Axial Compressor Deterioration Caused by Saltwater Ingestion
TLDR
In this article, the axial compressor of a General Electric J85-13 jet engine was degraded by spraying atomized droplets of saltwater into the engine intake, and the results of laboratory analysis of the salt deposits are presented, providing insight into the increased surface roughness and the deposit thickness and distribution.Abstract:
Gas turbine performance deterioration can be a major economic factor. An example is within offshore installations where a degradation of gas turbine performance can mean a reduction of oil and gas production. This paper describes the test results from a series of accelerated deterioration tests on a General Electric J85-13 jet engine. The axial compressor was deteriorated by spraying atomized droplets of saltwater into the engine intake. The paper presents the overall engine performance deterioration as well as deteriorated stage characteristics. The results of laboratory analysis of the salt deposits are presented, providing insight into the increased surface roughness and the deposit thickness and distribution. The test data show good agreement with published stage characteristics and give valuable information regarding stage-by-stage performance deterioration.read more
Citations
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Book ChapterDOI
Boundary Layer Theory
TL;DR: The boundary layer equations for plane, incompressible, and steady flow are described in this paper, where the boundary layer equation for plane incompressibility is defined in terms of boundary layers.
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A Review of Surface Roughness Effects in Gas Turbines
TL;DR: In this article, the effects of surface roughness on gas turbine performance are reviewed based on publications in the open literature over the past 60 years, and the conclusion remains that considerable research is yet necessary to fully understand the role of roughness in gas turbines.
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Performance-Based Gas Turbine Health Monitoring, Diagnostics, and Prognostics: A Survey
TL;DR: This paper focuses on surveying state-of-the-art condition monitoring, diagnostic and prognostic techniques using performance parameters acquired from gas-path data that are mostly available from the operating systems of gas turbines.
Proceedings ArticleDOI
Fouling Mechanisms in Axial Compressors
Rainer Kurz,Klaus Brun +1 more
TL;DR: Fouling is caused by the adherence of particles to airfoils and annulus surfaces, and the result is a build-up of material that causes increased surface roughness and to some degree changes the shape of the airfoil as mentioned in this paper.
References
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Book ChapterDOI
Boundary Layer Theory
TL;DR: The boundary layer equations for plane, incompressible, and steady flow are described in this paper, where the boundary layer equation for plane incompressibility is defined in terms of boundary layers.
Book
Gas turbine theory
TL;DR: In this article, the authors present an analysis of the performance of simple gas turbines for aircraft propulsion and demonstrate that simple gas turbine cycles can be used to achieve state-of-the-art performance.
Book
Gas Turbine Performance
TL;DR: In this paper, the authors present guidelines for engineers on how to achieve optimum fuel efficiency, stability, and emissions control in a gas turbine system, including the effects of liquid, vapor and ice on gas turbines, and examines fuel and oil properties and their impact on performance.
Journal ArticleDOI
Loss Sources and Magnitudes in Axial-Flow Compressors
C. C. Koch,Leroy H. Smith +1 more