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    Systematic Assessment of Combustion Turbine Inlet Air-Cooling Techniques

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001::page 159
    Author:
    Abdalla M. Al-Amiri
    ,
    Montaser M. Zamzam
    ,
    Senior Mechanical Engineer
    DOI: 10.1115/1.1805008
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
    keyword(s): Temperature , Cooling , Combustion , Cooling systems , Design , Turbines , Heat , Evaporative cooling , Flow (Dynamics) AND Stress ,
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      Systematic Assessment of Combustion Turbine Inlet Air-Cooling Techniques

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/131836
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    • Journal of Engineering for Gas Turbines and Power

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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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