Ambient-Temperature Mechanical Response of Alumina–Fluoromica Laminates

Flexural delamination experiments were used to evaluate the mechanical performance of thermochemically stable alumina–fluoromica laminates. Hot-pressed, precracked laminate specimens, in which two MgAl₂O₄-spinel-coated alumina substrates were separated by a thin layer of fluorophlogopite (KMg₃(AlSi₃)O₁₀F₂), were tested in fourpoint flexure at room temperature. Two types of mechanical response were observed: steady-state delamination and brittle failure. Microstructural analysis showed that the delamination response was associated with fine (≤5 μm) grains of the mica; the brittle response occurred when the mica interphase consisted of large (>30 μm) grains that bridged the interphase. The steady-state strain-energy release rate ( G _ss) measured on the graceful, delaminating beams was 9.1 ± 0.4 Jm^–2 for randomly oriented ∼ 5–μm grains but only 2.8 ± 0.2 Jm^–2 for ∼1–μm grains that were aligned with easy-cleavage planes parallel to the laminate interfaces. The results suggested that debonding of the specimens occurred via cleavage of the mica grains. Observation of delamination cracks confirmed this point: propagation occurred within the fluoromica interphase rather than along the spinel/alumina or spinel/fluorophlogopite interfaces. The mechanical feasibility of laminate specimens without the protective spinel coating on the substrate containing the notch was also tested to address an issue related to the preparation of alumina fiber/mica interphase/alumina matrix composites. The delamination response again occurred for the case of a fine-grained mica interphase.