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国产CCF700-12K碳纤维及其复合材料的性能研究
引用本文:张芳,殷永霞,夏英伟.国产CCF700-12K碳纤维及其复合材料的性能研究[J].宇航材料工艺,2019,49(6):33-35.
作者姓名:张芳  殷永霞  夏英伟
作者单位:北京空间机电研究所,北京 100094
摘    要:文摘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。

关 键 词:CCF700-12K碳纤维  复合材料  性能研究
收稿时间:2019/3/4 0:00:00

Research on the Performance of CCF700-12K Carbon Fibers and Their Composites
ZHANG Fang,YIN Yongxi,XIA Yingwei.Research on the Performance of CCF700-12K Carbon Fibers and Their Composites[J].Aerospace Materials & Technology,2019,49(6):33-35.
Authors:ZHANG Fang  YIN Yongxi  XIA Yingwei
Abstract: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.
Keywords:CCF700-12K carbon fiber  Composite  Performance research
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