Crack propagation in metal matrix composites system Ti–SiC under cyclic loads (review)

Serpova V.M., Sidorov D.V., Shavnev A.A., Kurbatkina E.I., Krasnov E.I.
UDC
669.018.95
DOI
10.18577/2307-6046-2020-0-9-52-60
Article PDF (Russian) (823.89 KB)
How to cite
Serpova V.M., Sidorov D.V., Shavnev A.A., Kurbatkina E.I., Krasnov E.I. Crack propagation in metal matrix composites system Ti–SiC under cyclic loads (review) // Proceedings of VIAM. 2020. No. 9. DOI: 10.18577/2307-6046-2020-0-9-52-60. URL: https://test.viam.ru/en/journal/2020/9/6
Keywords
metal matrix composite, silicon carbide, fiber, titanium matrix composites, fatigue.
Abstract

The article presents a literature review of the features of crack development in fibrous metal composite materials (MCMs) system Ti–SiC under cyclic loads. The mechanisms that provide resistance to crack development and factors affecting the process of crack growth in fibrous MCMs system Ti–SiC are presented. The influence of temperature, frequency, and medium on the development velocity of a crack in fibrous MCMs system Ti–SiC under the action of cyclic loads is considered. In conclusion, of the review, conclusions are drawn and it is shown that the development of a fatigue crack and its resistance to growth in MCMs system Ti–SiC are associated with the structural features of the material.

