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High-temperature treatment of carbon-carbon composite materials. Communication 2. Thermal stabilization of two-dimensionally reinforced carbon-carbon composite material object geometry

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Refractories and Industrial Ceramics Aims and scope

Billet deformation as a result of high-temperature treatment is observed and measured. A connection is established for material deformation with structure. Deformation of carbon fiber with constant loading in the temperature range from 20 – 2000°C is measured. Temperature ranges are established when there is possibly adjustment of deformation under action of an external load. The load capable of deforming carbon material or restoring initial billet shape is calculated. Groups of carbon materials are proposed for manufacturing shaping mandrels for high-temperature treatment.

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Authors and Affiliations

  1. OAO NIIgrafit, Moscow, Russia

    S. A. Kolesnikov & G. E. Mostovoi

  2. ZAO Éskarb, Moscow, Russia

    S. V. Vasil’chenko

Authors
  1. S. A. Kolesnikov
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  2. G. E. Mostovoi
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  3. S. V. Vasil’chenko
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Translated from Novye Ogneupory, No. 6, pp. 32 – 40, June, 2012.

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Kolesnikov, S.A., Mostovoi, G.E. & Vasil’chenko, S.V. High-temperature treatment of carbon-carbon composite materials. Communication 2. Thermal stabilization of two-dimensionally reinforced carbon-carbon composite material object geometry. Refract Ind Ceram 53, 185–192 (2012). https://doi.org/10.1007/s11148-012-9490-6

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  • DOI: https://doi.org/10.1007/s11148-012-9490-6

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