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

被引:5
|
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
  • [1] Strength Analysis of Bearing Support in Heavy-Duty Gas Turbine
    Duan, Wenbo
    Deng, Zhikai
    Cheng, Wenjie
    [J]. 2021 4TH INTERNATIONAL CONFERENCE ON ROBOTICS, CONTROL AND AUTOMATION ENGINEERING (RCAE 2021), 2021, : 321 - 325
  • [2] Integrity of heavy-duty gas turbine rotors
    Becker, B
    Termuehlen, H
    [J]. PROCEEDINGS OF THE AMERICAN POWER CONFERENCE, VOL 58, PTS I AND II, 1996, 58 : 720 - 726
  • [3] The Performance Comparison among Common Struts of Heavy-duty Gas Turbine
    Li, Jian
    Zhou, Jian
    Xu, Guohui
    Yu, Lie
    Yan, Xinping
    [J]. PROCEEDINGS OF THE 5TH INTERNATIONAL CONFERENCE ON INFORMATION ENGINEERING FOR MECHANICS AND MATERIALS, 2015, 21 : 1516 - 1521
  • [4] Prediction model of NOx emissions in the heavy-duty gas turbine combustor based on MILD combustion
    Zhao, Qiaonan
    Liu, Feng
    Jiao, Anyao
    Yang, Qiguo
    Xu, Hongtao
    Liao, Xiaowei
    [J]. ENERGY, 2023, 282
  • [5] Reliability analysis for the domestic control system of the heavy-duty gas turbine
    Zhong, Xinmeng
    Chen, Yuanye
    Fang, Fang
    Wang, Wei
    Liu, Yusheng
    [J]. Yi Qi Yi Biao Xue Bao/Chinese Journal of Scientific Instrument, 2022, 43 (09): : 131 - 139
  • [6] Failure analysis of first stage nozzle in a heavy-duty gas turbine
    Mirhosseini, Amir Masoud
    Nazari, S. Adib
    Pour, A. Maghsoud
    Haghighi, S. Etemadi
    Zareh, M.
    [J]. ENGINEERING FAILURE ANALYSIS, 2020, 109
  • [7] A dual-driven approach for refined modeling and performance analysis of heavy-duty gas turbine
    Guan, Jin
    Lv, Xiaojing
    Weng, Yiwu
    [J]. APPLIED THERMAL ENGINEERING, 2024, 244
  • [8] Impact of the Inflow Conditions on the Heavy-Duty Gas Turbine Exhaust Diffuser Performance
    Vassiliev, Vladimir
    Irmisch, Stefan
    Abdel-Wahab, Samer
    Granovskiy, Andrey
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2012, 134 (04):
  • [9] 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
  • [10] 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