鸟撞过程中撞击位置与撞击姿态对风扇叶片损伤影响研究

郭鹏1,刘志远2,张桂昌3,Reza Hedayati4,张俊红2

振动与冲击 ›› 2021, Vol. 40 ›› Issue (12) : 124-131.

PDF(3094 KB)
PDF(3094 KB)
振动与冲击 ›› 2021, Vol. 40 ›› Issue (12) : 124-131.
论文

鸟撞过程中撞击位置与撞击姿态对风扇叶片损伤影响研究

  • 郭鹏1,刘志远2,张桂昌3,Reza Hedayati4,张俊红2
作者信息 +

Study on effect of bird impact position and attitude on fan blade damage

  • GUO Peng1,LIU Zhiyuan2,ZHANG Guichang3,REZA Hedayati4,ZHANG Junhong2
Author information +
文章历史 +

摘要

为研究鸟撞风扇叶片过程中撞击位置及撞击姿态对风扇叶片瞬态冲击响应的影响,通过CT扫描建立光滑粒子流体动力学(smooth particle hydrodynamics, SPH)绿头鸭模型,根据相对速度原则对五个撞击位置和十五种撞击姿态的旋转风扇-鸟体撞击过程进行模拟。获得了撞击位置及撞击姿态对叶片不同位置应力响应及位移响应的影响规律。结果表明:在鸟撞叶片过程中叶片前后叶根以及前后缘易发生应力集中,在撞击过程中该区域最易发生损伤变形,且前叶根要比后叶根受到的应力更大,更易发生损伤变形;鸟撞击2/6叶高位置时,叶片受到的撞击力、叶根处及前缘处应力最大;Y-135°、Y-270°、Y-315°、Z-135°及Z-315°撞击姿态下前叶根受到的等效应力最大,Z-135°撞击姿态下后叶根受到的等效应力最大,Y-270°撞击姿态下前缘接触处位移最大。研究结果对航空发动机风扇叶片抗鸟撞设计及适航评估具有参考价值。

Abstract

To study the influence of bird impact position and impact posture on the transient response of a fan blade, a smooth particle hydrodynamics (SPH) mallard model established by CT scanning was used to simulate the process of a real bird strikes a high-speed rotating fan with five different impact positions and fifteen different impact attitudes according to the relative speed principle.The effect of impact position and attitude on the transient stress and displacement of the fan blade was obtained.Results show that during the impact process, stress concentration is likely to occur in the blade root and the leading edge, these areas are most susceptible to damage and deformation, and the anterior root has greater stress than the posterior root, which is more likely to be damaged.The impact force on the blade and the stress at the blade root and the leading edge are the largest when the bird strikes the 2/6 blade height position.In the Y-135°, Y-270°, Y-315°, Z-135° and Z-315° impact postures, the equivalent stress of the anterior root is the largest.In the Z-135 impact posture, the equivalent stress of the posterior root is the largest, and the displacement of the leading edge is the largest in the Y-270° impact posture.The results of this study have reference value for the design of anti-bird impact and airworthiness evaluation of fan blades in aero-engine.

关键词

鸟撞 / 撞击姿态 / 撞击位置 / 撞击响应 / 风扇叶片

Key words

bird strike / impact position / impact posture / impact response / fan blade

引用本文

导出引用
郭鹏1,刘志远2,张桂昌3,Reza Hedayati4,张俊红2. 鸟撞过程中撞击位置与撞击姿态对风扇叶片损伤影响研究[J]. 振动与冲击, 2021, 40(12): 124-131
GUO Peng1,LIU Zhiyuan2,ZHANG Guichang3,REZA Hedayati4,ZHANG Junhong2. Study on effect of bird impact position and attitude on fan blade damage[J]. Journal of Vibration and Shock, 2021, 40(12): 124-131

