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contributor authorWebb, J.
contributor authorCasaday, B.
contributor authorBarker, B.
contributor authorBons, J. P.
contributor authorGledhill, A. D.
contributor authorPadture, N. P.
date accessioned2017-05-09T01:03:36Z
date available2017-05-09T01:03:36Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_2_021033.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153445
description abstractAn accelerated deposition test facility was operated with four different coal ash species to study the effect of ash composition on deposition rate and spatial distribution. The facility seeds a combusting (natural gas) flow with 10–20 micron mass mean diameter coal ash particulate. The particulateladen combustor exhaust is accelerated through a rectangulartoannular transition duct and expands to ambient pressure through a nozzle guide vane annular sector. For the present study, the annular cascade consisted of two CFM56 aeroengine vane doublets, comprising three full passages and two half passages of flow. The inlet Mach number (0.1) and gas temperature (1100 آ°C) are representative of operating turbines. Ash samples were tested from the three major coal ranks: lignite, subbituminous, and bituminous. Investigations over a range of inlet gas temperatures from 900 آ°C to 1120 آ°C showed that deposition increased with temperature, though the threshold for deposition varied with ash type. Deposition levels varied with coal rank, with lignite producing the largest deposits at the lowest temperature. Regions of heightened deposition were noted; the leading edge and pressure surface being particularly implicated. Scanning electron microscopy was used to identify deposit structure. For a limited subset of tests, film cooling was employed at nominal design operating conditions but provided minimal protection in cases of severe deposition.
publisherThe American Society of Mechanical Engineers (ASME)
titleCoal Ash Deposition on Nozzle Guide Vanes—Part I: Experimental Characteristics of Four Coal Ash Types
typeJournal Paper
journal volume135
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4006571
journal fristpage21033
journal lastpage21033
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 002
contenttypeFulltext


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