Off-design performance of gas turbine power units with alternative load-control strategies

被引:0
|
作者
Pan Z. [1 ]
Lin Z. [1 ]
Fan K. [2 ]
Yang C. [2 ]
Ma X. [2 ]
机构
[1] Guangzhou Zhujiang LNG Power Generation Co., Ltd., Guangzhou
[2] School of Electric Power, South China University of Technology, Guangzhou
关键词
Comparative simulation; Gas turbine; Operating strategy; Part load performance;
D O I
10.32604/EE.2020.013585
中图分类号
学科分类号
摘要
Gas turbine power units, as an effective way to cope with the severe challenge of renewable energy accommodation in power grids, arouse the interest of power enterprises in the deep peak-load regulation performance. Two common alternative load-control strategies including constant turbine inlet temperature (TIT) and constant turbine exhaust temperature (TET) regulations were taken into consideration. To comparatively investigate the part-load performance under these strategies, both mathematical and physical models were set up successively to serve as a validation and complementary to each other. For the mathematical model of compressor with inlet guide vane (IGV), combustor and turbine, stage-stacking method based on blade average geometric parameter, energy con-servation and turbine stage model were adopted respectively. For the physical model, design and off-design analysis were carried out based on GT PRO and THERMOFLEX respectively. The simulation result of mathematical model vali-dated the reliability of the physical model. Based on this, the influence of ambient temperature and different load-regulating strategies on the off-design performance of gas turbine power units was studied in THERMOFLEX. The results in the case of a PG 9351FA gas turbine show that the ambient temperature has a great impact on system performance, i.e., every 5°C increase in the ambient temperature pro-duces a reduction of 3.7% in the relative full-load output and 1.1% in the relative efficiency respectively; when the gas turbine operates under constant TIT strategy, TET starts to rise till it reaches the maximum allowable value with the load rate decreasing, and IGV keeps at the minimum angle with both TIT and TET decreasing when the load rate is lower than 65%; when the gas turbine operates under constant TET strategy, TIT drops slightly at load rate of above 60% while both TIT and TET evidently decrease below 60% load rate operating along the constant corrected speed line at the minimum allowable IGV opening; gas turbine efficiency is greatly affected by load rate and the performance degradation is more obvious especially in lower load rate regions; constant TET strategy is superior in the operating efficiency to constant TIT strategy under part-load conditions. © 2021, Tech Science Press. All rights reserved.
引用
收藏
页码:119 / 141
页数:22
相关论文
共 50 条
  • [1] Effects of different alternative control methods for gas turbine on the off-design performance of a trigeneration system
    Wang, Zefeng
    Han, Wei
    Zhang, Na
    Su, Bosheng
    Gan, Zhongxue
    Jin, Hongguang
    Applied Energy, 2018, 215 : 227 - 236
  • [2] PERFORMANCE SIMULATION AND OFF-DESIGN PERFORMANCE CONTROL OF REHEAT GAS TURBINE ENGINES
    Li, Yi-Guang
    Liu, Yang
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 8, 2024,
  • [3] Off-design performance control and simulation for gas turbine engines with sequential combustors
    Li, Yi-Guang
    Liu, Yang
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2025,
  • [4] Design and off-design characteristics of the alternative recuperated gas turbine cycle with divided turbine expansion
    Hwang, Sung Hoon
    Yoon, Soo Hyung
    Kim, Tong Seop
    PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 4, 2006, : 459 - 468
  • [5] Off-design performance analysis of hybridised aircraft gas turbine
    Zhao, X.
    Sahoo, S.
    Kyprianidis, K.
    Rantzer, J.
    Sielemann, M.
    AERONAUTICAL JOURNAL, 2019, 123 (1270): : 1999 - 2018
  • [6] ANALYSIS OF OFF-DESIGN POINT PERFORMANCE OF GAS TURBINE.
    Tsujikawa, Yoshiharu
    Sawada, Teruo
    Nagaoka, Makoto
    Tsukamoto, Yujiro
    Bulletin of the University of Osaka Prefecture, Series A Engineering and Natural Sciences, 1986, 35 (02): : 111 - 120
  • [7] DIRECT OFF-DESIGN PERFORMANCE PREDICTION OF MICRO GAS TURBINE ENGINE FOR DISTRIBUTED POWER GENERATION
    Barannik, Valentyn
    Burlaka, Maksym
    Moroz, Leonid
    Nassar, Abdul
    PROCEEDINGS OF THE ASME GAS TURBINE INDIA CONFERENCE, 2017, VOL 1, 2018,
  • [8] Design Optimization of a Gas Turbine Engine for Marine Applications: Off-Design Performance and Control System Considerations
    Machmudah, Affiani
    Lemma, Tamiru Alemu
    Solihin, Mahmud Iwan
    Feriadi, Yusron
    Rajabi, Armin
    Afandi, Mohamad Imam
    Abbasi, Aijaz
    ENTROPY, 2022, 24 (12)
  • [9] Gas turbine off-design performance adaptation using a genetic algorithm
    Lo Gatto, E.
    Li, Y. G.
    Pilidis, P.
    Proceedings of the ASME Turbo Expo 2006, Vol 2, 2006, : 551 - 560
  • [10] Effect of Variation of Fuel Composition on Gas Turbine Off-Design Performance
    Park, Yesuel
    Park, Saemi
    Lee, Joongseong
    Choi, Gyungmin
    ELECTRONICS, MECHATRONICS AND AUTOMATION III, 2014, 666 : 194 - +