摘要
采用缠绕成型的方法制备了F-3A/E复合材料薄壁圆管,通过对比试验研究了树脂配方和增强纤维对管件轴压性能的影响,并对缠绕管件的轴压破坏模式进行研究。同时与F-12/E复合材料进行了对比分析。结果表明:(1)TH-1配方适合F-3A纤维制备复合材料;(2)F-3A/E复合材料缠绕管件轴压承载力比F-12/E复合材料管件的高16.5%~23.9%,且轴压性能具有良好的稳定性;(3)F-3A/E管件轴压破坏形式表现为脆性破坏,而F-12/E管件轴压则表现为韧性破坏模式。
Filament winding process is used to fabricate the F-3A composite tubes, and the effect of resin formu- la and reinforced fiber on axial compression property as well as the failure mode of composite tubes was studied. The results reveal that ( 1 )The TH-1 resin formula shows excellent compatibility for the F-3 A fiber composite, (2)The ax- ial compressive strength of domestic F-3A fiber composite tube is higher than F-12 composite tube up to 16.5% to 23.9% and higher stability, (3)The failure mode of domestic F-3A fiber composite tube appears brittleness while F- 12 fiber composite tube shows toughness.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
2013年第6期31-34,共4页
Aerospace Materials & Technology
关键词
复合材料
缠绕成型
轴压
Composite, Filament winding, Axial compressive