Skip to main content
SpringerLink
Log in

Experimental and Numerical Study of the Formation of Thermophysical Characteristics of Carbon Composite Materials. Part 2. Numerical Simulation of Operability of a Refractory Product Made of Carbon Composite Material

  • Published:
Refractories and Industrial Ceramics Aims and scope

A heating of a carbon-made product and thermophysical properties of a carbon material in the temperature range from 300 to 2,500 K were studied. A discrete-heterogeneous mechanism of heating the surface of a multi-dimensionally reinforced carbon-carbon composite material (CCCM) subject to accelerated heating was revealed. Based on the results of testing carbon materials in the temperature range from 300 to 3,000 K, a numerical stress analysis of the product was performed, in which the arising stress condition was considered to be resultant from constraining the deformation of the heated parts of the product by relatively cold fragments. The safety factor levels were found for different parts of the product. It was shown that an additional increase in thermal strength as part of the combined definition of thermal resistance of CCCM products is associated with high thermal conductivity of 1D-reinforced rods of material structure.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

Fig. 1.
Fig. 2.
Fig. 3.
Fig. 4.
Fig. 5.
Fig. 6.
Fig. 7.

Similar content being viewed by others

References

  1. C. W. Ohlhorst, W. L. Vauhn, P. O. Ransone, and H.-T. Tsou, Thermal conductivity database of various structural carbon-carbon composite materials, Langley Research Center, Hampton, Virginia (1997), http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.82.682&rep=rep1&type=pdf.

  2. Ch. Pradere, Thermal and thermomechanical characterization of carbon and ceramic fibers at very high temperature, Ecole Natiionale Superiered’Arts et Metiers Centre de Bordeaux (2004), https://pastel.archives-ouvertes.fr/file/index/docid/500111/filename/ThesePradere.pdf.

  3. W.-J. Li, H.-M. Huang, Y.-M. Hu, “Thermochemical ablation of carbon/carbon composites with non-linear thermal conductivity,” Thermal Science, 18(5), 1625 – 1629 (2014), http://www.doiserbia.nb.rs/img/doi/0354-9836/2014/0354-98361405625L.pdf.

    Article  CAS  Google Scholar 

  4. J. Lachaud, Y. Aspa, G. L. Vignoles, and J.-M. Goyheneche, 3D modeling of thermochemical ablation in carbon-based materials: effect of anisotropy on surface roughness onset, http://jeanlachaud.com/research/lachaud-ISMSE2006.pdf.

  5. M. Grujicic, C. L. Zhao, E. C. Dusel, et al., “Computational analysis of the thermal conductivity of the carbon–carbon composite materials,” J. Mater. Sci., 41(24), 8244 – 8256 (2006), https://link.springer.com/article/10.1007/s10853-006-1003-x.

    Article  CAS  Google Scholar 

  6. Patent RU249896, G. A. Krechka, V. D. Kleymenov, and V. N. Savelyev, Reinforcing frame made of carbon-carbon composite material, Application No. 2011127880/02, appl. date: July 06, 2011, publ. date: Nov. 20, 2013, Bul. No. 32. http://www.findpatent.ru/patent/249/2498962.html.

  7. O. N. Dementyev, G. F. Kostin, N. N. Tikhonov, and B. M. Tyulkin, “Assessment of the effect of mechanically carried away particles of the thermal protection of hypersonic aircraft on stability of the boundary layer flow and heat transfer,” Vestn. Chelyab. Gos. Univ., Fizika, 13, No. 14(268), 9 – 13 (2012), https://cyberleninka.ru/article/n/otsenka-vliyaniya-mehanicheskiunosimyhchastits- teplovoy-zaschity-giperzvukovyh-letatelnyhapparatov-na-ustoychivost-techeniya-v.

  8. I. A. Izhenbin, Tomographic system based on “Orel” tomograph for performing tomographic scanning of the samples of 39p7.001 and 4KMC-L type carbon-carbon composite materials, Electronic Scientific Archive of the Tomsk Polytechnic University (2016), http://earchive.tpu.ru/bitstream/11683/28151/1/TPU174557.pdf.

  9. H.-B. Shi, M Tang, B. Gao, and J.-M. Su, “Effect of graphitization parameters on the residual stress in 4D carbon fiber/carbon composites,” New Carbon Materials, 26(4), 287 – 288 (2011), 10. 1016/S1872-5805(11)60082-6. https://www.sciencedirect.com/journal/new-carbon-materials/vol/26/issue/4.

    Article  CAS  Google Scholar 

  10. S. A. Kolesnikov, M. Yu. Bamborin, V. A. Vorontsov, et al., “Formation of carbon-carbon composite material thermal conductivity standards,” Refract. Ind. Ceram., 58(1), 94 – 102 (2017)

    Article  CAS  Google Scholar 

  11. S. A. Kolesnikov, L. V. Kim, V. A. Vorontsov, Study of thermophysical property formation of spatially reinforced carbon- carbon composite material, Refract. Ind. Ceram., 58(4), 439 – 449 (2017).

