The evaporative inlet cooling systems do not work well in humid areas. However, desiccant wheels can be used to dehumidify the air before passing it through the evaporative cooler. A previous study of combined direct and indirect evaporative coolers showed that a single desiccant wheel does not offer much higher effectiveness compared with the multistage evaporative systems. In this paper, additional dehumidification and indirect evaporative cooling stages are added to increase the effectiveness of the desiccant-based inlet cooling. A typical gas turbine cycle along with an industrial gas turbine with actual performance curves are used to study the performance of the proposed system in three different climatic conditions. It is shown that the added stages substantially improve the effectiveness of the desiccant-based inlet cooling.
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e-mail: a.a.zadpoor@tudelft.nl
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May 2009
Technical Briefs
Development of an Improved Desiccant-Based Evaporative Cooling System for Gas Turbines
Amir Abbas Zadpoor,
Amir Abbas Zadpoor
Faculty of Aerospace Engineering,
e-mail: a.a.zadpoor@tudelft.nl
Delft University of Technology
, Kluyverweg 1, Delft 2629HS, The Netherlands
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Ali Asadi Nikooyan
Ali Asadi Nikooyan
Faculty of Mechanical, Maritime and Materials Engineering,
Delft University of Technology
, Mekelweg 2, Delft 2628CD, The Netherlands
Search for other works by this author on:
Amir Abbas Zadpoor
Faculty of Aerospace Engineering,
Delft University of Technology
, Kluyverweg 1, Delft 2629HS, The Netherlandse-mail: a.a.zadpoor@tudelft.nl
Ali Asadi Nikooyan
Faculty of Mechanical, Maritime and Materials Engineering,
Delft University of Technology
, Mekelweg 2, Delft 2628CD, The NetherlandsJ. Eng. Gas Turbines Power. May 2009, 131(3): 034506 (5 pages)
Published Online: February 19, 2009
Article history
Received:
June 20, 2008
Revised:
July 22, 2008
Published:
February 19, 2009
Citation
Zadpoor, A. A., and Nikooyan, A. A. (February 19, 2009). "Development of an Improved Desiccant-Based Evaporative Cooling System for Gas Turbines." ASME. J. Eng. Gas Turbines Power. May 2009; 131(3): 034506. https://doi.org/10.1115/1.3030875
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