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Greening the future of transport by using a regenerative variable geometry gas turbine engine

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Gas turbine engines are cleaner, have multi-fuel capability, and a lower volume to power ratio than piston engines. A main disadvantage of gas turbine engines in automotive use is their poor part-load efficiency. As transport engines spend most of their operating life at part-load; a gas turbine engine that achieves a wide range of high-efficiency should be used. This paper aims to develop a computer model to simulate the performance of regenerative gas turbine engines for transport use. A computer program for the performance prediction was designed based on the characteristics of each component in the engine and the compatibility between them. The influence of a variable power turbine setting-angle on engine performance was investigated. Compressor and turbines maps were used in a particular form; hence, each point on the map has a specific value of rotational speed, pressure ratio, mass flow rate, and efficiency. Variation in effectiveness of the regenerator was considered. Variable pressure drop and mass flow rate across the combustion chamber and the regenerator were included.
Rocznik
Strony
259--269
Opis fizyczny
Bibliogr. 17 poz., rys., tab., wykr.
Twórcy
  • Jordan University of Science and Technology, Ar Ramtha, Irbid 22110, Jordan
  • University of Tabuk, Tabuk 71491, Saudi Arabia
Bibliografia
  • [1] D. Barbeau, The Performance of Vehicle Gas Turbines. SAE Technical Paper 670198 (1967). doi:10.4271/670198.
  • [2] D. Wilson, K. Theodosios, Models for predicting the performance of brayton-cycle engines, Engineering for Gas Turbines and Power 116 (1994) 381–388.
  • [3] R. Whalley, M. Ebrahimi, Automotive gas turbine regulation, IEEE transaction on Control Systems Technology 12 (3) (2004) 465–473.
  • [4] A. Juhasz, Automotive gas turbine power systemperformance analysis code, NASA Technical Memorandum 107386 (1997) 1–5.
  • [5] A. Lazzaretto, A. Toffolo, Analytical and neural network models for gas turbine design and off-design simulation, Applied Thermodynamics 4 (4) (2001) 173–182.
  • [6] S. Companari, Full load and part-load performance prediction for integrated sofc and microturbine systems, Engineering for Gas Turbines and Power 121 (2000) 239–246.
  • [7] J. Kim, T. Kim, J. Sohn, S. Ro, Comparative analysis of off-design performance characteristics of single and twoshaft industrial gas turbines, Engineering for Gas Turbines and Power 125 (2003) 954–960.
  • [8] T. Kim, S. Hwang, Part load performance analysis of recuperated gas turbines considering engine configuration and operation strategy, Energy 31 (2006) 260–277.
  • [9] K. McLallin, M. Kofskey, Cold-air performance of free power turbine designed for 112-kilo Watt automotive gasturbine engine, Tech. rep., USA DOE/NASA (February 1979).
  • [10] D.Wilson, K. Theodosios, The Design of High-Efficiency Turbomachinery and Gas Turbines, 2nd Edition, Prentice-Hall Inc, New Jersey, 1998.
  • [11] W. Bathie, Fundamentals of Gas Turbines, 2nd Edition, John Wiley and Sons Inc, New York, 1996.
  • [12] H. Saravanamuttoo, G. Rogers, H. Cohen, Gas Turbine Theory, 5th Edition, Pearson Education Limited, London, 2001.
  • [13] J. Horlock, Axial Flow Turbines, Butterworths, London, 1966.
  • [14] W. Kays, A. London, Compact Heat Exchangers, 3rd Edition, McGraw-Hill Company, New York, 1984.
  • [15] P. Walsh, P. Fletcher, Gas Turbine Performance, 2nd Edition, Blackwell Science and ASME, New Jersey, 2004.
  • [16] R. Harman, Gas Turbine Engineering, Macmillan Press LTD, London, 1981.
  • [17] F. Haglind, Variable geometry gas turbines for improving the part load performance of marine combined cyclescombined cycle performance, Applied Thermal Engineering 31 (2011) 467–476.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-0880ffac-4f28-42e1-9d4c-074678764dcc
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