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contributor authorJobaidur R. Khan
contributor authorMustapha Chaker
contributor authorTing Wang
date accessioned2017-05-09T00:50:36Z
date available2017-05-09T00:50:36Z
date copyrightFebruary, 2012
date issued2012
identifier issn1528-8919
identifier otherJETPEZ-27183#022001_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148918
description abstractThe output and efficiency of gas turbines are reduced significantly during the summer, especially in areas where the daytime temperature reaches as high as 50°C. Gas turbine inlet fogging and overspray has been considered a simple and cost-effective method to increase the power output. One of the most important issues related to inlet fogging is to determine the most effective location of the fogging device by determining (a) how many water droplets actually evaporate effectively to cool down the inlet air instead of colliding on the wall or coalescing and draining out (i.e., fogging efficiency), and (b) quantifying the amount of nonevaporated droplets that may reach the compressor bellmouth to ascertain the erosion risk for compressor airfoils if wet compression is to be avoided. When the silencer is installed, there is an additional consideration for placing the fogging device upstream or downstream of the silencer baffles. Placing arbitrarily the device upstream of the silencer can cause the silencer to intercept water droplets on the silencer baffles and lose cooling effectiveness. This paper employs computational fluid dynamics (CFD) to investigate the water droplet transport and cooling effectiveness with different spray locations such as before and after the silencer baffles. Analysis on the droplet history (trajectory and size) is employed to interpret the mechanism of droplet dynamics under influence of acceleration, diffusion, and body forces when the flow passes through the baffles and duct bent. The results show that, for the configuration of the investigated duct, installing the fogging system upstream of the silencer is about 3 percentage points better in evaporation effectiveness than placing it downstream of the silencer, irrespective of whether the silencer consists of a single row of baffles or two rows of staggered baffles. The evaporation effectiveness of the staggered silencer is about 0.8 percentage points higher than the single silencer. The pressure drop of the staggered silencer is 6.5% higher than the single silencer.
publisherThe American Society of Mechanical Engineers (ASME)
titleInvestigation of Cooling Effectiveness of Gas Turbine Inlet Fogging Location Relative to the Silencer
typeJournal Paper
journal volume134
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4004044
journal fristpage22001
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsGas turbines
keywordsSilencers
keywordsWater
keywordsTemperature
keywordsTurbulence
keywordsCooling
keywordsDucts
keywordsBoundary-value problems AND Evaporation
treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 002
contenttypeFulltext


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