Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines

Liquefied gas reaction turbines are subject to the hydraulic affinity laws. Particularly for liquefied hydrocarbon gas-driven turbines, deviations from the affinity laws are encountered. In the case of reaction turbines, where the geometry is fixed, the affinity law relationships between flow, head,...

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Main Author: Sarah D. Alison-Youel
Format: Article
Language:English
Published: Hindawi Limited 2008-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/2008/737285
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spelling doaj-c56ec19cd6a84312bc1a85dbe36b9c1b2020-11-24T21:28:15ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1542-30342008-01-01200810.1155/2008/737285737285Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction TurbinesSarah D. Alison-Youel0Research and Development, Cryodynamics Division, Ebara International Corporation, 350 Salomon Circle, Sparks, NV 89434, USALiquefied gas reaction turbines are subject to the hydraulic affinity laws. Particularly for liquefied hydrocarbon gas-driven turbines, deviations from the affinity laws are encountered. In the case of reaction turbines, where the geometry is fixed, the affinity law relationships between flow, head, and rotational speed are relevant. Field experience confirms that the affinity law relationships are adequate, but that the predictions made also tend to deviate from real turbine performance. Part of the deviations seen may be attributed to the nonideal fluid; however, further examination is warranted. This paper presents an investigation into the affinity law relationships between head, flow, and rotational speed in conjunction with actual turbine performance. The three basic affinity law relationships are combined to form the most general performance equation. This equation subsequently incorporates both the affinity law relationships and the conservation of energy principal. Application of real turbine test data shows that this general performance equation presents a more accurate representation of turbine performance than the affinity law relationships alone.http://dx.doi.org/10.1155/2008/737285
collection DOAJ
language English
format Article
sources DOAJ
author Sarah D. Alison-Youel
spellingShingle Sarah D. Alison-Youel
Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
International Journal of Rotating Machinery
author_facet Sarah D. Alison-Youel
author_sort Sarah D. Alison-Youel
title Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
title_short Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
title_full Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
title_fullStr Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
title_full_unstemmed Observation and Analysis of Affinity Law Deviations through Tested Performance of Liquefied Gas Reaction Turbines
title_sort observation and analysis of affinity law deviations through tested performance of liquefied gas reaction turbines
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
1542-3034
publishDate 2008-01-01
description Liquefied gas reaction turbines are subject to the hydraulic affinity laws. Particularly for liquefied hydrocarbon gas-driven turbines, deviations from the affinity laws are encountered. In the case of reaction turbines, where the geometry is fixed, the affinity law relationships between flow, head, and rotational speed are relevant. Field experience confirms that the affinity law relationships are adequate, but that the predictions made also tend to deviate from real turbine performance. Part of the deviations seen may be attributed to the nonideal fluid; however, further examination is warranted. This paper presents an investigation into the affinity law relationships between head, flow, and rotational speed in conjunction with actual turbine performance. The three basic affinity law relationships are combined to form the most general performance equation. This equation subsequently incorporates both the affinity law relationships and the conservation of energy principal. Application of real turbine test data shows that this general performance equation presents a more accurate representation of turbine performance than the affinity law relationships alone.
url http://dx.doi.org/10.1155/2008/737285
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