volume percentage of reinforcements (TiB and TiC) was 5%. SP treatment was performed using an air blast machine (Carthing Machinery Company, Shanghai). In the process of SP, a great amount of high hardness small shot balls impact on the surface of metal materials with

Results and discussion

XRD patterns of the peened surface under different annealing time and temperatures have been shown in Fig. 1, and the peak breadth decreases with the increase of annealing time at the same annealing temperature. Comparing Fig. 1(a) with (b), it reveals that under the same annealing time, the breadth of diffraction peaks become narrower at the higher annealing temperature. For metal materials, in the process of SP, a great amount of small shot balls with high kinetic energy impacting on the

Conclusions

Using X-ray diffraction, the recrystallization behavior of surface deformation layer of (TiB + TiC)/Ti–6Al–4V and Ti–6Al–4V introduced by shot peening were investigated. The results revealed that with increasing annealing time, domain size increased and microstrain relaxed. The recrystallization activation energies of (TiB + TiC)/Ti–6Al–4V and Ti–6Al–4V were obtained, which were 341 and 294 kJ/mol respectively, and it was showed that the recrystallization activation energy of composite was larger

Acknowledgement

This work is supported by the project of 973 Program under grant no. 2007CB613806.

References (29)

  • A.K. Kuruvilla et al.

    Scripta Metall. Mater.

    (1990)
  • W. Lu et al.

    Scripta Mater.

    (2001)
  • W. Lu et al.

    J. Alloys Compd.

    (2001)
  • L. Wagner

    Mater. Sci. Eng. A

    (1999)
  • N. Sidhom et al.

    Int. J. Fatigue

    (2005)
  • Y.F. Al-Obaid

    Eng. Fract. Mech.

    (1995)
  • K. Geng et al.

    Mater. Lett.

    (2003)
  • S.C. Tjong et al.

    Mater. Sci. Eng. R

    (2000)
  • T. Ungar

    Mater. Sci. Eng. A

    (2001)
  • W. Luan et al.

    Mater. Sci. Eng. A

    (2008)
  • S. Ranganath et al.

    Mater. Sci. Eng. A

    (1992)
  • X. Zhang et al.

    Scripta Mater.

    (1999)
  • S. Vives et al.

    Mater. Sci. Eng. A

    (2004)
  • G. Liu et al.

    Mater. Sci. Eng. A

    (2000)
  • Cited by (0)

    View full text