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Microstructure and thermal properties of copper matrix composites reinforced with titanium-coated graphite fibers 被引量:12

Microstructure and thermal properties of copper matrix composites reinforced with titanium-coated graphite fibers
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摘要 Milled form of mesophase pitch-based graphite fibers were coated with a titanium layer using chemical vapor deposition technique and Ti-coated graphite fiber/Cu composites were fabricated by hot-pressing sintering. The composites were characterized with X-ray diffraction, scanning/transmission electron microscopies, and by mea- suring thermal properties, including thermal conductivity and coefficient of thermal expansion (CTE). The results show that the milled fibers are preferentially oriented in a plane perpendicular to the pressing direction, leading to anisotropic thermal properties of the composites. The Ti coating reacted with graphite fiber and formed a continuous and uniform TiC layer. This carbide layer establishes a good metallurgical interracial bonding in the composites, which can improve the thermal properties effectively. When the fiber content ranges from 35 vol% to 50 vol%, the in-plane thermal conductivities of the composites increase from 383 to 407 W.(m.K)-~, and the in-plane CTEs decrease from 9.5 x 10-6 to 6.3 10-6 K-1. Milled form of mesophase pitch-based graphite fibers were coated with a titanium layer using chemical vapor deposition technique and Ti-coated graphite fiber/Cu composites were fabricated by hot-pressing sintering. The composites were characterized with X-ray diffraction, scanning/transmission electron microscopies, and by mea- suring thermal properties, including thermal conductivity and coefficient of thermal expansion (CTE). The results show that the milled fibers are preferentially oriented in a plane perpendicular to the pressing direction, leading to anisotropic thermal properties of the composites. The Ti coating reacted with graphite fiber and formed a continuous and uniform TiC layer. This carbide layer establishes a good metallurgical interracial bonding in the composites, which can improve the thermal properties effectively. When the fiber content ranges from 35 vol% to 50 vol%, the in-plane thermal conductivities of the composites increase from 383 to 407 W.(m.K)-~, and the in-plane CTEs decrease from 9.5 x 10-6 to 6.3 10-6 K-1.
出处 《Rare Metals》 SCIE EI CAS CSCD 2013年第1期75-80,共6页 稀有金属(英文版)
基金 financially supported by the National Natural Science Foundation of China(No.51274040) the Fundamental Research Funds for the Central Universities(FRF-TP-10-003B)
关键词 Metal matrix composites Titanium coating MICROSTRUCTURE Thermal conductivity Coefficient of thermal expansion Metal matrix composites Titanium coating Microstructure Thermal conductivity Coefficient of thermal expansion
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