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contributor authorM. F. Bardon
date accessioned2017-05-08T23:13:16Z
date available2017-05-08T23:13:16Z
date copyrightApril, 1982
date issued1982
identifier issn1528-8919
identifier otherJETPEZ-26772#341_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95795
description abstractIt is already well known that alcohols can be burned in open-cycle gas turbines by direct firing in the combustor. This paper demonstrates however, that there are significant improvements in thermal efficiency possible by modifying the manner in which alcohols are used in Brayton cycle engines. It is shown that injection of the alcohol during the compression process can materially improve both thermal efficiency and specific work because of the intercooling effect of evaporation. Calculations are given which demonstrate the improvement theoretically possible at representative values of peak turbine inlet temperature. It is also shown that the optimum pressure ratio for both regenerated and unregenerated cycles is different when such compressor evaporative intercooling is used rather than simply injecting the fuel into the combustor.
publisherThe American Society of Mechanical Engineers (ASME)
titleModified Brayton Cycles Utilizing Alcohol Fuels
typeJournal Paper
journal volume104
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227284
journal fristpage341
journal lastpage348
identifier eissn0742-4795
keywordsFuels
keywordsBrayton cycle
keywordsEthanol
keywordsCycles
keywordsCombustion chambers
keywordsEvaporation
keywordsGas turbines
keywordsTurbines
keywordsEngines
keywordsCompressors
keywordsPressure
keywordsTemperature
keywordsFiring (materials) AND Compression
treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002
contenttypeFulltext


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