期刊文献+

机翼前缘局部填充泡沫铝抗鸟撞特性 被引量:2

Anti-bird Impact Characteristics of Partially Filled Aluminum Foaminthe Leading Edge of Wing
在线阅读 下载PDF
导出
摘要 在保证飞机机翼前缘质量特性的前提下,通过一种泡沫铝局部填充机翼前缘的优化结构来提高机翼前缘的抗鸟撞性能。通过LS-DYNA软件分别开展机翼前缘未填充和局部填充泡沫铝材料抗鸟撞分析,研究两者撞击响应、前墙响应和吸能特性的差异性,并基于D80气炮开展鸟撞铝板试验来验证鸟体本构参数的准确性和有效性。研究结果表明:通过减少蒙皮厚度并局部填充泡沫铝的方式能够在优化机翼前缘质量的同时有效地增强机翼前缘的抗冲击强度;机翼前缘局部填充泡沫铝之后前墙面板中心点位移以及等效应力得到有效降低,填充机翼前缘结构比空机翼前缘结构能够更有效地抵御鸟体撞击;在蒙皮和泡沫铝的共同作用下,局部填充泡沫铝的机翼前缘能够比空机翼前缘在相同撞击工况下吸收更多的能量。 Under the premise of ensuring the weight characteristics of the leading edge of the aircraft wing,improved the anti-bird strike performance of the aircraft through a wing leading edge structure partially filled with aluminum foam.The anti-bird impact performance analysis of the unfilled front edge and partially filled aluminum foam was carried out by LS-DYNA.The differences of impact response,front wall response and energy absorption characteristics of the two were studied.And the bird impact aluminum plate test was carried out by D80 gas gun to verify the accuracy and effectiveness of the bird constitutive parameters.Results show that reducing the thickness of the skin and partially filling the aluminum foam not only optimizes the weight of the leading edge of the wing but also effectively enhance the strength of the structure.The displacement and the equivalent stress of the center point of the front wall of the leading edge of the wing partially filled with aluminum foam are effectively reduced.The leading edge of the wing partially filled with aluminum foam is more effective against bird impact;With the combination of skin and aluminum foam,the leading edge of the partially filled aluminum foam can absorb more energy under the same impact conditions.
作者 郭亚周 刘小川 白春玉 王计真 郭军 GUO Ya-zhou;LIU Xiao-chuan;BAI Chun-yu;WANG Ji-zhen;GUO Jun(Aviation Key Laboratory of Scienceand Technologyon Structures Impact Dynamics,China Aircraft Strength Research Institute,Xi’an 710065,China)
出处 《科学技术与工程》 北大核心 2020年第8期3348-3355,共8页 Science Technology and Engineering
基金 陕西省青年科技新星项目(S2018-ZC-XXXM-0029)。
关键词 机翼前缘 局部填充泡沫铝 抗鸟撞 前墙响应 吸能特性 the leading edge partially filled aluminum foam anti-bird impact front wall response energy absorption characteristics
  • 相关文献

参考文献11

二级参考文献78

共引文献119

同被引文献16

引证文献2

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部