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/双轴预拉载荷对碳纤维复合材料高速冲击性能的影响研究
引用本文:尹昰凯,陈伟,刘璐璐,赵振华,罗刚.单/双轴预拉载荷对碳纤维复合材料高速冲击性能的影响研究[J].推进技术,2022,43(6):295-301.
作者姓名:尹昰凯  陈伟  刘璐璐  赵振华  罗刚
作者单位:1.南京航空航天大学 能源与动力学院 航空发动机热环境与热结构工业和信息化部重点实验室, 江苏 南京 210016;2.南京航空航天大学 能源与动力学院 机械结构力学及控制国家重点实验室,江苏 南京 210016
基金项目:国家科技重大专项(2017-Ⅳ-0006-0043);国家自然科学基金(51975279)。
摘    要:针对发动机工作时受预载荷的叶片受到外物冲击的情况,设计一种面内单轴及双轴预加载装置,开展单轴与双轴不同大小预拉载荷下碳纤维/环氧树脂复合材料(T700/TDE-86)的高速冲击试验,探究预拉载荷对复合材料抗冲击性能的影响,并结合超声C扫描分析预拉载荷对损伤面积的影响。结果表明:面内初始载荷对复合材料层合板抗冲击性能和分层损伤面积有显著影响;预拉载荷会提高靶板的抗弯刚度,减少靶板吸收的能量,减小弹道极限,且在双轴预拉情况下更明显;弹体击穿靶板后分层损伤面积几乎不变,而预拉载荷会减小分层损伤面积,且在双轴预拉情况下更明显。

关 键 词:预加载  复合材料  高速冲击  分层损伤  能量吸收  弹道极限
收稿时间:2020/9/17 0:00:00
修稿时间:2021/3/31 0:00:00

Effects of Uniaxial/Biaxial Pretension Load on High-Speed Impact Properties of Carbon Fiber Composites
YIN Shi-kai,CHEN Wei,LIU Lu-lu,ZHAO Zhen-hu,LUO Gang.Effects of Uniaxial/Biaxial Pretension Load on High-Speed Impact Properties of Carbon Fiber Composites[J].Journal of Propulsion Technology,2022,43(6):295-301.
Authors:YIN Shi-kai  CHEN Wei  LIU Lu-lu  ZHAO Zhen-hu  LUO Gang
Institution:Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Infor-mation Technology,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,,Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Infor-mation Technology,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,,
Abstract:Aiming at the situation that the preloaded blades are impacted by foreign objects when the engine is working, an in-plane uniaxial and biaxial preloading device is designed. Carry out high-speed impact test of carbon fiber/epoxy resin composite (T700/TDE-86) under different pretension loads of uniaxial and biaxial. Explore the influence of pretension load on the impact resistance of composite materials, and analyze the effect of pretension load on damage area combined with ultrasonic C-scan. The results show that the initial in-plane load has a significant effect on the impact resistance and delamination damage area of the composite laminate. The pretension load will increase the flexural rigidity of the target plate, reduce the energy absorbed by the target plate, and reduce the ballistic limit, and that is more obvious in the case of biaxial pretension. After the projectile penetrates the target plate, the delamination damage area is almost unchanged. The pretension load will reduce the delamination damage area, and that is more obvious in the case of biaxial pretension.
Keywords:Preloading  Composite materials  High-speed impact  Delamination damage  Energy absorption  Ballistic limit
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