Modified Brayton Cycles Utilizing Alcohol FuelsSource: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002::page 341Author:M. F. Bardon
DOI: 10.1115/1.3227284Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: It 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.
keyword(s): Fuels , Brayton cycle , Ethanol , Cycles , Combustion chambers , Evaporation , Gas turbines , Turbines , Engines , Compressors , Pressure , Temperature , Firing (materials) AND Compression ,
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| contributor author | M. F. Bardon | |
| date accessioned | 2017-05-08T23:13:16Z | |
| date available | 2017-05-08T23:13:16Z | |
| date copyright | April, 1982 | |
| date issued | 1982 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26772#341_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95795 | |
| description abstract | It 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Modified Brayton Cycles Utilizing Alcohol Fuels | |
| type | Journal Paper | |
| journal volume | 104 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3227284 | |
| journal fristpage | 341 | |
| journal lastpage | 348 | |
| identifier eissn | 0742-4795 | |
| keywords | Fuels | |
| keywords | Brayton cycle | |
| keywords | Ethanol | |
| keywords | Cycles | |
| keywords | Combustion chambers | |
| keywords | Evaporation | |
| keywords | Gas turbines | |
| keywords | Turbines | |
| keywords | Engines | |
| keywords | Compressors | |
| keywords | Pressure | |
| keywords | Temperature | |
| keywords | Firing (materials) AND Compression | |
| tree | Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002 | |
| contenttype | Fulltext |