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contributor authorA. P. Tarabrin
contributor authorV. A. Schurovsky
contributor authorA. I. Bodrov
contributor authorJ.-P. Stalder
date accessioned2017-05-08T23:58:12Z
date available2017-05-08T23:58:12Z
date copyrightApril, 1998
date issued1998
identifier issn0889-504X
identifier otherJOTUEI-28665#256_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121325
description abstractThe paper describes the phenomenon of axial compressor fouling due to aerosols contained in the air. Key parameters having effect on the level of fouling are determined. A mathematical model of a progressive compressor fouling using the stage-by-stage calculation method is developed. Calculation results on the influence of fouling on the compressor performance are presented. A new index of sensitivity of axial compressors to fouling is suggested. The paper gives information about Turbotect’s deposit cleaning method of compressor blading and the results of its application on an operating industrial gas turbine. Regular on-line and off-line washings of the compressor flow path make it possible to maintain a high level of engine efficiency and output.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Analysis of Axial Compressor Fouling and a Blade Cleaning Method
typeJournal Paper
journal volume120
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841400
journal fristpage256
journal lastpage261
identifier eissn1528-8900
keywordsCompressors
keywordsBlades
keywordsIndustrial gases
keywordsTurbines
keywordsFlow (Dynamics)
keywordsAerosols AND Engines
treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
contenttypeFulltext


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