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contributor authorAbdalla M. Al-Amiri
contributor authorMontaser M. Zamzam
contributor authorSenior Mechanical Engineer
date accessioned2017-05-09T00:16:14Z
date available2017-05-09T00:16:14Z
date copyrightJanuary, 2005
date issued2005
identifier issn1528-8919
identifier otherJETPEZ-26854#159_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131836
description abstractThe current study is centered on assessing the benefits of incorporating combustion turbine inlet air-cooling systems into a reference combustion turbine plant, which is based on a simple cycle under base load mode. Actual climatic conditions of a selected site were examined thoroughly to identify the different governing weather patterns. The main performance characteristics of both refrigerative and evaporative cooling systems were explored by examining the effect of several parameters including inlet air temperature, airflow-to-turbine output ratio, coefficient of performance (for refrigerative cooling systems), and evaporative degree hours (for evaporative cooling systems). The impact of these parameters was presented against the annual gross energy increase, average heat rate reduction, cooling load requirements and net power increase. Finally, a feasibility design chart was constructed to outline the economic returns of employing a refrigerative cooling unit against different prescribed inlet air temperature values using a wide range of combustion turbine mass flow rates.
publisherThe American Society of Mechanical Engineers (ASME)
titleSystematic Assessment of Combustion Turbine Inlet Air-Cooling Techniques
typeJournal Paper
journal volume127
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1805008
journal fristpage159
journal lastpage169
identifier eissn0742-4795
keywordsTemperature
keywordsCooling
keywordsCombustion
keywordsCooling systems
keywordsDesign
keywordsTurbines
keywordsHeat
keywordsEvaporative cooling
keywordsFlow (Dynamics) AND Stress
treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001
contenttypeFulltext


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