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

航空发动机机匣螺栓连接结构力学特性影响因素

孙衍山 曾周末 杨昊

孙衍山, 曾周末, 杨昊. 航空发动机机匣螺栓连接结构力学特性影响因素[J]. 机械科学与技术, 2017, 36(12): 1964-1969. doi: 10.13433/j.cnki.1003-8728.2017.1225
引用本文: 孙衍山, 曾周末, 杨昊. 航空发动机机匣螺栓连接结构力学特性影响因素[J]. 机械科学与技术, 2017, 36(12): 1964-1969. doi: 10.13433/j.cnki.1003-8728.2017.1225
Sun Yanshan, Zeng Zhoumo, Yang Hao. Analysis of Influencing Factors on Mechanical Characteristics of Bolt Connection Structure in Aircraft Engine[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(12): 1964-1969. doi: 10.13433/j.cnki.1003-8728.2017.1225
Citation: Sun Yanshan, Zeng Zhoumo, Yang Hao. Analysis of Influencing Factors on Mechanical Characteristics of Bolt Connection Structure in Aircraft Engine[J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(12): 1964-1969. doi: 10.13433/j.cnki.1003-8728.2017.1225

航空发动机机匣螺栓连接结构力学特性影响因素

doi: 10.13433/j.cnki.1003-8728.2017.1225
基金项目: 

国家重点基础研究发展计划项目(2011cb610505)与国家自然科学基金项目(61240038)资助

详细信息
    作者简介:

    孙衍山(1982-),工程师,博士,研究方向为油液在线检测技术、微电子机械系统,sun_yanshan@126.com

    通讯作者:

    曾周末(联系人),教授,博士生导师,zhmzeng@tju.edu.cn

Analysis of Influencing Factors on Mechanical Characteristics of Bolt Connection Structure in Aircraft Engine

  • 摘要: 由于航空发动机机匣的不连续性,机匣的力学传递特性将受到影响。对传统静子机匣部件振动特性进行分析时,常不考虑机匣螺栓连接结构的影响,从而导致仿真计算的结果产生较大的偏差。基于国内外研究现状,建立螺栓连接结构的有限元分析模型,在力学传递特性方面研究了螺栓预紧力、螺栓分布和螺栓数量对机匣抗弯刚度和振动频率的影响。结果表明:航空发动机机匣螺栓连接结构会导致其结构刚度下降;螺栓预紧力、螺栓分布和螺栓数量是影响航空发动机机匣抗弯刚度和振动频率的主要因素。
  • [1] Kim J, Yoon J C, Kang B S. Finite element analysis and modeling of structure with bolted joints[J]. Applied Mathematical Modelling, 2007,31(5):895-911
    [2] Pedersen N L, Pedersen P. On prestress stiffness analysis of bolt-plate contact assemblies[J]. Archive of Applied Mechanics, 2008,78(2):75-88
    [3] Oskouei R H, Keikhosravy M, Soutis C. Estimating clamping pressure distribution and stiffness in aircraft bolted joints by finite-element analysis[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2009,223(7):863-871
    [4] 杨红平,傅卫平,王雯,等.结合面法向和切向接触刚度的MPSO-BP神经网络算法的建模[J].仪器仪表学报,2012,33(8):1856-1861 Yang H P, Fu W P, Wang W, et al. Machine joints normal and tangential contact stiffness modeling based on MPSO-BP neural network algorithm[J]. Chinese Journal of Scientific Instrument, 2012,33(8):1856-1861(in Chinese)
    [5] 姚星宇,王建军.航空发动机螺栓连接载荷与结构参数对连接刚度影响规律[J].推进技术,2017,38(2):424-433 Yao X Y, Wang J J. Effects of load and structure parameters of aero-engine bolted joints on joint stiffness[J]. Journal of Propulsion Technology, 2017,38(2):424-433(in Chinese)
    [6] 姚星宇,王建军,翟学.航空发动机螺栓连接薄层单元建模方法[J].北京航空航天大学学报,2015,41(12):2269-2279 Yao X Y, Wang J J, Zhai X. Modeling method of bolted joints of aero-engine based on thin-layer element[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015,41(12):2269-2279(in Chinese)
    [7] 翟学,王建军,翟庆刚,等.航空发动机静子系统中螺栓连接结构的建模与修正(英文)[J].推进技术,2015,36(3):450-457 Zhai X, Wang J J, Zhai Q G, et al. Modeling and updating for bolted joints structure in aero-engine stator system[J]. Journal of Propulsion Technology, 2015,36(3):450-457(in Chinese)
    [8] 高希光,宋迎东,朱如鹏,等.航空发动机低压涡轮转子连接螺栓预紧力分析[J].机械科学与技术,2011,30(4):543-547 Gao X G, Song Y P, Zhu R P, et al. A method for calculating the preload of connecting bolts in aero-engine rotors[J]. Mechanical Science and Technology for Aerospace Engineering, 2011,30(4):543-547(in Chinese)
    [9] Nezhad H Y, Egan B, Merwick F, et al. Bearing damage characteristics of fibre-reinforced countersunk composite bolted joints subjected to quasi-static shear loading[J]. Composite Structures, 2017,166:184-192
    [10] Shi G, Chen X S, Wang D Y. Experimental study of ultra-large capacity end-plate joints[J]. Journal of Constructional Steel Research, 2017,128:354-361
    [11] Cheng X Q, Wang S W, Zhang J, et al. Effect of damage on failure mode of multi-bolt composite joints using failure envelope method[J]. Composite Structures, 2017,160:8-15
    [12] Feng R Q, Liu F C, Yan G R, et al. Mechanical behavior of Ring-sleeve joints of single-layer reticulated shells[J]. Journal of Constructional Steel Research, 2017,128:601-610
    [13] 于明月,陈果,姜广义,等.基于机匣加速度信号的航空发动机转静碰摩部位识别[J].中国机械工程,2014,25(8):1102-1108 Yu M Y, Chen G, Liu G Y, et al. Aero-engine rotor-stator rubbing positions identification based on casing acceleration signals[J]. China Mechanical Engineering, 2014,25(8):1102-1108(in Chinese)
    [14] 杨一舟,蒋东翔.概率神经网络用于机匣振动故障诊断[J].机械科学与技术,2016,35(12):1805-1810 Yang Y Z, Jiang D X. Casing vibration fault diagnosis based on probabilistic neural networks[J]. Mechanical Science and Technology for Aerospace Engineering, 2016,35(12):1805-1810(in Chinese)
    [15] 温登哲,陈予恕.径向简谐激励下航空发动机机匣的振动分析[J].航空动力学报,2015,30(1):96-105 Wen D Z, Chen Y S. Vibration analysis of aero-engine casing under radial harmonic excitation[J]. Journal of Aerospace Power, 2015,30(1):96-105(in Chinese)
  • 加载中
计量
  • 文章访问数:  191
  • HTML全文浏览量:  33
  • PDF下载量:  6
  • 被引次数: 0
出版历程
  • 收稿日期:  2016-12-16
  • 刊出日期:  2017-12-15

目录

    /

    返回文章
    返回