Re-defining failure envelopes for silicon carbide composites based on damage process analysis by acoustic emission

A silicon carbide fiber reinforced silicon carbide matrix (SiC/SiC) composite is a promising candidate for a fusion DEMO blanket. To develop design codes in practical use of them, strength anisotropy is an important issue to be clarified and therefore this study aimed to evaluate the failure behavior of the SiC/SiC composites to provide a strength map. For this purpose, detailed tensile, compressive and in-plane shear failure behaviors were evaluated by the acoustic emission (AE) technique for a plain–weave (P/W) chemically vapor-infiltration (CVI) SiC/SiC composite. The AE results distinguished damage accumulation processes by separately discussing localized variations of power within a time series by wavelet analysis. Of particular emphasis is that matrix cracking occurred prior to the proportional limit stress (PLS) by both tensile and compressive tests. This is because the rough-surface of SiC fibers resulted in the strong frictional stress at the fiber/matrix (F/M) interface, showing linearity in the stress–strain curve beyond the actual matrix cracking stress (i.e., possibly no sliding of the fibers at the F/M interface). In this paper, an updated failure envelope was provided by referring the true matrix cracking stresses as more realistic and reasonable failure criteria.