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Effect of Heat Treatment and Deformation on the Grain Size and Mechanical Properties of Duralumin-Type Alloys

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Abstract

Mechanical properties and the grain size of alloy D16ch and 1163 used for the sheeting of aircraft fuselages after 21% and 74% deformation and different kinds of heat treatment are studied. The effect of the modes of intermediate, preliminary, and final annealing operations on the grain size is determined. Recommendations are given for providing a small grain size.

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REFERENCES

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Authors and Affiliations

  1. All-Russia Institute of Aircraft Materials (VIAM), Moscow, Russia

    I. N. Fridlyander, V. V. Berstenev, E. A. Tkachenko, G. M. Goloviznina, L. V. Latushkina & L. P. Lantsova

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  1. I. N. Fridlyander
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  2. V. V. Berstenev
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  3. E. A. Tkachenko
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  4. G. M. Goloviznina
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  5. L. V. Latushkina
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  6. L. P. Lantsova
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Fridlyander, I.N., Berstenev, V.V., Tkachenko, E.A. et al. Effect of Heat Treatment and Deformation on the Grain Size and Mechanical Properties of Duralumin-Type Alloys. Metal Science and Heat Treatment 45, 239–245 (2003). https://doi.org/10.1023/A:1027316015223

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  • DOI: https://doi.org/10.1023/A:1027316015223

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