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    Basic Limitations on the Performance of Stirling Engines

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001::page 104
    Author:
    P. C. T. de Boer
    DOI: 10.1115/1.2204629
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The performance of Stirling engines is subject to limitations resulting from power dissipation in the regenerator. The dissipation is caused by pressure gradients in the regenerator required to generate flow. Without this flow the power output would be zero. Hence the dissipation is an essential element of the operation of the engine. Using linearized theory, the pressure in the compression and expansion spaces is found as a function of the ratio of piston amplitudes and piston phase difference. The regenerator is taken to be thermally perfect. All variations are taken to be sinusoidal in time. Expressions are derived for the dimensionless power output and the thermal efficiency at a given amplitude of the compression piston. Upper bounds on the power output and the efficiency are found as function of frequency and of regenerator void volume. Special attention is given to the case of piston amplitude ratio equal to 1.
    keyword(s): Pressure , Optimization , Compression , Equations , Pistons , Stirling engines , Temperature , Flow (Dynamics) , Energy dissipation , Engines , Space AND Pressure gradient ,
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      Basic Limitations on the Performance of Stirling Engines

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    https://yetl.yabesh.ir/yetl1/handle/yetl/135776
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    contributor authorP. C. T. de Boer
    date accessioned2017-05-09T00:23:48Z
    date available2017-05-09T00:23:48Z
    date copyrightJanuary, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26935#104_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135776
    description abstractThe performance of Stirling engines is subject to limitations resulting from power dissipation in the regenerator. The dissipation is caused by pressure gradients in the regenerator required to generate flow. Without this flow the power output would be zero. Hence the dissipation is an essential element of the operation of the engine. Using linearized theory, the pressure in the compression and expansion spaces is found as a function of the ratio of piston amplitudes and piston phase difference. The regenerator is taken to be thermally perfect. All variations are taken to be sinusoidal in time. Expressions are derived for the dimensionless power output and the thermal efficiency at a given amplitude of the compression piston. Upper bounds on the power output and the efficiency are found as function of frequency and of regenerator void volume. Special attention is given to the case of piston amplitude ratio equal to 1.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBasic Limitations on the Performance of Stirling Engines
    typeJournal Paper
    journal volume129
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2204629
    journal fristpage104
    journal lastpage113
    identifier eissn0742-4795
    keywordsPressure
    keywordsOptimization
    keywordsCompression
    keywordsEquations
    keywordsPistons
    keywordsStirling engines
    keywordsTemperature
    keywordsFlow (Dynamics)
    keywordsEnergy dissipation
    keywordsEngines
    keywordsSpace AND Pressure gradient
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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