留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

不同金属硬物冲击航空发动机叶片损伤研究

舒畅 程铭 许煜

舒畅, 程铭, 许煜. 不同金属硬物冲击航空发动机叶片损伤研究[J]. 航空动力学报, 2020, 35(1): 18-29. doi: 10.13224/j.cnki.jasp.2020.01.003
引用本文: 舒畅, 程铭, 许煜. 不同金属硬物冲击航空发动机叶片损伤研究[J]. 航空动力学报, 2020, 35(1): 18-29. doi: 10.13224/j.cnki.jasp.2020.01.003
SHU Chang, CHENG Ming, XU Yu. Study on damage of aero-engine blades caused by different metal hard materials[J]. Journal of Aerospace Power, 2020, 35(1): 18-29. doi: 10.13224/j.cnki.jasp.2020.01.003
Citation: SHU Chang, CHENG Ming, XU Yu. Study on damage of aero-engine blades caused by different metal hard materials[J]. Journal of Aerospace Power, 2020, 35(1): 18-29. doi: 10.13224/j.cnki.jasp.2020.01.003

不同金属硬物冲击航空发动机叶片损伤研究

doi: 10.13224/j.cnki.jasp.2020.01.003
基金项目: 国家重点基础研究发展计划(2015CB057400)

Study on damage of aero-engine blades caused by different metal hard materials

  • 摘要: 为分析不同金属硬物对航空发动机风扇叶片造成的外物损伤特征差异,选取钢、铜、铝、铅四种材料弹珠作为外来物,以两种角度、多种速度冲击真实叶片进气边缘进行高速弹道冲击试验,并采用数值方法仿真动态损伤过程。结果表明:钢、铜珠冲击时,叶片损伤形貌可分为凹坑、撕裂和缺口,产生撕裂形貌时,小角度相比于大角度冲击需要更高的冲击速度,铜珠相比于钢珠冲击需要更高的速度;铝、铅珠因冲击时自身变形较大,对叶片只能造成挤压变形。仿真结果表明:在22 J冲击能量条件下,铜珠、钢珠造成叶片撕裂损伤的过程中存在两个显著的接触力峰值,且伴随着“动能回升”现象;铜珠动能较多地转化为叶片和自身的应变能,因而对叶片的侵彻能力不如钢珠;铝珠冲击力峰值最大,其动能转化为自身应变能的比例最高;铅珠冲击力峰值不明显,其动能大部分转化为摩擦耗散的热量。

     