Reference list
  1. Kablov E.N. Innovative developments of FSUE «VIAM» SSC of RF on realization of «Strategic directions of the development of materials and technologies of their processing for the period until 2030». Aviacionnye materialy i tehnologii, 2015, no. 1 (34), pp. 3–33. DOI: 10.18577/2071-9140-2015-0-1-3-33.
  2. Kablov E.N., Valueva M.I., I.V. Zelenina, Khmelnitskiy V.V., Aleksashin V.M. Carbon plastics based on benzoxazine oligomers – perspective materials. Trudy VIAM, 2020, no. 1, paper no. 07. Available at: http://www.viam-works.ru (accessed: June 2, 2020). DOI: 10.18577/2307-6046-2020-0-1-68-77.
  3. Kablov E.N. What to make the future of? New generation materials, technologies for their creation and processing - the basis of innovations. Krylya Rodiny, 2016, no. 5, pp. 8–18.
  4. Grashchenkov D.V. Strategy of development of non-metallic materials, metal composite materials and heat-shielding. Aviacionnye materialy i tehnologii, 2017, No. S, pp. 264–271. DOI: 10.18577/2071-9140-2017-0-S-264-271.
  5. Volkov A.M., Vostrikov A.V. Low-cycle fatigue resistance of PM Ni-base superalloys (review). Aviacionnye materialy i tehnologii, 2016, no. S1, pp. 74–79. DOI: 10.18577/2071-9140-2016-0-S1-74-79.
  6. Antipov V.V. Prospects for development of aluminium, magnesium and titanium alloys for aerospace engineering. Aviacionnye materialy i tehnologii, 2017, no. S, pp. 186–194. DOI: 10.18577/2107-9140-2017-0-S-186-194.
  7. Sidorov D.V., Serpova V.M., Shavnev A.A. Manufacturing methods and fields of application of high-strength fibrous composite materials reinforced with silicon carbide core fiber. Vse materialy. Entsiklopedicheskiy spravochnik, 2018, no. 3, pp. 15–22.
  8. Chawla N., Chawla K.K. Metal Matrix Composites. New York: Springer Sience+Business Media, Inc., 2006, pp. 351–379.
  9. Vassel A. Continuous fibre reinforced titanium and aluminium composites: a comparison. Materials Science and Engineering, 1999, vol. A263, pp. 305–313. DOI: 10.1016/s0921-5093(98)01161-7.
  10. Moongkhamklang P., Elzey D., Wadley H. Titanium matrix composite lattice structures. Composites, 2008, vol. A39, pp. 176–187. DOI: 10.1016/j.compositesa.2007.11.007.
  11. Doel T.J.A., Cardona D.C., Bowent P. Fatigue crack growth in selectively reinforced titanium metal matrix composites. International Journal of Fatigue, 1998, vol. 20, is. 1, pp. 35–50. DOI: 10.1016/s0142-1123(97)00093-5.
  12. Hayat M.D., Singh H., He Z., Cao P. Titatium metal matrix composites: An overiew. Composites. Part A: Applied Science and Manufacturing, 2019, vol. 121, pp. 418–438. DOI: 10.1016/j.compositesa.2019.04.005.
  13. Ivanov D.A., Sitnikov A.I., Shlyapin S.D. Dispersion-strengthened, fibrous and layered inorganic composite materials. Moscow: MATI, 2009, 306 p.
  14. Gupta V., Martinez D. Energy Criterion for crack deflection at an interface between two orthotropic media. Journal of the Mechanics and Physics of Solids, 1994, vol. 42, no. 8, pp. 1247–1271. DOI: 10.1016/0022-5096(94)90034-5.
  15. He M.Y., Evans A.G., Hutchinson J.W. Crack Deflection at an Interface Between Dissimilar Elastic Materials: Role of Residual Stresses. International Journal of Solids and Structures, 1994, vol. 31, no. 24, pp. 3443–3455. DOI: 10.1016/0020-7683(94)90025-6.
  16. Cook J., Gordon J.E. A Mechanism for the Control of Crack Propagation in All-Brittle Systems. Proceedings of the Royal Society of London. Series A: Mathematical and Physical Sciences, 1964, vol. 282, no. 1391, pp. 508–520. DOI: 10.1098/rspa.1964.0248.
  17. Fibrous composite materials. Ed. M.Kh. Shorshorov. Moscow: Mashinostroenie, 1983, 320 p.
  18. Zheng D., Ghonem H. Fatigue crack growth of SM-1240/TIMETAL-21S metal matrix composites at elevated temperatures. Metallurgical and Materials Transactions A, 1995, vol. 26A, pp. 2469–2478. DOI: 10.1007/bf02671261.
  19. Barney C., Cardona D., Bowen P. Fatigue crack growth resistance from unbridged defects in continuous fibre reinforced metal matrix composites. International Journal of Fatigue, 1998, vol. 20, no. 4, pp. 279–289. DOI: 10.1016/s0142-1123(97)00127-8.
  20. Ibbotson A.R., Bowen P., Beevers C.J. Cyclic fatigue resistance of fiber reinforced titanium metal matrix composites at ambient and elevated temperature. Proceedings of the 70th Titanium Conference, 1992, pp. 2601–2608.
  21. Davidson D.L. The micromechanics of fatigue crack growth at 25 °C in Ti–6Al–4V reinforced with SCS-6 fibers. Metallurgical Transactions A, 1992, vol. 23, no. 3, pp. 865–879. DOI: 10.1007/bf02675564.
  22. McMeeking R.M., Evans A.G. Matrix fatigue cracking in fiber composites. Mechanics of Materials, 1990, vol. 9, no. 3, pp. 217–227. DOI: 10.1016/0167-6636(90)90004-y.
  23. Cotterill P.J., Bowen P. Fatigue crack growth in a fibre-reinforced titanium MMC at ambient and elevated temperatures. Composites, 1993, vol. 24, no. 3, pp. 214–221. DOI: 10.1016/0010-4361(93)90166-6.
  24. Sinclair R., Preuss M., Maire E. et al. The effect of fibre fractures in the bridging zone of fatigue cracked Ti–6Al–4V/SiC fibre composites. Acta Materialia, 2004, vol. 52, no. 6, pp. 1423–1438. DOI: 10.1016/j.actamat.2003.11.024.
  25. Brisset F., Bowen P. Fatigue crack growth in fibre reinforced titanium MMC laminate at room and elevated temperatures. Materials Science and Technology, 1998, vol. 14, no. 7, pp. 651–657. DOI: 10.1179/mst.1998.14.7.651.
  26. Brett R. The influence of loading levels, temperature and environment on fibre failure during the fatigue of an SiC fibre reinforced Ti-MMC. International Journal of Fatigue, 1996, vol. 18, no. 1, pp. 1–8. DOI: 10.1016/0142-1123(95)00080-1.
  27. Stanley H., Dear M., Doel T.J.A., Bowen P. Fatigue Crack Growth Resistance of Titanium Metal Matrix Composites. Metal-Matrix Composites Innovations, Advances and Applications. TMS, 2018, pp. 87–102. DOI: 10.1007/978-3-319-72853-7 7.