Performance Degradation Due to Fouling and Recovery After Washing in a Multistage Test CompressorSource: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003::page 031020-1Author:Casari, Nicola
,
Pinelli, Michele
,
Spina, Pier Ruggero
,
Suman, Alessio
,
Vulpio, Alessandro
DOI: 10.1115/1.4049765Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Land-based power units have to fulfill even more high levels of production and reliability. In harsh environments (desert and tropical installations, typically), the power unit ingests high amounts of dust that might deposit inside the compressor. In this paper, the analysis of a multistage compressor performance that operates under sandy and humid conditions has been assessed. The compressor units, which equips the Allison 250 C18 compressor, has been subjected to multiple runs under severe conditions of soil dust ingestion. The compressor has been operated according to subsequent runs, and at the end of each run, the performance curve was recorded; the performance losses, in terms of pressure ratio, have been measured during the operations. The characteristic curve of each run is representative of the level of contamination of the unit. Finally, the compressor has been washed, and the performance curve, in the recovered conditions, has been recorded. The results show the modification and the downward shift of the characteristic curves which lead to a gradual loss of the compressor performance. The curves realized after dust ingestion have been compared with the recovered curve after online washing. The measurement shows a promising recovery of the performances, even if the compressor flow path appears affected by localized deposits able to resist to the droplet removal action. Detailed photographic reports of the inlet guide vane (IGV) and the first compressor stages have been included in this analysis. After each run, the IGV, the rotor blade and stator vane of the first stage, and the hub and the shroud surfaces have been photographed. The pictures show the deposition patterns on the blades and the compressor surfaces. The comparison of the pictures of the internal surfaces, before and after the washing, highlights the parts that are more critical to clean and needy of attention during offline washing and overhaul.
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contributor author | Casari, Nicola | |
contributor author | Pinelli, Michele | |
contributor author | Spina, Pier Ruggero | |
contributor author | Suman, Alessio | |
contributor author | Vulpio, Alessandro | |
date accessioned | 2022-02-05T22:20:02Z | |
date available | 2022-02-05T22:20:02Z | |
date copyright | 2/24/2021 12:00:00 AM | |
date issued | 2021 | |
identifier issn | 0742-4795 | |
identifier other | gtp_143_03_031020.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4277355 | |
description abstract | Land-based power units have to fulfill even more high levels of production and reliability. In harsh environments (desert and tropical installations, typically), the power unit ingests high amounts of dust that might deposit inside the compressor. In this paper, the analysis of a multistage compressor performance that operates under sandy and humid conditions has been assessed. The compressor units, which equips the Allison 250 C18 compressor, has been subjected to multiple runs under severe conditions of soil dust ingestion. The compressor has been operated according to subsequent runs, and at the end of each run, the performance curve was recorded; the performance losses, in terms of pressure ratio, have been measured during the operations. The characteristic curve of each run is representative of the level of contamination of the unit. Finally, the compressor has been washed, and the performance curve, in the recovered conditions, has been recorded. The results show the modification and the downward shift of the characteristic curves which lead to a gradual loss of the compressor performance. The curves realized after dust ingestion have been compared with the recovered curve after online washing. The measurement shows a promising recovery of the performances, even if the compressor flow path appears affected by localized deposits able to resist to the droplet removal action. Detailed photographic reports of the inlet guide vane (IGV) and the first compressor stages have been included in this analysis. After each run, the IGV, the rotor blade and stator vane of the first stage, and the hub and the shroud surfaces have been photographed. The pictures show the deposition patterns on the blades and the compressor surfaces. The comparison of the pictures of the internal surfaces, before and after the washing, highlights the parts that are more critical to clean and needy of attention during offline washing and overhaul. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Performance Degradation Due to Fouling and Recovery After Washing in a Multistage Test Compressor | |
type | Journal Paper | |
journal volume | 143 | |
journal issue | 3 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4049765 | |
journal fristpage | 031020-1 | |
journal lastpage | 031020-11 | |
page | 11 | |
tree | Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 003 | |
contenttype | Fulltext |