Mechanical Properties Of ZrB2 Ceramics Determined By Two Laboratories

The mechanical properties for zirconium diboride (ZrB2) were measured at two laboratories and compared. Two billets of ZrB2 were prepared by hot-pressing commercial powder. The relative densities of the billets were \u3e99% and with an average grain size of 5.9 ± 4.5 µm. Both laboratories prepared American Society for Testing and Materials (ASTM) C1161 B-bars for strength and ASTM C1421 bars with notch configuration A for fracture toughness. Specimens were machined by diamond grinding at the Army Research Laboratory (ARL) and electrical discharge machining (EDM) at Missouri S&T. Strength bars tested at Missouri S&T were polished to a.25 μm finish while the bars were tested as-ground at ARL. Strengths were 473 ± 79 MPa for the Missouri S&T bars and 438 ± 68 for the ARL bars while the fracture toughness values were 3.9 ±.7 MPa•m1/2 for the Missouri S&T bars and 4.4 ±.6 MPa•m1/2 for the ARL bars. Vickers hardness was measured by both laboratories over a range of indentation loads. The resulting hardness values were on the low end of previously reported values and were quite different from each other especially at indentation loads ≤20N. The study demonstrated that the properties of materials tested to ASTM standards at different laboratories can be compared directly. In addition, strength and fracture toughness were nearly identical for bars prepared by conventional diamond grinding or EDM

Interfacial characteristics and microstructural evolution of ceramics exposed to high temperature sand laden combustion environments

Sand laden combustion environments are a current challenge plaguing ceramic thermal barrier coatings (TBCs) and environmental barrier coatings (EBCs) on metallic and emerging ceramic matrix composite (CMC) turbomachinery components. Exposure of thermal and environmental barrier coatings on ceramic matrix composites to environmental particulate laden deteriorates the ceramic structure via chemical reactions and infiltration into pore structures. The challenge of environmental particulates, collectively referred to as calcium-magnesium-aluminosilicate (CMAS), is expected to be exacerbated in future components that utilize ceramic matric composites (CMCs), since the higher operating temperatures will accelerate particulate melting, infiltration, and diffusion kinetics. This study first presents efforts at ARL to develop sandphobic coatings resistant to CMAS infiltration and deposition. The results of a recent full scale sand ingestion engine test used to evaluate several ARL layered and blended coating compositions are presented. The study also includes the evaluation of interactions of CMAS plasma sprayed environmental barrier coatings and HfO2-Si bond coats on SiC/SiC CMCs in rig simulated engine test conditions. The focus is on the microstructural evolution of the coatings and the interfacial characteristics between the TBCs and EBCs and CMAS. Interfaces between coating constituents are also of interest in order to tailor coatings with superior thermal, structural, and chemical characteristics. Controlled studies on YSZ-based ceramic compacts are also performed in order to gain a more fundamental understanding of the effect of porosity on infiltration kinetics, as well as the nature of interfaces and interfacial products wrought by CMAS infiltration into YSZ ceramic grain boundaries. These model studies on YSZ are conducted by immersing the ceramic compacts into AFRL-02 sand and exposing the system to temperatures of up to 1300 °C. X-ray diffraction, scanning electron microscopy, transmission electron microscopy, electron back scattered diffraction, and focused ion beam (milling and imaging) are utilized for microstructural and interfacial characterization of the CMAS reacted thermal and environmental barrier coating systems