参考文献

[1]DOLBEER R A, BEGIER M J.Wildlife strikes to civil aircraft in the united states, 1990-2017 [R].The FAA National Wildlife Strike Database, Serial Report,2019.
[2]HEIMBS S. Computational methods for bird strike simulations: A review[J].Computers & Structures, 2011, 89(23/24):2093-2112.
[3]HEDAYATI R, ZIAEI-RAD S.Effect of bird geometry and orientation on bird-target impact analysis using SPH method[J].International Journal of Crashworthiness, 2012, 17(4):445-459.
[4]HEDAYATI R, ZIAEI-RAD S .A new bird model and the effect of bird geometry in impacts from various orientations[J].Aerospace Science and Technology, 2013, 28(1):9-20.
[5]MCCALLUM S C, CONSTANTINOU C.The influence of bird-shape in bird-strike analysis[C]//5th European LS-DYNA Users Conference, Birmingham, 2005.
[6]MCCALLUM S, SHOJI H, AKIYAMA H.Development of an advanced multi-material bird-strike model using the smoothed particle hydrodynamics method[J].International Journal of Crashworthiness, 2013, 18(6): 579-597.
[7]ZHANG D, FEI Q.Effect of bird geometry and impact orientation in bird striking on a rotary jet-engine fan analysis using SPH method[J].Aerospace Science & Technology, 2016, 54: 320-329.
[8]张大海,费庆国,刘宏月.基于真实形状鸟体的撞击方向对鸟撞分析影响研究[J].振动与冲击,2015,34(22):103-108.
ZHANG Dahai, FEI Qingguo, LIU Hongyue.Effects of bird's striking orientation on bird impact analysis based on a realistic bird model[J].Journal of Vibration and Shock, 2015,34(22): 103-108.
[9]寇剑锋, 徐绯, 纪三红, 等.鸟体姿态对结构抗鸟撞性能的影响[J].爆炸与冲击, 2017,37(5):937-944.
KOU Jianfeng, XU Fei, JI Sanhong, et al.Influence of bird yaw/pitch orientation on bird-strike resistance of aircraft structures [J].Explosion and Shock Waves, 2017,37(5): 937-944.
[10]杨杰. 风扇叶片鸟撞击响应及受损风扇气动性能分析方法研究[D].南京:南京航空航天大学, 2014.
[11]刘信超, 徐亚芳, 王露晨, 等.运输类飞机风挡鸟撞位置影响分析研究[J].振动与冲击, 2019, 38(17):95-102.
LIU Xinchao, XU Yafang, WANG Luchen, et al.Effects of bird strike position and boundary clamping component on transport airplane windshield safety[J].Journal of Vibration and Shock, 2019, 38(17):95-102.
[12]HEDAYATI R, SADIGHI M.Bird strike: an experimental, theoretical and numerical investigation[M].Woodhead Publishing, 2015.
[13]柴象海, 侯亮, 王志强, 等.航空发动机宽弦风扇叶片鸟撞损伤模型标定[J].航空动力学报, 2016, 31(5):1032-1038.
CHAI Xianghai, HOU Liang, WANG Zhiqiang, et al.Bird strike model calibration for aero engine wide-chord fan blade[J].Journal of Aerospace Power, 2016, 31(5):1032-1038.
[14]WILBECK J S. Impact behavior of low strength projectiles[R].Air Force Materials Lab Wright-Patterson AFB OH, 1978.
[15]HOU N, LI Y, LIU J.Numerical simulation of bird impact on hollow blades of titanium fan assembly[J].Journal of Aerospace Engineering, 2019, 32(4): 04019044.
[16]张海洋, 蔚夺魁, 王相平, 等.鸟撞击风扇转子叶片损伤模拟与试验研究[J].推进技术,2015,36(9):1382-1388.
ZHANG Haiyang, YU Duokui, WANG Xiangping, et al.Numerical and experimental investigation of damage of bird impact on fan blades[J].Journal of Propulsion Technology,  2015,36(9):1382-1388.

PDF(3094 KB)

640

Accesses

0

Citation

Detail

段落导航
相关文章

/