Strength Analysis of Bearing Support in Heavy-Duty Gas Turbine

被引：0
|
作者：
Duan, Wenbo [1 ]
Deng, Zhikai [2 ]
Cheng, Wenjie [1 ]
机构：
[1] Xian Inst Appl Opt, Xian, Peoples R China
[2] CRRC Zhuzhou Elect Co Ltd, Zhuzhou, Peoples R China
来源：
2021 4TH INTERNATIONAL CONFERENCE ON ROBOTICS, CONTROL AND AUTOMATION ENGINEERING (RCAE 2021) | 2021年
关键词：
Gas turbine; radial support; tangential support; strength;
D O I：
10.1109/RCAE53607.2021.9638943
中图分类号：
TP24 [机器人技术];
学科分类号：
080202 ; 1405 ;
摘要：
Aiming at the strength of the support in heavy gas turbine (HGT), a simplified method was proposed. The bearing house was regarded as a rigid body, and the supporting strut was moded by a fixed end beam. Based on the energy method and the deformation compatibility condition of the strut, the analytical formula was derived and verified by the finite element method (FEM). The results show that the analytical solution is consistent with the FEM results. The supporting strut is mainly affected by bending normal stress and axial tensile pressure, the shear stress is about 0.8% of the normal stress.
引用
收藏
页码：321 / 325
页数：5
相关论文
共 50 条
  • [41] Gas Turbine Fouling: A comparison Among One Hundred Heavy-Duty Frames
    Aldi, Nicola
    Casari, Nicola
    Morini, Mirko
    Pinelli, Michele
    Spina, Pier Ruggero
    Suman, Alessio
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 9, 2018,
  • [42] Model development and field testing of a heavy-duty gas-turbine generator
    Pourbeik, Pouyan
    Modau, Fhedzisani
    [J]. IEEE TRANSACTIONS ON POWER SYSTEMS, 2008, 23 (02) : 664 - 672
  • [43] Upgrade of the Intake Air Cooling System for a Heavy-Duty Industrial Gas Turbine
    Ingistov, Steve
    Chaker, Mustapha
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 4, 2012, : 579 - 590
  • [44] IMPACT OF THE INFLOW CONDITIONS ON THE HEAVY-DUTY GAS TURBINE EXHAUST DIFFUSERS PERFORMANCE
    Vassiliev, Vladimir
    Irmisch, Stefan
    Abdel-Wahab, Samer
    Granovskiy, Andrey
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 1401 - 1412
  • [45] PERFORMANCE TEST OF DLN COMBUSTOR FOR 110 MW HEAVY-DUTY GAS TURBINE
    Qi, Haiying
    Xie, Gang
    Li, Yuhong
    Feng, Chong
    Chen, Xiaoli
    [J]. PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON POWER ENGINEERING 2009 (ICOPE-09), VOL 1, 2009, : 59 - 64
  • [46] Study on combustion and emission characteristics of a heavy-duty gas turbine combustor fueled with natural gas
    Zeng, Wen
    Pang, Liyao
    Zheng, Weilin
    Hu, Erjiang
    [J]. FUEL, 2020, 275
  • [47] Frequency Domain Delay Performance Analysis of Heavy-Duty Gas Turbine Control System: Theory and Experiment
    Su, Yang
    Chen, Yuanye
    Liu, Yajuan
    Fang, Fang
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2024,
  • [48] Detailed exergetic evaluation of heavy-duty gas turbine systems running on natural gas and syngas
    Sorgenfrei, Max
    Tsatsaronis, George
    [J]. ENERGY CONVERSION AND MANAGEMENT, 2016, 107 : 43 - 51
  • [49] Analysis of the Journal Bearing Friction Losses in a Heavy-Duty Diesel Engine
    Knauder, Christoph
    Allmaier, Hannes
    Sander, David Emanuel
    Salhofer, Stefan
    Reich, Franz Markus
    Sams, Theodor
    [J]. LUBRICANTS, 2015, 3 (02): : 142 - 154
  • [50] Failure Analysis of a Heavy Duty Gas Turbine Blade*
    S. Asadikouhanjani
    M. Torfeh
    R. Ghorbanf
    [J]. Strength of Materials, 2014, 46 : 608 - 612
12345