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    Avoiding Compressor Surge During Emergency Shutdown Hybrid Turbine Systems

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 010::page 102602
    Author:
    Pezzini, Paolo
    ,
    Tucker, David
    ,
    Traverso, Alberto
    DOI: 10.1115/1.4025036
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new emergency shutdown procedure for a directfired fuel cell turbine hybrid power system was evaluated using a hardwarebased simulation of an integrated gasifier/fuel cell/turbine hybrid cycle (IGFC), implemented through the Hybrid Performance (Hyper) project at the National Energy Technology Laboratory, U.S. Department of Energy (NETL). The Hyper facility is designed to explore dynamic operation of hybrid systems and quantitatively characterize such transient behavior. It is possible to model, test, and evaluate the effects of different parameters on the design and operation of a gasifier/fuel cell/gas turbine hybrid system and provide a means of quantifying risk mitigation strategies. An openloop system analysis regarding the dynamic effect of bleed air, cold air bypass, and load bank is presented in order to evaluate the combination of these three main actuators during emergency shutdown. In the previous Hybrid control system architecture, catastrophic compressor failures were observed when the fuel and load bank were cut off during emergency shutdown strategy. Improvements were achieved using a nonlinear fuel valve ramp down when the load bank was not operating. Experiments in load bank operation show compressor surge and stall after emergency shutdown activation. The difficulties in finding an optimal compressor and cathode mass flow for mitigation of surge and stall using these actuators are illustrated.
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      Avoiding Compressor Surge During Emergency Shutdown Hybrid Turbine Systems

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    http://yetl.yabesh.ir/yetl1/handle/yetl/151704
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    contributor authorPezzini, Paolo
    contributor authorTucker, David
    contributor authorTraverso, Alberto
    date accessioned2017-05-09T00:58:32Z
    date available2017-05-09T00:58:32Z
    date issued2013
    identifier issn1528-8919
    identifier othergtp_135_10_102602.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151704
    description abstractA new emergency shutdown procedure for a directfired fuel cell turbine hybrid power system was evaluated using a hardwarebased simulation of an integrated gasifier/fuel cell/turbine hybrid cycle (IGFC), implemented through the Hybrid Performance (Hyper) project at the National Energy Technology Laboratory, U.S. Department of Energy (NETL). The Hyper facility is designed to explore dynamic operation of hybrid systems and quantitatively characterize such transient behavior. It is possible to model, test, and evaluate the effects of different parameters on the design and operation of a gasifier/fuel cell/gas turbine hybrid system and provide a means of quantifying risk mitigation strategies. An openloop system analysis regarding the dynamic effect of bleed air, cold air bypass, and load bank is presented in order to evaluate the combination of these three main actuators during emergency shutdown. In the previous Hybrid control system architecture, catastrophic compressor failures were observed when the fuel and load bank were cut off during emergency shutdown strategy. Improvements were achieved using a nonlinear fuel valve ramp down when the load bank was not operating. Experiments in load bank operation show compressor surge and stall after emergency shutdown activation. The difficulties in finding an optimal compressor and cathode mass flow for mitigation of surge and stall using these actuators are illustrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAvoiding Compressor Surge During Emergency Shutdown Hybrid Turbine Systems
    typeJournal Paper
    journal volume135
    journal issue10
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4025036
    journal fristpage102602
    journal lastpage102602
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 010
    contenttypeFulltext
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