Volume 35 Issue 6
Jun.  2020
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ZHANG Haiyang, WANG Xiangping, DU Shaohui. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005
Citation: ZHANG Haiyang, WANG Xiangping, DU Shaohui. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power, 2020, 35(6): 1157-1168. doi: 10.13224/j.cnki.jasp.2020.06.005

Design for anti-bird impact of aero-engine fan blade

doi: 10.13224/j.cnki.jasp.2020.06.005
  • Received Date: 2019-12-12
  • Publish Date: 2020-06-28
  • The first stage fan rotor blade is a key component of the engine against bird impact, and the leading edge of the blade is a key part of the anti-bird impact design, by investigating the structural characteristics of the engine and the damage characteristics after bird impact. Therefore, a theoretical analysis method of fan blade bird impact was established to study the relationship among impact conditions, structural parameters and bird impact process, and damage mode as well as damage degree. Results show that the leading edge angle is the key structural parameter of anti-bird impact. The leading edge angle determined the impact process, damage mode and damage degree, when the bird impact conditions were determined. A model with leading edge characteristics was designed and the influence rule of leading edge angle was verified using the method of display dynamics simulation analysis. Based on the results, an improved design of the actual fan blade was carried out. The deformation of improved blade was reduced by a minimum of 33% after being hit by a bird, and the anti-bird impact ability of the improved blade was obviously improved.

     

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  • [1]
    陈光.飞机发动机的防鸟撞设计与试验[J].国际航空,2009(11):63-65. CHEN Guang.Prevention of bird strike hazards to aero-engines[J].International Aviation,2009(11):63-65.(in Chinese)
    [2]
    李玉龙,石霄鹏.民用飞机鸟撞研究现状[J].航空学报,2012,33(2):189-198. LI Yulong,SHI Xiaopeng.Investigation of the present status of research on bird impacting on commercial airplanes[J].Acta Aeronautica et Astronautica Sinica,2012.33(2):189-198.(in Chinese)
    [3]
    刘大响,金捷,彭友梅,等.大型飞机发动机的发展现状和关键技术分析[J].航空动力学报,2008,23(6):976-980. LIU Daxiang,JIN Jie,PENG Youmei,et al.Summarization of development status and key technologise for large airplane engines[J].Journal of Aerospace Power,2008,23(6):976-980.(in Chinese)
    [4]
    吴大观.发动机吞鸟试验[J].航空标准化与质量,1984(5):29-31. WU Daguan.Aeroengine swallowing test[J].Aviation Standardization and Quality,1984(5):29-31.(in Chinese)
    [5]
    葛治美,姜锡明.军用航空涡喷和涡扇发动机吞鸟试验[J].航空发动机,1998,24(1):32-38. GE Zhimei,JIANG Ximing.Military aviation turbojet and turbofan engine swallowing test[J].Aeroengine,1998,24(1):32-38.(in Chinese)
    [6]
    BARBER J P,TAYLOR H R,WILBECK J S.Bird impacts forces and pressures on rigid and compliant targets[R].Dayton,Ohio:US:Air Force Flight Laboratory,1978.
    [7]
    WILBECK J S,BARBER J P.Bird impact loading[J].The Shock and Vibration Bulletin,1978,48(2):115-122.
    [8]
    WILBECK J S.Impact behavior of low strength projectiles[R].US Air Force Materials Laboratory,Wright-Patterson Air Force Base,AFML-TR-77-134,1978.
    [9]
    BARBER J P,TAYLOR H R,WILBECK J S.Characterization of bird impacts on a rigid plate:Part 1[R].US Air Force Flight Dynamics Laboratory,Wright-Patterson Air Force Base,AFFDL-TR-75-5,1975.
    [10]
    尹晶,高德平,范尔宁.鸟撞击叶片时的载荷模型[J].航空动力学报,1993,8(4):363-367. YIN Jing,GAO Deping,FAN Erning.The load model of bird impact blade[J].Journal of Aerospace Power,1993,8(4):363-367.(in Chinese)
    [11]
    李清红,高德平.叶片鸟撞击的理论和实验研究[J].航空动力学报,1990,5(4):335-339. LI Qinghong,GAO Deping.Analytical and experimental investigation of bird impacr on blade[J].Journal of Aerospace Power,1990,5(4):335-339.(in Chinese)
    [12]
    关玉璞,陈伟,黄志勇.一种鸟撞击叶片的切割模型[J].南京航空航天大学学报,2004,36(6):784-786. GUAN Yupu,CHEN Wei,HUANG Zhiyong.Sliced model for bird impacting blades[J].Journal of Nanjing University of Aeronautics and Astronautics,2004,36(6):784-786.(in Chinese)
    [13]
    关玉璞,陈伟,高德平.航空发动机叶片外物损伤研究现状[J].航空学报,2007,28(4):851-857. GUAN Yupu,CHEN Wei,GAO Deping.Present status of investigation of foreign object damage to blade in aeroengine[J].Acta Aeronautica et Astronautica Sinica,2007,28(4):851-857.(in Chinese)
    [14]
    GUAN Yupu,ZHAO Zhenhua,CHEN Wei.Foreign object damage to fan rotor blades of aeroengine:Part Ⅰ experimental study of bird impact[J].Chinese Journal of Aeronautics,2007,20(5):408-414.
    [15]
    文颖娟.叶片鸟撞击响应分析模化技术与验证研究[D].南京:南京航空航天大学,2006. WEN Yingjuan.Parametrization and validity analysis on the response of flat blades due to bird impact[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2006.(in Chinese)
    [16]
    陈伟,关玉璞,高德平.发动机叶片鸟撞击瞬态响应的数值模拟[J].航空学报,2003,24(6):531-533. CHEN Wei,GUAN Yupu,GAO Deping.Numerical simulation of the transient response of blade due to bird impact[J].Acta Aeronautica et Astronautica Sinica,2003,24(6):531-533.(in Chinese)
    [17]
    GUAN Yupu,ZHAO Zhenhua,CHEN Wei,et al.Foreign object damage to fan rotor blades of aeroengine:Part Ⅱ numerical simulation of bird impact[J].Chinese Journal of Aeronautics,2008,21(4):328-334.
    [18]
    刘军,李玉龙,刘元镛.基于SPH方法的叶片鸟撞数值模拟研究[J].振动与冲击,2008,27(9):90-93. LIU Jun,LI Yulong,LIU Yuanyong.Numerial simulation study of bird-impact on a balde using SPH method[J].Journal of Vibration and Shock,2008,27(9):90-93.(in Chinese)
    [19]
    蒋向华,王延荣.采用流固耦合方法的整级叶片鸟撞击数值模拟[J].航空动力学报,2008,23(2):299-304. JIANG Xianghua,WANG Yanrong.Numerical simulation of bird impacr on bladed rotor bird stage by fluid-solid coupling method[J].Journal of Aerospace Power,2008,23(2):299-304.(in Chinese)
    [20]
    陈伟,宋迎东,尹晶,等.离心载荷作用下平板叶片鸟撞击响应计算[J].航空动力学报,1997,12(2):122-126.CHEN Wei,SONG Yingdong,YIN Jing,et al.Numerical analysis of blade transient responses to bird impact under centrifugal loadings[J].Journal of Aerospace Power,1997,12(2):122-126.(in Chinese)
    [21]
    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.(in Chinese)
    [22]
    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.
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