Optimal design of the regenerative gas turbine engine with isothermal heat addition

被引:46
|
作者
Erbay, LB [1 ]
Göktun, S
Yavuz, H
机构
[1] Osmangazi Univ, Sch Engn, TR-26480 Bati Meselik, Eskisehir, Turkey
[2] Istanbul Tech Univ, Maritime Fac, TR-81716 Istanbul, Turkey
[3] Istanbul Tech Univ, Inst Nucl Energy, TR-80626 Istanbul, Turkey
关键词
D O I
10.1016/S0306-2619(00)00055-6
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
A regenerative gas turbine engine, with isothermal heat addition, working under the frame of a Brayton cycle has been analyzed. With the purpose of having a more efficient small-sized gas turbine engine, the optimization has been carried out numerically using the maximum power (MP) and maximum power density (MPD) method. The effects of internal irreversibilities have been considered in terms of the isentropic efficiencies of the turbine and compressor and of the regenerator efficiency. The results summarized by figures show that the regenerative gas turbine engine, with isothermal heat addition, designed according to the maximum power density condition gives the best performance and exhibits highest cycle efficiencies. (C) 2001 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:249 / 264
页数:16
相关论文
共 50 条
  • [21] Conjugate Heat Transfer Validation of Gas Turbine Engine Cooling Turbine Vanes
    Gorelov Y.G.
    Russian Aeronautics, 2023, 66 (02): : 316 - 324
  • [22] The Design and Realization of Gas Turbine Engine Test Visualization
    Li, Xunbo
    Liu, Dewu
    Hu, Tianyou
    Shen, Yan
    Yuan, Taiwen
    2008 INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION: (ICMA), VOLS 1 AND 2, 2008, : 1110 - 1114
  • [23] Control configuration design for the aircraft gas turbine engine
    Rolls-Royce plc, Bristol, United Kingdom
    Comput Control Eng J, 1 (22-28):
  • [24] Aerodynamic design of gas turbine engine intake duct
    Soemarwoto, Bambang I.
    Boelens, Okko J.
    Kanakis, Toni
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2016, 88 (05): : 605 - 612
  • [25] Design Technique of Sealing System in Gas Turbine Engine
    Samara University, Department of Aircraft Engine Construction and Design, Samara, Russia
    IEEE Int. Conf. Electron. Technol., ICET, 2022, (390-394):
  • [26] The improvement achieved by isothermal forging for a γ-TiAl based gas turbine engine material
    Huang, ZW
    Bowen, P
    Davey, S
    Blenkinsop, PA
    ADVANCES IN TURBINE MATERIALS, DESIGN AND MANUFACTURING, 1997, : 489 - 502
  • [27] Effect of heat resistance on the performance of closed gas turbine regenerative cycles
    Chen, Lingen
    Sun, Fengrui
    Wu, Chih
    International Journal of Power and Energy Systems, 1999, 19 (02): : 141 - 145
  • [28] Advanced machining technology for gas turbine and heat engine components
    Pujari, V. K.
    Vartabedian, A.
    Collins, W. T.
    INDUSTRIAL CERAMICS, 2010, 30 (02): : 129 - 132
  • [29] CONJUGATE HEAT TRANSFER APPROACH TO GAS TURBINE ENGINE MODELING
    Mulla, Jaasim
    Satpathy, R. K.
    Kaka, Fiyanshu
    PROCEEDINGS OF ASME 2023 GAS TURBINE INDIA CONFERENCE, GTINDIA2023, 2023,
  • [30] HEAT-TRANSFER IN THE BLADING OF A GAS-TURBINE ENGINE
    DORFMAN, AS
    DAVYDENKO, BV
    THERMAL ENGINEERING, 1988, 35 (11) : 627 - 630