scispace - formally typeset
Journal ArticleDOI

Degradation in Gas Turbine Systems

Rainer Kurz, +1 more
- 01 Jan 2001 - 
- Vol. 123, Iss: 1, pp 70-77
TLDR
In this article, the effects of degradation on the performance of a gas turbine systent degradation are discussed. But the authors focus on the degradation of the engine and not on isolated components.
Abstract
Any prime mover exhibits the effects of wear and tear over time. The problem of predicting the effects of wear and tear on the performance of any engine is still a matter of discussion. Because the function of a gas turbine is the result of the fine-tuned cooperation of many different components, the emphasis of this paper is on the gas turbine and its driven equipment (compressor or pump) as a system, rather than on isolated components. We will discuss the effect of degradation on the package as part of a complex system (e.g., a pipeline, a reinjection station, etc.). Treating the gas turbine package as a system reveals the effects of degradation on the match of the components as well as on the match with the driven equipment. This article will contribute insights into the problem of gas turbine systent degradation. Based on some detailed studies on the mechanisms that cause engine degradation, namely, changes in blade surfaces due to erosion or fouling, and the effect on the blade aerodynamics; changes in seal geometries and clearances, and the effect on parasitic flows; and changes in the combustion system (e.g., which result in different pattern factors), the effects of degradation will be discussed. The study includes a methodology to simulate the effects of engine and driven equipment degradation. With a relatively simple set of equations that describe the engine behavior, and a number of linear deviation factors which can easily be obtained from engine maps or test data, the equipment behavior for various degrees of degradation will be studied. A second model, using a stage by stage model for the engine compressor, is used to model the compressor deterioration. The authors have avoided to present figures about the speed of degradation, because it is subject to a variety of operational and design factors that typically cannot be controlled entirely.

read more

Citations
More filters
Journal ArticleDOI

Performance-based health monitoring, diagnostics and prognostics for condition-based maintenance of gas turbines: A review

TL;DR: In this paper, a systematic review of recently developed engine performance monitoring, diagnostic and prognostic techniques is presented, which provides experts, students or novice researchers and decision-makers working in the area of gas turbine engines with the state of the art for performance-based condition monitoring.
Proceedings ArticleDOI

Prognostic enhancements to diagnostic systems for improved condition-based maintenance [military aircraft]

TL;DR: In this paper, the authors present a framework for plug-and-play integration of new diagnostic and prognostic technologies into existing Naval platforms using a generic framework for developing interoperable prognostic "modules".
Journal ArticleDOI

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.
ReportDOI

Prognostic Enhancements to Diagnostic Systems for Improved Condition-Based Maintenance

TL;DR: In this paper, the authors present a framework for plug-n-play integration of new diagnostic and prognostic technologies into existing Naval platforms using a generic framework for developing interoperable prognostic modules.

Gas Turbine Performance

Rainer Kurz, +1 more
TL;DR: The impact of component degradation on individual component performance, as well as overall engine performance is discussed in this article, together with strategies to reduce the impact of degradation, and methods are introduced that allow the use of data for trending and comparison purposes.
References
More filters
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.
Journal ArticleDOI

Predicting Gas Turbine Performance Degradation Due to Compressor Fouling Using Computer Simulation Techniques

TL;DR: Etude par simulation sur ordinateur de la degradation des performances d'une turbine a gaz du fait de l'encrassement du compresseur as mentioned in this paper.
Proceedings ArticleDOI

Performance Deterioration in Industrial Gas Turbines

TL;DR: In this paper, the most important factors affecting the industrial turbine engine performance deterioration with service time are described and some approximate data on the prediction of the rate of deterioration is provided. Recommendations are made on how to detect and monitor the performance deterioration.
Journal ArticleDOI

An Approximate Analysis and Prediction Method for Tip Clearance Loss in Axial Compressors

TL;DR: In this paper, a simple model for loss created by the tip clearance flow in axial compressors is presented, based on an experimental program performed in conjunction with the Dawes three-dimensional Navier-Stokes calculation method.
Proceedings ArticleDOI

Endwall Blockage in Axial Compressors

TL;DR: In this article, a new methodology for quantifying compressor endwall blockage and an approach, using this quantification, for defining the links between design parameters, flow conditions, and the growth of blockage due to tip clearance flow is presented.