摘要
本文研究了大丝束碳纤维（48K）复合材料的常规力学性能及耐湿热性能，并与小丝束碳纤维（T300-3K）复合材料进行了对比，研究结果可为大丝束复合材料在航空器的次承力件或非承力件的应用提供技术基础。
The common mechanical properties and hot-wet properties of large-tow carbon fiber(48K) composite are studied preliminarily in this paper. And they are also compared with that of small-tow carbon fiber (T300-3K) composite. The results can provide the technologies for its future application on non-load-bearing component or subcomponent of aircraft.
出处
《高科技纤维与应用》
CAS
2003年第6期8-11,共4页
Hi-Tech Fiber and Application
关键词
大丝束碳纤维
复合材料
力学性能
耐湿热性
航空器
large-tow carbon fiber(48K)
composite
common mechanical properties
hot-wet properties
