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    Fuzzy Logic Estimation Applied to Newton Methods for Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001::page 88
    Author:
    Dan Martis
    DOI: 10.1115/1.2360597
    Publisher: 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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      Fuzzy Logic Estimation Applied to Newton Methods for Gas Turbines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135774
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    contributor authorDan Martis
    date accessioned2017-05-09T00:23:48Z
    date available2017-05-09T00:23:48Z
    date copyrightJanuary, 2007
    date issued2007
    identifier issn1528-8919
    identifier otherJETPEZ-26935#88_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135774
    description abstractThis 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.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFuzzy Logic Estimation Applied to Newton Methods for Gas Turbines
    typeJournal Paper
    journal volume129
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2360597
    journal fristpage88
    journal lastpage96
    identifier eissn0742-4795
    keywordsFuzzy logic
    keywordsNoise (Sound)
    keywordsGas turbines
    keywordsEngines
    keywordsCompressors
    keywordsEquations
    keywordsMeasurement AND Gaussian distribution
    treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001
    contenttypeFulltext
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