首页|SiCf/Ti65复合材料的拉伸行为研究

SiCf/Ti65复合材料的拉伸行为研究

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采用磁控溅射先驱丝法结合热等静压工艺制备SiCf/Ti65 复合材料,研究了SiCf/Ti65 复合材料室温、高温拉伸行为,揭示了SiCf/Ti65 复合材料拉伸断裂机制.研究结果表明:SiCf/Ti65 复合材料的室温、高温抗拉强度相比于Ti65 合金的抗拉强度分别提升 29%和 164%,验证了复合材料的增强效果.SiCf/Ti65 复合材料的室温拉伸断裂机制为反应层断裂、纤维/基体界面脱粘、基体脆性断裂、纤维断裂、包套韧性断裂;高温断裂机制为反应层断裂、纤维/基体界面脱粘、纤维断裂、W/SiC界面脱粘、基体和包套韧性断裂.
Study on Tensile Behavior of SiCf/Ti65 Composites
SiCf/Ti65 composite was prepared by magnetron sputtering precursor wire method combined with thermal isostatic pressure process,the tensile behavior of SiCf/Ti65 composite chamber at room temperature and high temperature was studied,and the tensile fracture mechanism of the composite was reveled.The results show that the room temperature and high temperature tensile strengths of the composite are 29%and 164%higher than those of Ti65 alloy,respectively.The enhancement effect of the composite material is verified.The room temperature tensile fracture mechanism of the composite is reaction layer fracture,fiber/matrix interface debond,matrix brittle fracture,fiber fracture and sheath toughness fracture;the high temperature fracture mechanism is reaction layer fracture,fiber/matrix interface debond,fiber fracture,W/SiC interface deadhesion,matrix and sheath toughness fracture.

compositetensile propertiesSiC fiberfracture mechanism

孟凡玲、刘范凯、杨丽娜、王玉敏

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沈阳理工大学 材料科学与工程学院,辽宁 沈阳 110159

中国科学院金属研究所轻质高强材料研究部,辽宁沈阳 110016

复合材料 拉伸性能 SiC纤维 断裂机制

国家科技重大专项项目

HT-J2019-VI-0007-0121

2024

热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
年,卷(期):2024.53(12)
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