在冲击下的复合转子叶片的性能和损伤研究
Guorui Yu1, Xiaobin Li1, Wenjun Huang1
1AVIC China Helicopter Design and Research Institute, Jingdezhen 333001, China.
Polymers
|March 13, 2024
概括
这项研究研究了复合式直升机叶片的弹道性能,发现损伤类型包括分层和纤维破裂. 一个经过验证的数值模型有助于预测战场环境中的刀片脆弱性.
科学领域:
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
- 机械工程 机械工程
背景情况:
- 复合式直升机叶片对于飞机在战斗中的生存能力至关重要.
- 了解弹道性能对于减轻直升机脆弱性至关重要.
研究的目的:
- 为了研究复合式直升机叶片的弹道性能和损伤特性.
- 开发和验证一个用于预测弹道损伤的数值模拟模型.
主要方法:
- 在弹道冲击下对复合材料旋翼叶片的实验测试.
- 使用Abaqus软件开发一个3D渐进式损伤故障模型.
- 对数值模型与实验结果进行验证.
主要成果:
- 弹道损伤包括分层,纤维破裂和泡崩.
- 撞击位置影响损伤类型:撞击时的剪切断裂,出口时的拉力断裂.
- 损坏大小受冲击角度和结构度的影响.
结论:
- 数字模拟模型准确地预测了复合刀片弹道损伤.
- 撞击角度和出口结构的刚性是影响损坏的关键因素.
- 该模型为提高直升机生存能力提供了有价值的参考.
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