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contributor authorM. De Lucia
contributor authorV. Boggio
contributor authorC. Lanfranchi
date accessioned2017-05-08T23:50:05Z
date available2017-05-08T23:50:05Z
date copyrightJuly, 1996
date issued1996
identifier issn1528-8919
identifier otherJETPEZ-26756#598_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116912
description abstractCompressor inlet air cooling is an effective method for enhancing the performance of gas turbine plants. This paper presents a comparative analysis of different solutions for cooling the compressor inlet air for the LM6000 gas turbine in a cogeneration plant operated in base load. Absorption and evaporative cooling systems are considered and their performance and economic benefits compared for the dry low-NOx LM6000 version. Reference is made to two sites in Northern and Southern Italy, whose climatic data series for modeling the variations in ambient temperature during the single day were used to account for the effects of climate in the simulation. The results confirmed the advantages of inlet air cooling systems. In particular, evaporative cooling proved to be cost effective, though capable of supplying only moderate cooling, while absorption systems have a higher cost but are also more versatile and powerful in base-load operation. An integration of the two systems proved to be able to give both maximum performance enhancement and net economic benefit.
publisherThe American Society of Mechanical Engineers (ASME)
titleBenefits of Compressor Inlet Air Cooling for Gas Turbine Cogeneration Plants
typeJournal Paper
journal volume118
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2816690
journal fristpage598
journal lastpage603
identifier eissn0742-4795
keywordsCooling
keywordsCompressors
keywordsGas turbines
keywordsCombined heat and power
keywordsIndustrial plants
keywordsStress
keywordsEvaporative cooling
keywordsAbsorption
keywordsTemperature
keywordsCooling systems
keywordsSimulation
keywordsModeling AND Climate
treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003
contenttypeFulltext


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