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Effect of Structure on the Critical Stresses and Strains in Titanium Nickelide-Based Alloys

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Abstract

The effect of the test temperature on the mechanical behavior of a titanium nickelide–based alloy is considered. The behavior of a titanium nickelide–based alloy is shown to be substantially dependent on the level of stresses and strains of the material. The critical stresses are determined by the solid-solution, grain-boundary, strain, and precipitation hardening mechanisms. The maximum critical strain can be achieved by a combination of several hardening mechanisms.

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ACKNOWLEDGMENTS

This work was performed on the equipment of the Resource Collective Use Center “Aerospace Materials and Technologies” of the Moscow Aviation Institute.

Funding

This work was carried out in the framework of state assignment to institutes of higher education no. 11.7449.2017/64.

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), 125993, Moscow, Russia

    M. Yu. Kollerov, D. E. Gusev, M. B. Afonina & R. E. Vinogradov

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  1. M. Yu. Kollerov
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  2. D. E. Gusev
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  3. M. B. Afonina
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  4. R. E. Vinogradov
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Corresponding author

Correspondence to M. Yu. Kollerov.

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Translated by Yu. Ryzhkov

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Kollerov, M.Y., Gusev, D.E., Afonina, M.B. et al. Effect of Structure on the Critical Stresses and Strains in Titanium Nickelide-Based Alloys. Russ. Metall. 2020, 760–766 (2020). https://doi.org/10.1134/S0036029520070095

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  • DOI: https://doi.org/10.1134/S0036029520070095

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