  • [1] 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 aero-engine[J].Acta Aeronautical et Astronautica Sinica,2007,28(4):851-857.(in Chinese)
    [2] 乔文逍,熊昌炳.航空发动机外物损伤实验技术研究[J].航空动力学报,1990,5(3):227-228. QIAO Wenxiao,XIONG Changbing.Experimental technology researches of foreign object damage in aero engine[J].Journal of Aerospace Power,1990,5(3):227-228.(in Chinese)
    [3] BRADFORD B.FY01 engine-related mishap summary[J].Flying Safety,2002,58(2):42-47.
    [4] PETERS J O,RITCHIE R O.Foreign-object damage and high-cycle fatigue of Ti-6Al-4V[J].Materials Science and Engineering A,2001,319-321:597-601.
    [5] SPANRAD S,TONG J.Characterization of foreign object damage (FOD) and early fatigue crack growth in laser shock peened Ti-6AL-4V aerofoil specimens[J].Materials Science and Engineering A,2011,528(4/5):2128-2136.
    [6] 魏雪霞,李广利.沙粒对飞机发动机叶片的冲击碰撞[J].北京理工大学学报,2005,25(6):471-474. WEI Xuexia,LI Guangli.The impact of sand on the blades of airplane engines[J].Transactions of Beijing Institute of Technology,2005,25(6):471-474.(in Chinese)
    [7] 赵振华,陈伟,关玉璞,等.外物损伤对不锈钢疲劳强度的影响[J].航空动力学报,2016,31(7):1736-1743. ZHAO Zhenhua,CHEN Wei,GUAN Yupu,et al.Effect of foreign object damage on fatigue strength of stainless steel[J].Journal of Aerospace Power,2016,31(7):1736-1743.(in Chinese)
    [8] 葛宁.发动机叶片抗外物损伤能力评估技术研究[D].南京:南京航空航天大学,2012. GE Ning.Research on evaluate technology about resistance to foreign object damage of engine blade[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
    [9] 胡绪腾,宋迎东.叶片外物损伤容限设计的本质特点及设计准则的发展[J].航空动力学报,2008,23(12):2153-2161. HU Xuteng,SONG Yingdong.Essential characteristic of foreign object damage tolerance design for airfoils in aeroengine and development of design criteria[J].Journal of Aerospace Power,2008,23(12):2153-2161.(in Chinese)
    [10] 胡绪腾,贾旭,朱自佳.凹坑型硬物损伤对TC4材料疲劳强度的影响[J].航空动力学报,2018,33(4):969-979. HU Xuteng,JIA Xu,ZHU Zijia.Effect of dent-type foreignobject damage on fatigue strength of TC4 material[J].Journal of Aerospace Power,2018,33(4):969-979.(in Chinese)
    [11] 贾旭,胡绪腾,宋迎东.虑及高循环疲劳的裂纹型外物损伤叶片的可用极限[J].航空动力学报,2019,34(2):292-304. JIA Xu,HU Xuteng,SONG Yingdong.Serviceable limits of a crack type foreign object damaged blade considering high cycle fatigue[J].Journal of Aerospace Power,2019,34(2):292-304.(in Chinese)
    [12] 贾旭,胡绪腾,朱自佳.FOD缺口型损伤对TC4疲劳极限强度的影响[J].航空动力学报,2018,33(7):1584-1594. JIA Xu,HU Xuteng,ZHU Zijia.Effect of FOD notch-type damage on fatigue limit strength of TC4[J].Journal of Aerospace Power,2018,33(7):1584-1594.(in Chinese)
    [13] KAUFMAN A,MEYER A J J.Investigation of the effect of impact damage on fatigue strength of jet-engine compressor rotor blades[J].Technical Report Archive and Image Library,1956,18(3):158-162.
    [14] NICHOLAS T.High cyclefatigue:a mechanics of materials perspective[M].Washington DC:Elsevier Science and Technology,2006.
    [15] 马超,王玉娜,武耀罡,等.航空发动机风扇叶片硬物冲击损伤特征[J].航空动力学报,2017,32(5):1105-1111. MA Chao,WANG Yuna,WU Yaogang,et al.Hard object impact damage characteristic of aero-engine fan blade[J].Journal of Aerospace Power,2017,32(5):1105-1111.(in Chinese)
    [16] 马超,武耀罡,师利中,等.航空发动机风扇叶片硬物冲击损伤的统计分析[J].航空维修与工程,2016(3):41-42. MA Chao,WU Yaogang,SHI Lizhong,et al.Hard object impact damage statistical analysis of aero-engine fan blade[J].Aviation Maintenance and Engineering,2016(3):41-42.(in Chinese)
    [17] 孙振德,鲁启新.外物撞击损伤叶片的模拟试验方法[J].航空动力学报,1989,4(1):30-32. SUN Zhende,LU Qixin.Simulation test method of foreign objects damage[J].Journal of Aerospace Power,1989,4(1):30-32.(in Chinese)
    [18] MALL S,HAMRICK J L.High cycle fatigue behavior of Ti-6Al-4V with simulated foreign object damage[J].Mechanics of Materials,2001,33(11):679-692.
    [19] 潘辉,赵振华,陈伟.航空发动机叶片外物损伤试验模拟方法[J].航空发动机,2012,38(1):51-54. PAN Hui,ZHAO Zhenhua,CHEN Wei.Aeroengine blade foreign object damage test simulation method[J].Aeroengine,2012,38(1):51-54.(in Chinese)
    [20] 胡绪腾,宋迎东.外物损伤对风扇/压气机叶片高循环疲劳性能影响的研究[J].航空发动机,2012,38(3):18-23. HU Xuteng,SONG Yingdong.Research on effect of foreign object damage on high cycle fatigue performance for fan/compressor blades[J].Aeroengine,2012,38(3):18-23.(in Chinese)
    [21] NICHILAS T,THOMPSON S R,PORTER W J,et al.Comparison of fatigue limit strength of Ti-6Al-4V in tension and torsion after real and simulated foreign object damage[J].International Journal of Fatigue,2005,27(10):1637-1643.
    [22] CHEN X.Foreign object damage on the leading edge of a thin blade[J].Mechanics of Materials,2005,37(4):447-457.
    [23] MAJILA A N,RAMACHANDRA S,MANNAN S L,et al.Influence of foreign object damage on high cycle fatigue of Ti-6Al-4V alloy[J].Transactions of the Indian Institute of Metals,2015,69(8):1-7.
    [24] 刘庆瑔.航空发动机钛合金叶片制造技术及失效分析[M].北京:航空工业出版社,2018.
    [25] 胡绪腾.外物损伤及其对钛合金叶片高循环疲劳强度的影响[D].南京:南京航空航天大学,2009. HU Xuteng.Foreign object damage and its effect on high cycle fatigue strength of titanium alloy engine blades[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
    [26] 季玉辉.基于Johnson-Cook模型的硬物损伤数值模拟研究[D].南京:南京航空航天大学,2009. JI Yuhui.Numerical simulation of hard-body foreign object damage based on Johnson-Cook model[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
    [27] 陈敏.TC4钛合金力学性能测试及动态材料模型研究[D].南京:南京航空航天大学,2012. CHEN Min.Research on mechanical properties test and dynamic material model of Ti6Al4V titanium alloy[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
    [28] DONALD R L.Experimental investigations of material models for Ti-6Al-4V titanium and 2024-T3 aluminum[R].Washington DC:Department of Transportation,DOT/FAA/AR-00/25,2000.
    [29] 熊令芳,胡凡金.ANSYS LS-DYNA非线性动力分析方法与工程应用[M].北京:中国铁道出版社,2016.
    [30] 曾正明,彭福泉.机械工程材料手册[M].北京:机械工业出版社,1998.
    [31] 曾正明.实用有色金属材料手册[M].北京:机械工业出版社,2016.
  • 加载中
计量
  • 文章访问数:  456
  • HTML浏览量:  5
  • PDF量:  464
  • 被引次数: 0
出版历程
  • 收稿日期:  2019-06-26
  • 刊出日期:  2020-01-28

目录

    /

    返回文章
    返回