Abstract

Fouling is the most important performance degradation factor, so it is necessary to accurately predict the effect of fouling on engine performance. In the previous research, it is very difficult to accurately model the fouled axial flow compressor. This paper develops a new performance calculation method of fouled multistage axial flow compressor based on experiment result and operating data. For multistage compressor, the whole compressor is decomposed into two sections. The first section includes the first 50% stages which reflect the fouling level, and the second section includes the last 50% stages which are viewed as the clean stage because of less deposits. In this model, the performance of the first section is obtained by combining scaling law method and linear progression model with traditional stage stacking method; simultaneously ambient conditions and engine configurations are considered. On the other hand, the performance of the second section is calculated by averaged infinitesimal stage method which is based on Reynolds' law of similarity. Finally, the model is successfully applied to predict the 8-stage axial flow compressor and 16-stage LM2500-30 compressor. The change of thermodynamic parameters such as pressure ratio, efficiency with the operating time, and stage number is analyzed in detail.

Highlights

  • The performance of gas turbine is strongly influenced by environment conditions of the power plant

  • Gas turbine performance degradation over time is mainly due to the change of the blade profiles of compressor and turbine caused by fouling, corrosion, erosion, and foreign object damage (FOD)

  • The experiment data shows that the changes in mass flow rate and pressure ratio due to axial flow compressor fouling are nearly equal

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Summary

Introduction

The performance of gas turbine is strongly influenced by environment conditions of the power plant. Gas turbine performance degradation over time is mainly due to the change of the blade profiles of compressor and turbine caused by fouling, corrosion, erosion, and foreign object damage (FOD). Melino et al [6] developed a model to evaluate the performance degradation of an axial compressor due to fouling by using a stage-stacking method for the simulation of compressor behavior. This paper presents a new performance prediction method to evaluate the effect of fouling on compressor performance during the steady operation. The performance of the clean stages is estimated by averaged infinitesimal stage characteristics method

Stage-Stacking Method
Stage Performance Curve due to Compressor Fouling
Stage Performance Degradation Model
Stage Performance of Clean Stages
Performance Prediction Model of the Whole Compressor
Simulation Result Analysis
20 New and clean
Findings
Conclusions
Full Text
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