A thermodynamics-informed deep learning approach for lightweight modeling of gas turbine performance

被引:0
|
作者
Jiang, Xiaomo [1 ,3 ]
Liu, Yiyang [2 ]
Wei, Manman [3 ]
Cheng, Xueyu [4 ]
Wang, Zhicheng [3 ,5 ]
机构
[1] Dalian Univ Technol, State Key Lab Struct Anal Optimizat & CAE Software, Prov Key Lab Digital Twin Ind Equipment, Dalian 116024, Peoples R China
[2] Dalian Univ Technol, Sch Mech & Aerosp Engn, Dalian 116024, Peoples R China
[3] Dalian Univ Technol, Sch Energy & Power Engn, Dalian 116024, Peoples R China
[4] Clayton State Univ, Coll Arts & Sci, Morrow, GA 30260 USA
[5] Dalian Univ Technol, Lab Ocean Energy Utilizat, Minist Educ, Dalian 116024, Peoples R China
基金
芬兰科学院;
关键词
Gas turbine; Thermodynamic heat balance; Performance modeling; Lightweight method; Deep learning operator networks; SIMULATION;
D O I
10.1016/j.engappai.2025.110022
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Lightweight performance modeling approaches are particularly crucial in the condition monitoring system of a heavy-duty gas turbine (HDGT) to track its efficiency changes over time accurately and promptly. This ensures sufficient productivity through a well-planned predictive maintenance strategy. This paper introduces a physics-informed deep learning methodology for lightweight modeling of HDGT performance, aimed at areal- time degradation monitoring for predictive maintenance. Initially, a mechanism-based thermodynamic model is established to serve as a performance benchmark. Subsequently, corrections are applied by adjusting base-load operating conditions to reference conditions, thereby mitigating the influence of ambient conditions and power demand. A substitute model called deep operator networks (DeepONet) is then constructed by integrating actual and simulation data to rapidly obtain crucial gas turbine performance parameters, such as compressor and turbine efficiency, as well as corrected power output and heat rate of the system. A standardized procedure is developed to automate the efficient performance modeling for gas turbines. To showcase the benefits of the proposed methodology and procedure, a comparative study with three different classical models is conducted using data from two various real-world HDGT machines. The DeepONet deep learning model is utilized to rapidly generate multivariate performance results for a gas turbine at 10ms for a single-step prediction, significantly faster than the physics-based model, which takes 6s. The prediction error is less than 0.1% on average when compared to the latter. Numerical results demonstrate that the proposed methodology offers a promising tool for real-time performance prediction of a gas turbine for predictive maintenance purposes.
引用
收藏
页数:19
相关论文
共 50 条
  • [21] Physics-informed deep learning model in wind turbine response prediction
    Li, Xuan
    Zhang, Wei
    RENEWABLE ENERGY, 2022, 185 : 932 - 944
  • [22] A novel data-driven deep learning approach for wind turbine power curve modeling
    Wang, Yun
    Duan, Xiaocong
    Zou, Runmin
    Zhang, Fan
    Li, Yifen
    Hu, Qinghua
    ENERGY, 2023, 270
  • [23] Facial expression recognition using lightweight deep learning modeling
    Ahmad, Mubashir
    Saira
    Alfandi, Omar
    Khattak, Asad Masood
    Qadri, Syed Furqan
    Saeed, Iftikhar Ahmed
    Khan, Salabat
    Hayat, Bashir
    Ahmad, Arshad
    MATHEMATICAL BIOSCIENCES AND ENGINEERING, 2023, 20 (05) : 8208 - 8225
  • [24] Deep Residual Learning applied to real-gas thermodynamics
    Ge, Yipeng
    Hansinger, Maximilian
    Traxinger, Christoph
    Pfitzner, Michael
    INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN SCIENCES AND ENGINEERING 2018 (ICCMSE-2018), 2018, 2040
  • [25] Modeling the air-cooled gas turbine: Part 1 - General thermodynamics
    Young, JB
    Wilcock, RC
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2002, 124 (02): : 207 - 213
  • [26] A digital twin approach for gas turbine performance based on deep multi-model fusion
    Zhang, Jingkai
    Wang, Zhitao
    Li, Shuying
    Wei, Pengfei
    APPLIED THERMAL ENGINEERING, 2024, 246
  • [27] MODELING AND ANALYSIS OF GAS-TURBINE PERFORMANCE DETERIORATION
    LAKSHMINARASIMHA, AN
    BOYCE, MP
    MEHERHOMJI, CB
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1994, 116 (01): : 46 - 52
  • [28] Performance deterioration modeling in aircraft gas turbine engines
    Zaita, AV
    Buley, G
    Karlsons, G
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1998, 120 (02): : 344 - 349
  • [29] Performance Modeling of a Modern Gas Turbine for Dispatch Optimization
    Boksteen, S. Z.
    van der Vecht, D. J.
    Pecnik, R.
    van Buijtenen, J. P.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 3, 2012, : 835 - +
  • [30] SIMULATION OF A GAS TURBINE ENGINE WITH PERFORMANCE DEGRADATION MODELING
    Campora, Ugo
    Carretta, Mauro
    Cravero, Carlo
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2011, VOL 1, 2012, : 1 - +