Fuzzy Logic Estimation Applied to Newton Methods for Gas TurbinesSource: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001::page 88Author:Dan Martis
DOI: 10.1115/1.2360597Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This method, based on fuzzy logic principles, is intended to find the most likely solution of an over-determined system, in specific conditions. The method addresses typical problems encountered in gas turbine performance analysis and, more specifically, to the alignment of a synthesis model with measured data. Generally speaking, the relatively low accuracy of measurements introduces a random noise around the true value of a performance parameter and distorts any deterministic solution of a square matrix-based linear system. The fuzzy logic estimator is able to get very close to the real solution by using additional (pseudo-redundant) parameters and by building the most likely solution based on each of the measurement accuracies. The accuracy—or “quality”—of a measurement is encapsulated within an extra dimension which is defined as fuzzy and which encompasses the whole range of values, between 0 (false) and 1 (true). The value of the method is shown in two examples. The first simulates compressor fouling, the other deals with actual engine test data following a hardware modification. Both examples experience noisy measurements. The method is stable and effective even at high level of noise. The results are within the close vicinity of the expected levels (within 0.2% accuracy) and the accuracy is about ten times lower than the noise level.
keyword(s): Fuzzy logic , Noise (Sound) , Gas turbines , Engines , Compressors , Equations , Measurement AND Gaussian distribution ,
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contributor author | Dan Martis | |
date accessioned | 2017-05-09T00:23:48Z | |
date available | 2017-05-09T00:23:48Z | |
date copyright | January, 2007 | |
date issued | 2007 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26935#88_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135774 | |
description abstract | This method, based on fuzzy logic principles, is intended to find the most likely solution of an over-determined system, in specific conditions. The method addresses typical problems encountered in gas turbine performance analysis and, more specifically, to the alignment of a synthesis model with measured data. Generally speaking, the relatively low accuracy of measurements introduces a random noise around the true value of a performance parameter and distorts any deterministic solution of a square matrix-based linear system. The fuzzy logic estimator is able to get very close to the real solution by using additional (pseudo-redundant) parameters and by building the most likely solution based on each of the measurement accuracies. The accuracy—or “quality”—of a measurement is encapsulated within an extra dimension which is defined as fuzzy and which encompasses the whole range of values, between 0 (false) and 1 (true). The value of the method is shown in two examples. The first simulates compressor fouling, the other deals with actual engine test data following a hardware modification. Both examples experience noisy measurements. The method is stable and effective even at high level of noise. The results are within the close vicinity of the expected levels (within 0.2% accuracy) and the accuracy is about ten times lower than the noise level. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Fuzzy Logic Estimation Applied to Newton Methods for Gas Turbines | |
type | Journal Paper | |
journal volume | 129 | |
journal issue | 1 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2360597 | |
journal fristpage | 88 | |
journal lastpage | 96 | |
identifier eissn | 0742-4795 | |
keywords | Fuzzy logic | |
keywords | Noise (Sound) | |
keywords | Gas turbines | |
keywords | Engines | |
keywords | Compressors | |
keywords | Equations | |
keywords | Measurement AND Gaussian distribution | |
tree | Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001 | |
contenttype | Fulltext |