%0 Journal Article %T 国产CCF700-12K碳纤维及其复合材料的性能研究 %T Research on the Performance of CCF700-12K Carbon Fibers and Their Composites %A 张芳 %A 殷永霞 %A 夏英伟 %A ZHANG,Fang %A YIN,Yongxia %A XIA,Yingwei %J 宇航材料工艺 %J Aerospace Materials & Technology %@ 1007-2330 %V 49 %N 6 %D 2019 %P 33-35 %K CCF700-12K碳纤维;复合材料;性能研究 %K CCF700-12K carbon fiber;Composite;Performance research %X 以某重要型号产品高强碳纤维材料国产化为研究背景,开展了CCF700-12K碳纤维及其复合材料力学性能、耐空间环境性能以及热性能研究。结果表明,国产CCF700-12K碳纤维拉伸强度为4 706 MPa,拉伸模量为268 GPa;CCF700-12K/F46复合材料单向板拉伸强度为1 958.8 MPa,拉伸模量为144.79 GPa;CCF700-12K碳纤维的力学性能优异,工艺性能稳定,能够满足复合材料结构工程应用要求。 %X The mechanical properties, survivability of space environment, and thermal properties of CCF700-12K carbon fibers and their composites, are studied based on the localization research of high-strength carbon fiber materials for a major product. The tensile strength of domestic CCF700-12K carbon fibers is 4 706 MPa, with a tensile modulus of 268 GPa. The tensile strength of one-way slabs containing CCF700-12K/F46 composite is 1958.8 MPa, and with a tensile modulus of 144.79 GPa. The results confirm that CCF700-12K carbon fibers show excellent mechanical properties, stable process performance, which can meet the requirements for structrural engineering applications of composite materials. %R 10.12044/j.issn.1007-2330.2019.06.006 %U http://www.yhclgy.com/yhclgy/home %1 JIS Version 3.0.0