Volume 35 Issue 11
Nov.  2020
Turn off MathJax
Article Contents
LI Chao, LIU Di, MA Yanhong. Dynamic characteristics of rotor and safety design of support structure with fan blade off[J]. Journal of Aerospace Power, 2020, 35(11): 2263-2274. doi: 10.13224/j.cnki.jasp.2020.11.003
Citation: LI Chao, LIU Di, MA Yanhong. Dynamic characteristics of rotor and safety design of support structure with fan blade off[J]. Journal of Aerospace Power, 2020, 35(11): 2263-2274. doi: 10.13224/j.cnki.jasp.2020.11.003

Dynamic characteristics of rotor and safety design of support structure with fan blade off

doi: 10.13224/j.cnki.jasp.2020.11.003
  • Received Date: 2020-03-23
  • Publish Date: 2020-11-28
  • A pivot load response analysis method of comprehensively considering various mechanical processes, such as impact, inertia asymmetry, and deceleration over-critical for load control of aero engine under extreme load of blades off, was established. A safety design of buffer damping support structure for the thrust support was proposed, which can affect the dynamic characteristics of the rotor system by controlling the stiffness and damping parameters of the support structure, reducing the critical speed of the rotor. Quantitative evaluation of effectiveness for the buffer damping structure was carried out by the above pivot load response analysis method. The effects of pivot load during the impact-deceleration process was proved. Results showed that the impact effect and deceleration over the critical process caused by the blade off are the main factors that threaten the bearing capacity of the supporting structure. And the use of a buffer damping pivot structure can effectively reduce the pivot of the rotor system to 20% when fan blade off appeared, making it an effective design for the safety of the support structure.

     

  • loading
  • [1]
    PLONA D G.Bearing arrangement for a rotation shaft:US 7 909514B2[P].2011-05-22.
    [2]
    KASTL J A,VONDRELL R M.Bearing support fuse:US 6447248[P].2002-09-10.
    [3]
    VAN DUYN K G,BLOOMFIELD C T.Turbine engine beraing:US6331078B1[P].2001-12-18.
    [4]
    JADCZAK E J,MAGRET C,OLLIVIER P,et al.Uncoupling system for an aircraft turbojet engine rotary shaft:US 8646978B2[P].2014-02-11.
    [5]
    GENTA G.Dynamics of rotating systems[M].New York:Springer Science and Business Media,2007.
    [6]
    KALINOWSKI P,VAN BARGEN O,LIEBICH R.Vibrations of rotating machinery due to sudden mass loss[R].Seoul:the 8th International Federation for the Promotion of Mechanism and Machine Science World Congress,2010.
    [7]
    王宗勇,龚斌,闻邦椿.质量及激励幅值突变转子系统动力学研究[J].振动与冲击,2008,27(8):48-51,176. WANG Zongyong,GONG Bin,WEN Bangchun.Research on rotor dynamics with sudden change of mass and excitation magnitude[J].Journal of Vibration and Shock,2008,27(8):48-51,176.(in Chinese)
    [8]
    DZENAN H.Mechanical loads on a turbofan engine structure at blade-off[D].Luleā,Sweden:Luleā University of Technology,2009.
    [9]
    MA Y,LIANG Z,ZHANG D,et al.Experimental investigation on dynamical response of an overhung rotor due to sudden unbalance[R].ASME Paper GT2015-42453,2015.
    [10]
    WANG C,ZHANG D,MA Y.Theoretical and experi-mental investigation on the sudden unbalance and rub-impact in rotor system caused by blade off[J].Mechanical Systems and Signal Processing,2016,76/77:111-135.
    [11]
    袁慧群.转子动力学基础[M].北京:冶金工业出版社,2013.
    [12]
    CHEN G.Vibration modelling and verifications for whole aero-engine[J].Journal of Sound and Vibration,2015,349:163-176.
    [13]
    洪杰,栗天壤,王永锋,等.叶片丢失激励下航空发动机柔性转子系统的动力学响应[J].航空动力学报,2018,33(2):257-264. HONG Jie,LI Tianrang,WANG Yongfeng,et al.Dynamic response of the aero-engine flexible rotor system under the blade-off[J].Journal of Aerospace Power,2018,33(2):257-264.(in Chinese)
    [14]
    YU Pingchao,ZHANG Dayi,MA Yanhong.Dynamic modeling and vibration characteristics analysis of the aero-engine dual-rotor system with fan blade out[J].Mechanical Systems and Signal Processing,2018,106:158-175.
    [15]
    LAWRENCE C,CARNEY K,GALLARDO V.Simulation of aircraft engine blade-out structural dynamics[R].NASA/TM-2001-210957,2001.
    [16]
    彭刚,李超,曹冲,等.冲击激励转子系统动力学响应及安全性设计[J].推进技术,2018,39(5):1111-1121. PENG Gang,LI Chao,CAO Chong,et al.Dynamic re-sponse and safety design of rotor system with impact excitatior[J].Journal of Propulsion Technology,2018,39(5):1111-1121.(in Chinese)
    [17]
    郭宝亭,朱梓根.金属橡胶阻尼器在转子系统中的应用[J].航空动力学报,2003,18(5):662-668. GUO Baoting,ZHU Zigen.Application of metal-rubber damper to the rotor system[J].Journal of Aerospace Power,2003,18(5):662-668.(in Chinese)
    [18]
    陈艳秋,郭宝亭,朱梓根.金属橡胶减振垫刚度特性及本构关系研究[J].航空动力学报,2002,17(4):416-420.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (539) PDF downloads(330) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return