Affiliation of Author(s):民航学院

Journal:APPLIED COMPOSITE MATERIALS

Key Words:Ceramic-matrix composites (CMCs) Airworthiness Strength Oxidation Matrix cracking Interface debonding Fibers failure

Abstract:In this paper, the strength degradation of non-oxide and oxide/oxide fiber-reinforced ceramic-matrix composites (CMCs) subjected to cyclic loading at elevated temperatures in oxidative environments has been investigated. Considering damage mechanisms of matrix cracking, interface debonding, interface wear, interface oxidation and fibers fracture, the composite residual strength model has been established by combining the micro stress field of the damaged composites, the damage models, and the fracture criterion. The relationships between the composite residual strength, fatigue peak stress, interface debonding, fibers failure and cycle number have been established. The effects of peak stress level, initial and steady-state interface shear stress, fiber Weibull modulus and fiber strength, and testing temperature on the degradation of composite strength and fibers failure have been investigated. The evolution of residual strength versus cycle number curves of non-oxide and oxide/oxide CMCs under cyclic loading at elevated temperatures in oxidative environments have been predicted.

ISSN No.:0929-189X

Translation or Not:no

Date of Publication:2018-02-01

Correspondence Author:llb