Multidimensional analysis and performance prediction of heavy-duty gas turbine based on actual operational data

被引:9
作者
Guan, Jin [1 ]
Wang, Xusheng [1 ]
Lv, Xiaojing [2 ]
Weng, Yiwu [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Mech Engn, Key Lab Power Machinery & Engn, Minist Educ, Shanghai 200240, Peoples R China
[2] Shanghai Jiao Tong Univ, China UK Low Carbon Coll, Shanghai 201306, Peoples R China
关键词
Heavy-duty Gas turbine; Multidimensional analysis; Data-driven model; Performance prediction; Compressor surge; THERMODYNAMIC MODEL; COMBINED-CYCLE; SIMULATION; DIAGNOSTICS;
D O I
10.1016/j.applthermaleng.2023.121280
中图分类号
O414.1 [热力学];
学科分类号
摘要
This study aims to analyze and predict the degradation, safety and operational performance of a heavy-duty gas turbine based on actual operational data after running for a long time. The dataset consists of 288,039 operational records from the Ban Shan Power Plant. The data is screened using Pearson correlation coefficients and 2means clustering. Then, efficiency degradation of compressor and gas turbine is conducted by decoupling operation state from degradation. Next, Long short-term memory(LSTM) is employed to build data-driven Tmodel based on algorithm structure similarity. Meanwhile, the safety requirements containing the compressor surge and turbine inlet temperature boundary are determined, which are considered in operational performance analysis. Results show that abnormal operation data is identified during operational times 37, 38, 39, 40, 41, 42, and 248. After 254,341 minutes, the compressor efficiency degrades nearly 1%. The surge margin of a compressor is a binary function of the corrected air mass flow and inlet guide vane (IGV). The pressure ratio of the working margin moves downward by 0.11 for each 1 degrees increase in IGV. What's more, the T-model demonstrates high accuracy and can predict operational performance at high environmental temperatures, with the accuracy of turbine outlet temperature within 0.995. The unit is particularly sensitive to IGV, natural gas flow mass, compressor inlet temperature, and turbine outlet gauge pressure. When the relative humidity is 68%, the electrical power is the highest and overall efficiency is the best. Overall, this study's approach has significant potential for multidimensional analysis and performance prediction.
引用
收藏
页数:15
相关论文
共 50 条
  • [21] LP compressor blade vibration characteristics at starting conditions of a 100 MW heavy-duty gas turbine
    An Sung Lee
    Alexandre F. Vedichtchev
    KSME International Journal, 2004, 18 : 895 - 903
  • [22] LP compressor blade vibration characteristics at starting conditions of a 100 MW heavy-duty gas turbine
    Lee, AS
    Vedichtchev, AF
    KSME INTERNATIONAL JOURNAL, 2004, 18 (06): : 895 - 903
  • [23] The effects of load conditions and structural parameters on fretting wear of annular flat in heavy-duty gas turbine
    Wu, Wei
    Wang, Kai
    Wang, Xinyuan
    Yang, Lihua
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART J-JOURNAL OF ENGINEERING TRIBOLOGY, 2025, 239 (01) : 109 - 130
  • [24] A neuro-fuzzy controller for grid-connected heavy-duty gas turbine power plants
    Iqbal, Mohamed Mustafa Mohamed
    Xavier, Rayappan Joseph
    Kanakaraj, Jagannathan
    TURKISH JOURNAL OF ELECTRICAL ENGINEERING AND COMPUTER SCIENCES, 2017, 25 (03) : 2375 - 2387
  • [25] A Dynamic Firefly Algorithm-Based Fractional Order Fuzzy-PID Approach for the Control of a Heavy-Duty Gas Turbine
    Haji, Vahab Haji
    Fekih, Afef
    Monje, Concepcion A.
    IFAC PAPERSONLINE, 2020, 53 (02): : 11913 - 11919
  • [26] Vibration and noise analysis of heavy-duty trucks based on powertrain lightweighting
    Zheng, Li-Feng
    Wang, Tie
    Li, Guo-Xing
    JOURNAL OF VIBROENGINEERING, 2017, 19 (06) : 4573 - 4590
  • [27] Analysis of power split vibration absorber performance in heavy-duty truck powertrains
    Wramner, Lina
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART D-JOURNAL OF AUTOMOBILE ENGINEERING, 2020, 234 (10-11) : 2509 - 2521
  • [28] Reaction Kinetic Simulation of NOx Emission Performance for a Heavy Duty Gas Turbine
    Liu A.
    Zhu Y.
    Chen B.
    Zeng W.
    Weng Y.
    Liu K.
    Wang C.
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2017, 51 (11): : 1383 - 1390
  • [29] Directional solidification casting technology of heavy-duty gas turbine blade with liquid metal cooling(LMC) process
    Xiao-fu Liu
    Yan-chun Lou
    Bo Yu
    Gui-qiao Su
    Chang-chun Li
    Xin-li Guo
    Biao Li
    Guo-yan Shui
    ChinaFoundry, 2019, 16 (01) : 23 - 30
  • [30] Directional solidification casting technology of heavy-duty gas turbine blade with liquid metal cooling (LMC) process
    Xiao-fu Liu
    Yan-chun Lou
    Bo Yu
    Gui-qiao Su
    Chang-chun Li
    Xin-li Guo
    Biao Li
    Guo-yan Shui
    China Foundry, 2019, 16 : 23 - 30