Abstract

The lack of gas turbine field data, especially faulty engine data, and the complexity of fault embedding into gas turbines on test benches cause difficulties in representing healthy and faulty engines in diagnostic algorithms. Instead, different gas turbine models are often used. The available models fall into two main categories: physics-based and data-driven. Given the models’ importance and necessity, a variety of simulation tools were developed with different levels of complexity, fidelity, accuracy, and computer performance requirements. Physics-based models constitute a diagnostic approach known as Gas Path Analysis (GPA). To compute fault parameters within GPA, this paper proposes to employ a nonlinear data-driven model and the theory of inverse problems. This will drastically simplify gas turbine diagnosis. To choose the best approximation technique of such a novel model, the paper employs polynomials and neural networks. The necessary data were generated in the GasTurb software for turboshaft and turbofan engines. These input data for creating a nonlinear data-driven model of fault parameters cover a total range of operating conditions and of possible performance losses of engine components. Multiple configurations of a multilayer perceptron network and polynomials are evaluated to find the best data-driven model configurations. The best perceptron-based and polynomial models are then compared. The accuracy achieved by the most adequate model variation confirms the viability of simple and accurate models for estimating gas turbine health conditions.

Highlights

  • Reliable gas turbine health information is essential for successful the implementation of condition-based maintenance [1] Gas-path diagnostic techniques provide such information by analyzing engine performance and early identifying potential faults before they develop into serious accidents [2]

  • Engine components are presented in the model by experimental component performance maps initially corresponding to a new engine

  • The present paper proposes and proves a new simulation methodology for the Gas Path Analysis (GPA)

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Summary

Introduction

Reliable gas turbine health information is essential for successful the implementation of condition-based maintenance [1] Gas-path diagnostic techniques provide such information by analyzing engine performance and early identifying potential faults before they develop into serious accidents [2]. In the case of GPA, an inverse problem consists in evaluating the conditions of engine components through estimating health parameters using measured operating conditions and monitored variables [9]. It is proposed to consolidate the advantages of these models by creating a new nonlinear data-driven model that computes health parameters using measured operating conditions and monitored variables as inputs. The proposed inverse nonlinear data-driven model and the corresponding mode to diagnose gas turbines present a hybrid approach because the original GPA is based on a data-driven model. The necessary data to build and test the models were generated by the software GasTurb that offers a nonlinear thermodynamic simulation of main gas turbine types The use of this wellknown and commercially available software in the present study allows every researcher to repeat the investigation and verify its results. For such a verification the paper provides all necessary details of the calculations performed

Thermodynamic Model
Multilayer
Polynomials
Input Data
Perceptron Configuration
One Regime Diagnostic Model
Original
Extended Diagnostic Model
Extended MLP-Based Turbo Fan Diagnostic Model
Comparison between MLP- and Polynomials-Based Models
Findings
Conclusions
Full Text
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