Change in Interlayer Strength and Fracture Toughness of Carbon-Carbon Composite Material under the Impact of Cyclic Loads
- Авторы: Stepashkin A.A.1, Ozherelkov D.Y.1, Sazonov Y.B.1, Komissarov A.A.1, Mozalev V.V.2
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Учреждения:
- National University of Science and Technology MISiS
- OAO Rubin Aviation Corporation
- Выпуск: Том 10, № 1 (2019)
- Страницы: 155-161
- Раздел: Article
- URL: https://journals.rcsi.science/2075-1133/article/view/207799
- DOI: https://doi.org/10.1134/S2075113319010301
- ID: 207799
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Аннотация
The effect of low-cycle fatigue loading on interlayer strength and fracture toughness of discretely reinforced carbon-carbon composite material (CCCM) for friction use is studied. The material demonstrates good resistance to fatigue loads. In the described mechanisms for increasing CCCM fracture toughness after applying fatigue load, the fiber–matrix interface plays a key part. The dependences of CCCM fracture toughness and interlayer strength on the fatigue loading parameters are determined.
Об авторах
A. Stepashkin
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
Россия, Moscow
D. Ozherelkov
National University of Science and Technology MISiS
Автор, ответственный за переписку.
Email: d.ozherelkov@gmail.com
Россия, Moscow
Yu. Sazonov
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
Россия, Moscow
A. Komissarov
National University of Science and Technology MISiS
Email: d.ozherelkov@gmail.com
Россия, Moscow
V. Mozalev
OAO Rubin Aviation Corporation
Email: d.ozherelkov@gmail.com
Россия, Balashikha
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