Research on bird strike resistance performance of hollow plates with warren structure

Bin Wang, Jinfeng Lv, Yu Ning, Zhongbin Tang, Cunxian Wang
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引用次数: 0

Abstract

This study initially conducted bird strike tests and numerical simulations on hollow plates with the Warren structure. The plates manifested notable plastic deformation devoid of fracture. The simulated deformations and strain data of the plates closely corresponded with the outcomes of bird strike impact tests, thereby validating the employed bird strike simulation methodology in this study. Subsequently, while maintaining the outer dimensions of the hollow plate constant, an investigation into the structural parameters of the hollow plate was conducted. Correlations between the thickness of the outer panel, thickness of the Warren, angle of the Warren, and the anti-bird-strike performance of the hollow plate structure were established. The research findings offer valuable insights for informing the design of bird strike resistance in engine blades and hollow plates.
疣状结构空心板抗鸟击性能研究
这项研究最初对具有沃伦结构的空心板进行了鸟击试验和数值模拟。试验结果表明,空心板发生了明显的塑性变形,但没有发生断裂。板材的模拟变形和应变数据与鸟击撞击试验结果非常吻合,从而验证了本研究采用的鸟击模拟方法。随后,在保持中空板外部尺寸不变的情况下,对中空板的结构参数进行了研究。建立了外板厚度、华伦厚度、华伦角度与中空板结构抗鸟击性能之间的相关性。研究结果为发动机叶片和空心板的抗鸟击设计提供了宝贵的启示。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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