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Microstructures and Toughening of TiC-TiB2Ceramic Composites with Cr-Based Alloy Phase Prepared by Combustion Synthesis in High-Gravity Field

机译:重力场中燃烧合成制备的CrC合金相的TiC-TiB2陶瓷复合材料的组织与增韧

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Micro-nanocrystalline microstructures which are characterized by TiB2platelets of the average thickness close to or smaller than 1 μm can be achieved in nearly full-density solidified TiC-TiB2ceramic composites with Cr-based alloy phases by combustion synthesis in ultra-high gravity field of 2500 g. The filler phases in ceramic composites are actually Cr-based alloy with a little solidified solution of Ni atoms and Al atoms. The hardness, flexural strength, and fracture toughness of the materials are 18.5 ± 1.5 GPa, 650 ± 35 MPa, and 16.5 ± 1.5 MPa⋅m0.5, respectively. The improved fracture toughness of TiC-TiB2ceramic composites results from crack deflection, crack bridging, and pull-out by a large number of fine TiB2platelets and plastic deformation with some Cr-based alloy phases.
机译:通过在2500的超高重力场中燃烧合成,可以在具有Cr基合金相的几乎全密度凝固TiC-TiB2陶瓷复合材料中,实现以平均厚度接近或小于1μm的TiB2片为特征的微纳米晶体微结构。 G。陶瓷复合材料中的填充相实际上是基于Cr的合金,其中含有少量的Ni原子和Al原子固化溶液。材料的硬度,弯曲强度和断裂韧性分别为18.5±1.5 GPa,650±35 MPa和16.5±1.5 MPa·m0.5。 TiC-TiB2陶瓷复合材料的断裂韧性得到改善,这是由于大量细小的TiB2血小板产生的裂纹偏转,裂纹桥接和拉出以及某些Cr基合金相的塑性变形所致。

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