上海大学学报(自然科学版)
上海大學學報(自然科學版)
상해대학학보(자연과학판)
JOURNAL OF SHANGHAI UNIVERSITY (NATURAL SCIENCE EDITION)
2014年
1期
75-82
,共8页
周计明%郑武强%齐乐华%马玉钦
週計明%鄭武彊%齊樂華%馬玉欽
주계명%정무강%제악화%마옥흠
真空吸渗挤压%二维正交铺层Cf/Al复合材料%压缩性能%失效机制
真空吸滲擠壓%二維正交鋪層Cf/Al複閤材料%壓縮性能%失效機製
진공흡삼제압%이유정교포층Cf/Al복합재료%압축성능%실효궤제
extrusion directly following vacuum pressure infiltration technique%2D cross-ply Cf/Al composite%compressive property%failure mechanism
采用真空吸渗挤压技术制备了二维正交铺层碳纤维增强铝基(2D-Cf/Al)复合材料,研究了室温下2D-Cf/Al复合材料沿不同方向的压缩性能及其失效行为.研究结果表明:利用真空吸渗挤压技术制备的复合材料的浸渗质量良好,微观组织致密,基体铝合金和纤维分布均匀,无明显缺陷存在;沿垂直于纤维铺层方向的压缩屈服强度约为平行方向的2.5倍,比基体铝合金的压缩强度提高了57%.复合材料的压缩破坏机制与纤维铺层方向密切相关:当压缩载荷垂直于纤维铺层方向时,主要以剪切失效为主;当压缩载荷平行于纤维铺层方向时,主要以界面脱粘和纤维弯折失效为主.
採用真空吸滲擠壓技術製備瞭二維正交鋪層碳纖維增彊鋁基(2D-Cf/Al)複閤材料,研究瞭室溫下2D-Cf/Al複閤材料沿不同方嚮的壓縮性能及其失效行為.研究結果錶明:利用真空吸滲擠壓技術製備的複閤材料的浸滲質量良好,微觀組織緻密,基體鋁閤金和纖維分佈均勻,無明顯缺陷存在;沿垂直于纖維鋪層方嚮的壓縮屈服彊度約為平行方嚮的2.5倍,比基體鋁閤金的壓縮彊度提高瞭57%.複閤材料的壓縮破壞機製與纖維鋪層方嚮密切相關:噹壓縮載荷垂直于纖維鋪層方嚮時,主要以剪切失效為主;噹壓縮載荷平行于纖維鋪層方嚮時,主要以界麵脫粘和纖維彎摺失效為主.
채용진공흡삼제압기술제비료이유정교포층탄섬유증강려기(2D-Cf/Al)복합재료,연구료실온하2D-Cf/Al복합재료연불동방향적압축성능급기실효행위.연구결과표명:이용진공흡삼제압기술제비적복합재료적침삼질량량호,미관조직치밀,기체려합금화섬유분포균균,무명현결함존재;연수직우섬유포층방향적압축굴복강도약위평행방향적2.5배,비기체려합금적압축강도제고료57%.복합재료적압축파배궤제여섬유포층방향밀절상관:당압축재하수직우섬유포층방향시,주요이전절실효위주;당압축재하평행우섬유포층방향시,주요이계면탈점화섬유만절실효위주.
2D cross-ply carbon fiber reinforced aluminum matrix composites were fabri-cated by extrusion directly following vacuum pressure infiltration. The compressive prop-erty and failure mechanism of 2D-Cf/Al composites were investigated at room temperature by applying loadings along different directions with respect to the fiber layer. The results show that the composite with ideal infiltration quality and dense microstructure could be fabricated successfully by extrusion directly following vacuum pressure infiltration the aluminum alloy and fibers are evenly distributed, and seldom defects can be found in com-posite. The compression yield strength perpendicular to the fiber layer is almost 2.5 times as that parallel to the fiber layer. Further analysis shows that the different properties are caused by different failure mechanisms. When the loading direction is perpendicular to the fiber layer, composites failure is mainly caused by shear fracture. When the loading direction is parallel to the direction of fiber, interface debonding and fiber bending failure are the main failure mechanism.