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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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