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    Performance Assessment of Turbocharged Pem Fuel Cell Systems for Civil Aircraft Onboard Power Production

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002::page 21701
    Author:
    Stefano Campanari
    ,
    Uwe Wollrab
    ,
    Giampaolo Manzolini
    ,
    Andrea Beretti
    DOI: 10.1115/1.2772636
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In recent years, civil aircraft projects are showing a continuous increase in the demand of onboard electrical power, both for the partial substitution of hydraulic or pneumatic controls and drives with electrical ones, and for the consumption of new auxiliary systems developed in response to flight safety and environmental control issues. Aiming to generate onboard power with low emissions and better efficiency, several manufacturers and research groups are considering the possibility to produce a relevant fraction of the electrical power required by the aircraft by a fuel cell system. The first step would be to replace the conventional auxiliary power unit (based on a small gas turbine) with a polymer electrolyte membrane (PEM) fuel cell type, which today is favored with respect to other fuel cell types; thanks to its higher power density and faster startup. The PEM fuel cell can be fed with a hydrogen rich gas coming from a fuel reformer, operating with the same jet fuel used by the aircraft, or relying on a dedicated hydrogen storage onboard. The cell requires also an air compression unit, where the temperature, pressure, and humidity of the air stream feeding the PEM unit during land and in-flight operation strongly influence the performance and the physical integrity of the fuel cell. In this work we consider different system architectures, where the air compression system may exploit an electrically driven compressor or a turbocharger unit. The compressor type and the system pressure level are optimized according to a fuel cell simulation model, which calculates the cell voltage and efficiency as a function of temperature and pressure, calibrated over the performances of real PEM cell components. The system performances are discussed under different operating conditions, covering ground operation, and intermediate and high altitude cruise conditions. The optimized configuration is selected, presenting energy balances and a complete thermodynamic analysis.
    keyword(s): Pressure , Temperature , Fuels , Compressors , Fuel cells , Aircraft , Hydrogen , Proton exchange membrane fuel cells , Proton exchange membranes , Electric potential , Flight , Electricity (Physics) , Turbines , Flow (Dynamics) , Compression , Industrial plants AND Emissions ,
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      Performance Assessment of Turbocharged Pem Fuel Cell Systems for Civil Aircraft Onboard Power Production

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    http://yetl.yabesh.ir/yetl1/handle/yetl/137973
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorStefano Campanari
    contributor authorUwe Wollrab
    contributor authorGiampaolo Manzolini
    contributor authorAndrea Beretti
    date accessioned2017-05-09T00:28:00Z
    date available2017-05-09T00:28:00Z
    date copyrightMarch, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27001#021701_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137973
    description abstractIn recent years, civil aircraft projects are showing a continuous increase in the demand of onboard electrical power, both for the partial substitution of hydraulic or pneumatic controls and drives with electrical ones, and for the consumption of new auxiliary systems developed in response to flight safety and environmental control issues. Aiming to generate onboard power with low emissions and better efficiency, several manufacturers and research groups are considering the possibility to produce a relevant fraction of the electrical power required by the aircraft by a fuel cell system. The first step would be to replace the conventional auxiliary power unit (based on a small gas turbine) with a polymer electrolyte membrane (PEM) fuel cell type, which today is favored with respect to other fuel cell types; thanks to its higher power density and faster startup. The PEM fuel cell can be fed with a hydrogen rich gas coming from a fuel reformer, operating with the same jet fuel used by the aircraft, or relying on a dedicated hydrogen storage onboard. The cell requires also an air compression unit, where the temperature, pressure, and humidity of the air stream feeding the PEM unit during land and in-flight operation strongly influence the performance and the physical integrity of the fuel cell. In this work we consider different system architectures, where the air compression system may exploit an electrically driven compressor or a turbocharger unit. The compressor type and the system pressure level are optimized according to a fuel cell simulation model, which calculates the cell voltage and efficiency as a function of temperature and pressure, calibrated over the performances of real PEM cell components. The system performances are discussed under different operating conditions, covering ground operation, and intermediate and high altitude cruise conditions. The optimized configuration is selected, presenting energy balances and a complete thermodynamic analysis.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance Assessment of Turbocharged Pem Fuel Cell Systems for Civil Aircraft Onboard Power Production
    typeJournal Paper
    journal volume130
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2772636
    journal fristpage21701
    identifier eissn0742-4795
    keywordsPressure
    keywordsTemperature
    keywordsFuels
    keywordsCompressors
    keywordsFuel cells
    keywordsAircraft
    keywordsHydrogen
    keywordsProton exchange membrane fuel cells
    keywordsProton exchange membranes
    keywordsElectric potential
    keywordsFlight
    keywordsElectricity (Physics)
    keywordsTurbines
    keywordsFlow (Dynamics)
    keywordsCompression
    keywordsIndustrial plants AND Emissions
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 002
    contenttypeFulltext
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