Long-term ceramic matrix composite for aeroengine

نویسندگان

چکیده

Abstract Three strategies were proposed to prolong the service life of continuous fiber-reinforced silicon carbide ceramic matrix composite (CMC-SiC), which served as thermal-structure components aeroengine at thermo-mechanical-oxygenic coupling environment. As for some with low working stress, improving degree densification was crucial life, and related process approaches recited. If worked under moderate cracking stress ( σ mc ) should be improved far possible. The fiber preform architecture, interface shear strength, residual thermal strengthening associated in this review. Introducing self-healing quite significant appearance microcracks when CMC-SiC more severe environment hundreds hours. damage can sealed by glass phase originating from reaction between oxygen. effective temperature range different first summarized distinguished. structure, composition, preparation systematically designed optimized achieve long duration target.

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ژورنال

عنوان ژورنال: Journal of Advanced Ceramics

سال: 2022

ISSN: ['2227-8508', '2226-4108']

DOI: https://doi.org/10.1007/s40145-022-0611-5