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Thermal conductivity of thermal barrier coatings

  • Aircraft and Rocket Engine Theory
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Abstract

The results of experimental studies of the thermal conductivity coefficient of thermal barrier coatings (TBC) are presented. A technique for its determination is proposed and tested. The data of design evaluation of the TBC thickness distribution along the outline of a cooled turbine blade are given.

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References

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Authors and Affiliations

  1. Tupolev State Technical University, Kazan, Russia

    A. V. Il’inkov, T. A. Il’inkova, A. V. Shchukin, I. V. Basargin & R. R. Valiev

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  1. A. V. Il’inkov
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  2. T. A. Il’inkova
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  3. A. V. Shchukin
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  4. I. V. Basargin
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  5. R. R. Valiev
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Additional information

Original Russian Text © A.V. Il’inkov, T.A. Il’inkova, A.V. Shchukin, I.V.Basargin, R.R. Valiev, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 3, pp. 54–58.

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Il’inkov, A.V., Il’inkova, T.A., Shchukin, A.V. et al. Thermal conductivity of thermal barrier coatings. Russ. Aeronaut. 52, 340–346 (2009). https://doi.org/10.3103/S1068799809030131

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  • DOI: https://doi.org/10.3103/S1068799809030131

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