Densification behavior, microstructure, and mechanical properties of zirconium diboride (ZrB 2 ) ceramics modified with a complex Zr/Si/O-based additive were studied. ZrB 2 ceramics with 5-20 vol.% additions of Zr/Si/O-based additive were densified to >95% relative density at temperatures as low as 1400 • C by hotpressing. Improved densification behavior of ZrB 2 was observed with increasing additive content. The most effective additive amount for densification was 20 vol.%, hot-pressed at 1400 • C (∼98% relative density). Microstructural analysis revealed up to 7 vol.% of residual second phases in the final ceramics. Improved densification behavior was attributed to ductility of the silicide phase, liquid phase formation at the hot-pressing temperatures, silicon wetting of ZrB 2 particles, and reactions of surface oxides. Room temperature strength ranged from 390 to 750 MPa and elastic modulus ranged from 440 to 490 GPa. Vickers hardness ranged from 15 to 16 GPa, and indentation fracture toughness was between 4.0 and 4.3 MPa⋅m 1/2 . The most effective additive amount was 7.5 vol.%, which resulted in high relative density after hot-pressing at 1600 • C and the best combination of mechanical properties.
K E Y W O R D Sdensification, mechanical properties, microstructure, ZrB 2 , ZrSi 2
INTRODUCTIONZirconium diboride (ZrB 2 ) is one of several materials considered to be ultra-high temperature ceramics (UHTCs). These materials have extremely high melting points (>3000 • C) and are useful for applications including molten metal crucibles, 1,2 high temperature electrodes, 1,3 cutting tools, 4,5 and leading edges for hypersonic aerospace vehicles. [6][7][8][9] The high degree of metallic bonding character, 10 the relatively high thermal conductivity (up to 145 W⋅[m⋅K] −1 ) 11 and low electrical resistivity (as low as 7.8 μΩ⋅cm) 12 of borides set them apart from other UHTC materials, specifically transition metal carbides and nitrides. Combined with their high thermal conductivity, extremely high melting temperature (>3000 • C), and high strength (>500 MPa), ZrB 2 -based ceramics are attractive candidates for ultra-high temperature aerospace applications. [11][12][13][14][15] Advancements to mechanical reliability in these materials will require reinforcing phases to enable graceful failure and improve damage tolerance. Previous studies have shown that addition of SiC whiskers, or shortchopped SiC fibers, improve the fracture toughness of ZrB 2 . [16][17][18][19] Toughening in these materials is achieved by 2224