Vibration Analysis of Aeroengine Compressor Blade-Disc Coupling System

被引：7
|
作者：
Zhao, Weiqiang [1 ,2 ]
Liu, Yongxian [1 ]
Lu, Mowu [2 ]
机构：
[1] Northeastern Univ, Sch Mech Engn & Automat, Shenyang Liaoning 110004, Peoples R China
[2] Shenyang Inst Aeronaut Engn, Engn Trainning Ctr, Shenyang, Peoples R China
来源：
E-ENGINEERING & DIGITAL ENTERPRISE TECHNOLOGY VII, PTS 1 AND 2 | 2009年 / 16-19卷
关键词：
Compressor blade-disc system; Finite element method; Modal analysis;
D O I：
10.4028/www.scientific.net/AMM.16-19.264
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
This paper introduces the FEA method for cyclic symmetric structures and makes an vibration characteristics analysis to a certain aeroengine compressor blade-disc coupling system based on this method. According to the anslysis results the dynamic characteristics of the blade-disc coupling system are discussed. The analysis method and results in this paper can be used for further study on optimal design and vibration safety verification for the blade-disc coupling system.
引用
收藏
页码：264 / 268
页数：5
相关论文
共 50 条
  • [41] ANALYSIS OF AN AXIAL COMPRESSOR BLADE VIBRATION BASED ON WAVE REFLECTION THEORY
    OWCZAREK, JA
    MECHANICAL ENGINEERING, 1983, 105 (06) : 87 - 87
  • [42] An Influence of Geometrical Parameters of the Lock of the Blade-Disc Joint on Stress in the FEA and DIC Methods
    Kozakiewicz, Adam
    Grzejszczak, Olga
    ADVANCES IN SCIENCE AND TECHNOLOGY-RESEARCH JOURNAL, 2021, 15 (01) : 209 - 217
  • [43] DETECTION AND STUDY OF COMPRESSOR-BLADE VIBRATION
    HOHENBER.R
    EXPERIMENTAL MECHANICS, 1967, 7 (06) : A19 - &
  • [44] Holographic vibration measurement of disc-blade coupling in high-speed rotation
    Qiufang, Wu
    Guoliang, Jiang
    Kaining, Zhao
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 1992, 7 (02): : 131 - 134
  • [45] Coupling vibration mechanism of rotating shaft-disc-blade system with blade crack-A systematical investigation on the effect of crack, condition, and structure parameters
    Yang, Lai-Hao
    Sun, Yu
    Yang, Zhi-Bo
    Mao, Zhu
    Chen, Xue-Feng
    THIN-WALLED STRUCTURES, 2024, 205
  • [46] SIMULATION OF THERMAL FLUID-STRUCTURE INTERACTION IN BLADE-DISC CONFIGURATION OF AN AIRCRAFT TURBINE MODEL
    Lueck, Hannes
    Schaefer, Michael
    Schiffer, Heinz-Peter
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5A, 2014,
  • [47] Fast analysis of forced vibration response on intermediate stage compressor rotor blade
    Han L.
    Wang Y.
    Wei D.
    Yang W.
    Li D.
    Zou Z.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2022, 37 (11): : 2636 - 2646
  • [48] Analysis on coupling vibration frequency characteristics of wind turbine blade rotating fatigue loading system
    Liao G.
    Wu J.
    Zhang L.
    1600, Nanjing University of Aeronautics an Astronautics (36): : 1085 - 1090
  • [49] Mechanism of Nonsynchronous Blade Vibration in a Transonic Compressor Rig
    Moeller, Daniel
    Juengst, Maximilian
    Holzinger, Felix
    Brandstetter, Christoph
    Schiffer, Heinz-Peter
    Leichtfuss, Sebastian
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2017, 139 (01):
  • [50] COMPUTATIONAL ANALYSIS OF COMPRESSOR BLADE EROSION IN A WET COMPRESSION SYSTEM
    Chidambaram, Palani Kumar
    Song, Tae Hoon
    Kim, In Won
    Lee, Kwon Hee
    Kim, Heuy Dong
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2C, 2016,
12345