Change in Interlayer Strength and Fracture Toughness of Carbon-Carbon Composite Material under the Impact of Cyclic Loads


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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.

作者简介

A. Stepashkin

National University of Science and Technology MISiS

Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow

D. Ozherelkov

National University of Science and Technology MISiS

编辑信件的主要联系方式.
Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow

Yu. Sazonov

National University of Science and Technology MISiS

Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow

A. Komissarov

National University of Science and Technology MISiS

Email: d.ozherelkov@gmail.com
俄罗斯联邦, Moscow

V. Mozalev

OAO Rubin Aviation Corporation

Email: d.ozherelkov@gmail.com
俄罗斯联邦, Balashikha

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