Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
10282100 | Applied Energy | 2005 | 9 Pages |
Abstract
The aim of this investigation is to describe a way of setting up a fuzzy-logic process to achieve diagnoses, based on gas-path measurements, for modern military turbofan engines. Each engine's gas-path components' faults are quantified, taking into account measurement noise, through a non-linear analysis. A simplified version of this theoretical tool is explained by focusing on one engine-component and assuming that only a single fault occurs at a given time. Eventually the concept is generalised to cater for multiple-component fault diagnoses.
Keywords
Related Topics
Physical Sciences and Engineering
Energy
Energy Engineering and Power Technology
Authors
S.O.T. Ogaji, L. Marinai, S. Sampath, R. Singh, S.D. Prober,