Analysis of anti-bird strike performance on GLARE laminate structure

doi:10.19936/j.cnki.2096-8000.20250828.016

Abstract

Abstract: With the development of aeronautical technologies, the speed of aircraft is improved dramatically. The probability of bird impact on aircraft during take-off and landing is greatly increased. It will result in the aircraft crash. In order to guarantee flight safety, CCAR25 airworthiness regulations have made relevant requirements for impact resistance of the leading-edge structure. Glass fiber reinforced aluminum (GLARE) as a kind of material with good impact resistance, it has been applied to the empennage leading-edge structures such as A380. In this paper, firstly, the methods and theory of anti-bird strike for GLARE leading edge structure is introduced. The analytical method has been verified. Secondly, the finite element analysis method and explicit impact software LS-DYNA is used, the four same thickness but different lay-up of GLARE leading edge structure has been studied. Thirdly, the study is conducted on different curvature GLARE laminate structure. According to analysis the failure mode, the results shows that the deformation and failure of GLARE laminate structure, structure energy absorption, stress nephogram and bird strike force. It is found that the GLARE laminate structure with 3/2[A/+45/-45/+45/-45/A/+45/-45/+45/-45/A] and curvature radius of 100 mm has the best impact resistance.

Key words: GLARE material, laminate structure, bird strike analysis, test verification

CLC Number:

TB332

TIAN Xiaoyu, ZHANG Fa, JI Shengcheng, SHI Chen, WU Xiaoguang, LIN Dakai. Analysis of anti-bird strike performance on GLARE laminate structure[J]. COMPOSITES SCIENCE AND ENGINEERING, 2025, 0(8): 132-141.

References

[1] 朱书华, 童明波, 王跃全. 某型飞机风挡鸟撞试验与数值模拟[J]. 应用力学学报, 2009, 26(3): 444-449.
[2] 刘永强, 王向盈, 唐长红, 等. 四种飞机蒙皮材料抗鸟撞性能对比研究[J]. 航空材料学报, 2015, 35(5): 82-89.
[3] 任冀宾, 王斌, 王振, 等. 某型飞机机翼前缘抗鸟撞结构设计与试验验证[J]. 爆炸与冲击, 2019, 39(2): 133-141.
[4] DOLBEER R A, WRIGHT S E, WELLER J, et al. Wildlife strike to civil aircraft in the United States 1990—2008: FAA National Wildlife Strike Database Serial Report No.15[R]. Washington: FAA, 2009.
[5] 汲生成, 温顺达, 史前, 等. 民用客机短舱和尾翼前缘鸟撞分析验证[C]//澳汰尔工程软件(上海)有限公司. 2017 Altair技术大会论文集. 南京: 2017: 1049-1058.
[6] ZHU S H, TONG M B, WANG Y Q. Experiment and numerical simulation of a full-scale aircraft wind shield subjected to bird impact: AIAA-2009-2575[R/OL]. (2009-05-04)[2024-07-16]. https://doi.org/10.2514/6.2009-2575.
[7] SMOJVER I, IVANCEYIC D. Numeric simulation of bird strike damage prediction in airplane flap structure[J]. Composite Structure, 2010, 92(9): 2016-2026.
[8] HANSSEN A G, GIRADET Y, OLOYSSON L, et al. Numerical model for bird strike of aluminum foam-based sandwich panels[J]. International Journal of Impact Engineering, 2006, 32(7): 1127-1144.
[9] AUDIC S, BERTHILLIER M, BONINI J, et al. Prediction of bird impact in hollow fan blades: AIAA-2000-3201[R/OL]. (2000-07-24)[2024-07-16]. https://doi.org/10.2514/6.2000-3201.
[10] 门向南, 闫东东, 郎利辉, 等. 刚性模和柔性介质拉深成形工艺对GLARE层板筒型件成形极限及壁厚分布的影响规律[J]. 锻压技术, 2022, 47(8): 53-59.
[11] 谢灿军, 童明波, 刘富, 等. GLARE平板抗鸟撞数值模拟[J]. 复合材料学报, 2013, 30(12): 212-218.
[12] 刘永强, 冯震宙, 唐长红. 不同铺层角度GLARE层板复合材料的抗鸟撞性能[J]. 机械工程材料, 2016, 40(5): 105-110.
[13] 熊晓枫, 张庆茂. 国内外关于Glare的研究和应用[J]. 航空制造技术, 2013(增刊2): 141-143.
[14] SINMAZÇELIK T, AVCU E, BORA M Ö, et al. A review: fiber metal laminates background, bonding types and applied test methods[J]. Materials and Design, 2011, 32(7): 3671-3685.
[15] 董彦芝, 刘芃, 王国栋. 航天器结构用材料应用现状与未来需求[J]. 航天器环境工程, 2010, 17(1): 41-45.
[16] 李晓峰, 曲贵民. GLARE层合板抗低速冲击性能分析与数值模拟[J]. 哈尔滨理工大学学报, 2017, 22(6): 140-146.
[17] 苏康, 白瑞祥, 刘琛, 等. 飞机尾翼前缘结构鸟撞仿真与改进设计[J]. 工程力学, 2022, 39(6): 236-245.
[18] 陈勇, 廖高健, 任立海, 等. 玻璃纤维增强铝合金层板高速冲击损伤容限[J]. 航空学报, 2018, 39(7): 131-142.
[19] GUIDA M, MARULO F, MEO M, et al. Analysis of bird impact on a composite tailplane leading edge[J]. Applied Composite Materials, 2008, 15(4-6): 241-257.
[20] SMOJVER I, IVANCEVIC D. Bird strike damage analysis in aircraft structures using ABAQUS/Explicit and coupled Eulerian Lagrangian approach[J]. Composites Science and Technology, 2011, 71(4): 489-498.
[21] 朱书华. 鸟撞飞机风挡动响应分析与仿真试验平台研究[D]. 南京: 南京航空航天大学, 2009: 11-20.
[22] 刘富. 贮箱内液体晃动动力学分析及结构防晃技术研究[D]. 南京: 南京航空航天大学, 2010: 19-31.
[23] 刘志明, 陈静芬, 毛欢. 基于率相关三维弹塑性损伤模型的复合材料渐进失效分析[J]. 复合材料学报, 2022, 39(5): 2482-2495.
[24] 谭建设, 张晓晶, 张俊琪. 复合材料层合板低速冲击的接触力和能量响应仿真[J]. 复合材料学报, 2014, 31(4): 971-980.
[25] 姜紫薇, 杨东, 陈建彬. 面向高速切削的钛合金Ti-6Al-4V动态本构模型[J]. 航空材料学报, 2023, 43(4): 55-67.
[26] 刘丰睿, 章凌, 杨帆, 等. 复合材料径向和轴向螺栓连接失效预测方法及失效模式分析[J]. 宇航总体技术, 2023, 7(5): 20-28.