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Analysis of In Situ Synthesis and Cross-Sectional Evolution of Wear Scars of TiAl-Ag Composites

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Abstract

The need for reducing the energy consumption and volume of materials used in the aerospace industry has been driving the further optimization of the behavior of TiAl alloy under friction and wear. Therefore, investigating the micro-/nanostructures of the wear scar cross sections when TiAl-Ag composites slide against an immobile Si3N4 ball should help to analyze the friction and wear behaviors. Plastic deformation was observed to occur in the cross sections of the analyzed wear scar during the initial −25 min of the experiments; consequently, a work-hardened layer formed, and the friction coefficient and wear rate rapidly decreased. During the 25-60 min interval, the wear debris was refined in succession and formed a lubrication film, and the friction resistance and material loss were reduced. During the 60-120 min interval, a remarkably large amount of Ag was determined to be well distributed across the wear scar. It coincided with excellent deformation; moreover, the friction coefficients and wear rates of the TiAl-10 wt.% Ag composites were low.

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Acknowledgments

This work is supported by China postdoctoral Science Foundation (2019M662484), Henan postdoctoral Foundation and postdoctoral Foundation (BHJ2019006), as well as Doctoral Start-up Funding (BSJ2018005) of Anyang Institute of Technology, Foundation of Henan Educational Committee (19A460011), Project for Science and Technology Plan of Henan Province (192102210010), Tribology Science Fund of State Key Laboratory of Tribology (SKLTKF18B09), and Sichuan Provincial Key Lab of Process Equipment and Control (GK201901). Authors are also appreciative to Nan**g XFNANO Materials Tech Co., Ltd., for their kind assistance.

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Appendix

Appendix

$$E_{\text{TiAl - Ag}} = E_{\text{Ag}} \cdot \phi_{\text{Ag}} + E_{\text{TiAl}} \cdot (1 - \phi_{\text{Ag}} )$$
(1)
$$a = \left\{ {\frac{{3\pi \cdot F \cdot R_{\text{TiAl - Ag}} \cdot R_{{{\text{Si}}_{3} {\text{N}}_{4} }} }}{{4\left( {R_{\text{TiAl - Ag}} + R_{{{\text{Si}}_{3} {\text{N}}_{4} }} } \right)}}\left[ {\frac{{1 - \upsilon_{{^{\text{TiAl - Ag}} }}^{2} }}{{\pi \cdot E_{\text{TiAl - Ag}} }} + \frac{{1 - \upsilon_{{{\text{Si}}_{3} {\text{N}}_{4} }}^{2} }}{{\pi \cdot E_{{{\text{Si}}_{3} {\text{N}}_{4} }} }}} \right]} \right\}^{{{\raise0.7ex\hbox{$1$} \!\mathord{\left/ {\vphantom {1 3}}\right.\kern-0pt} \!\lower0.7ex\hbox{$3$}}}}$$
(2)
$$\sigma_{x} = \frac{3F}{{2\pi \cdot a^{3} }}\left[ {(1 + \upsilon_{\text{TiAl - Ag}} ) \cdot (z \cdot \tan^{ - 1} (a/z) - a) + \frac{{a^{3} }}{{2(a^{2} + z^{2} )}}} \right]$$
(3)
$$\sigma_{y} = \frac{3F}{{2\pi \cdot a^{3} }}\left[ {(1 + \upsilon_{\text{TiAl - Ag}} ) \cdot (z \cdot \tan^{ - 1} (a/z) - a) + \frac{{a^{3} }}{{2(a^{2} + z^{2} )}}} \right]$$
(4)
$$\sigma_{z} = \frac{3F}{{2\pi \cdot a^{3} }}\left[ {\frac{{ - a^{3} }}{{a^{2} + z^{2} }}} \right]$$
(5)
$$F_{f} = \mu \cdot F\quad \tau_{xy} = 0\quad \tau_{yz} = 0$$
(6)
$$\tau_{zx} = \frac{{3F_{f} }}{{2\pi \cdot a^{3} }} \cdot \left[ { - a + \frac{3}{2}z \cdot \tan^{ - 1} (a/z) - \frac{{a \cdot z^{2} }}{{2(a^{2} + z^{2} )}}} \right]$$
(7)
$$\sigma_{\text{TiAl - Ag}} = \frac{\sqrt 2 }{2} \cdot \sqrt {(\sigma_{x} - \sigma_{y} )^{2} + (\sigma_{y} - \sigma_{z} )^{2} + (\sigma_{z} - \sigma_{x} )^{2} + 6 \cdot (\tau_{xy}^{2} + \tau_{yz}^{2} + \tau_{zx}^{2} )}$$
(8)
$${\text{Tkp}} = {\text{Tkw}}_{1} + {\text{Tkm}}\quad {\text{Tkw}}_{1} = {\text{Dtw}} + {\text{Tkw}}_{n}$$
(9)

where mx, ρx, υx, φx, and Ex are named as additive amount, material density, Poisson’s ratio, and Young’s modulus. x is termed as sliver, TiAl alloys, or TiAl-Ag materials. a is contact radius of Hertzian. RSi3N4 is ball radius. Ff is friction force. σTiAl-Ag is von Mises stress. Tkm is a thickness of micro-deformation layer. Dtw and Tkpy are the depth and thickness of wear scars. y is known as the numbers of sliding cycles.

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Li, F., Yang, K., Ma, H. et al. Analysis of In Situ Synthesis and Cross-Sectional Evolution of Wear Scars of TiAl-Ag Composites. J. of Materi Eng and Perform 29, 2514–2523 (2020). https://doi.org/10.1007/s11665-020-04664-6

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