    Article  CAS  Google Scholar 

  12. The United Nations, A/AC.105/C.1/L.312, Principles concerning the use of nuclear power sources in outer space, adopted by the General Assembly Resolution 47/68 dated December 14 (1992), http://www.un.org/ru/documents/decl_conv/conventions/outerspace_nucpower.shtml.

  13. A. K. Protsenko and S. A. Kolesnikov, Development of carbon- carbon technologies and their development potential, In: “55 years of the Research Institute of Graphite-based Structural Materials”, Nauchnye Tekhnologii, Moscow (2015), http://www.niigrafit.ru/nauka-i-obrazovanie/sbornik.pdf.

  14. V. V. Khartov, M. B. Martynov, A. V. Lukyanchikov, and S. N. Aleksashkin, “Design concept of the landing module “ExoMars-2018,” being developed by the NPO named after S. A. Lavochkin,” Vestn. NPO named after S. A. Lavochkin, No. 2 (23), 5 – 12 (2014).

  15. Yu. V. Polezhaev and F. B. Yuryevich, Thermal Protection [in Russian], Ed. by A. V. Lykov, Energiya, Moscow (1976).

  16. Thermal unit of the “Angel” radioactive thermoelectric generator, https://helpiks.org/6-77726.html.

  17. R. Upadhyay, P. T. Bauman, R. Stogner, et al., Steady-state ablation model coupling with hypersonic flow, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 4 – 7 (2010), pp. 1 – 10. https://arc.aiaa.org/doi/10.2514/6.2010-1176.

  18. Multi-dimensional reinforced carbon-carbon composites. http://niigrafit.ru/produktsiya/kompozity.php.

  19. L. M. Manocha, “High performance carbon-carbon composites,” Sadhana, 28, parts 1/2, 349 – 358 (2003), http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.582.8031&rep=rep1&type=pdf.

  20. V. L. Salich, “Design of the chamber of the 100 N propulsion oxygen-hydrogen rocket engine based on numerical simulation of intrachamber processes,” Vestn. UGATU, 18, 4 (65), 20 – 26 (2014), http://journal.ugatu.ac.ru.

  21. V. P. Sosedov, V. G. Nagornyi, A. S. Kotosonov, et al., Properties of Graphite-based Structural Materials [in Russian], Reference guide, Metallurgiya, Moscow (1975).

  22. GOST 9.910–88, Method of testing for thermal fatigue in gas flows using wedge-shaped samples, http://echemistry.ru/assets/files/literatura/gost/gost-9.910-88-edinaya-sistema-zashhity-ot-korrozii-istareniya-metally-splavypokrytiyazharostojkiemetodispytaniya-na-termoustalost-v-gazovyh-potokah-naklinovidnyh-obrazcah.pdf.

  23. S. P. Timoshenko and J. Goodyear, The Theory of Elasticity, 2nd ed., transl. from English, ed. by G. S. Shapiro, Nauka, Glavn. Red. Fiz. Mat. Lit., Moscow (1979).

  24. A. P. Karpov and G. Ye. Mostovoi, “High-temperature mechanical properties of carbon and carbon-carbon composite materials,” Perspect. Mater., No. 3, 13 – 21 (2015).

  25. L. M. Akselrod and A. V. Zabolotskii, “Mathematical simulation of fracturing of the lining of metallurgical equipment under thermal shock conditions,” Sborn. Nauchn. Idei, Sovr. Nauka, No. 2 (4), 165 – 169 (2010), http://modern.science.triacon.org/ru/issues/2010/files/papers/2/165-169.pdf.

  26. S. A. Kolesnikov, G. E. Mostovoi, S. V. Vasil’chenko, et al., “High-temperature treatment of carbon-carbon composite materials. Part 2. Thermal stabilization of two-dimensionally reinforced carbon-carbon composite material object geometry,” Refract. Ind. Ceram., 53(3), 185 – 192 (2012).

    Article  CAS  Google Scholar 

Download references

Author information

Authors and Affiliations

  1. JSC “NIIGrafit”,, Moscow, Russia

    S. A. Kolesnikov, L. V. Kim & V. R. Dudin

Authors
  1. S. A. Kolesnikov
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. L. V. Kim
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. V. R. Dudin
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to S. A. Kolesnikov.

Additional information

Translated from Novye Ogneupory, No. 8, August, 2019.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Kolesnikov, S.A., Kim, L.V. & Dudin, V.R. Experimental and Numerical Study of the Formation of Thermophysical Characteristics of Carbon Composite Materials. Part 2. Numerical Simulation of Operability of a Refractory Product Made of Carbon Composite Material. Refract Ind Ceram 60, 336–345 (2019). https://doi.org/10.1007/s11148-019-00363-5

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11148-019-00363-5

Keywords

Search

Navigation