Method of formulating input parameters of neural network for diagnosing gas-turbine engines

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Date

2013-05

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Volume Title

Publisher

Aviation. Taylor&Francis

Abstract

A method of obtaining test and training data sets has been developed. 弻ese sets are intended for train- ing a static neural network to recognise individual and double defects in the air-gas path units of a gas-turbine engine. 弻ese data are obtained by using operational process parameters of the air-gas path of a bypass turbofan engine. 弻e method allows sets that can project some changes in the technical conditions of a gas-turbine engine to be received, taking into account errors that occur in the measurement of the gas-dynamic parameters of the air-gas path. 弻e op- eration of the engine in a wide range of modes should also be taken into account

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Keywords

gas-turbine engine, air-gas path, mathematical model of operational process, neural network

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