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    Improved Multiple Point Nonlinear Genetic Algorithm Based Performance Adaptation Using Least Square Method

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 003::page 31701
    Author:
    Y.G. Li
    ,
    M. F. Abdul Ghafir
    ,
    K. Huang
    ,
    X. Feng
    ,
    L. Wang
    ,
    R. Singh
    ,
    W. Zhang
    DOI: 10.1115/1.4004395
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: At off-design conditions, engine performance model prediction accuracy depends largely on its component characteristic maps. With the absence of actual characteristic maps, performance adaptation needs to be done for good imitations of actual engine performance. A nonlinear multiple point genetic algorithm based performance adaptation developed earlier by the authors using a set of nonlinear scaling factor functions has been proven capable of making accurate performance predictions over a wide range of operating conditions. However, the success depends on searching the right range of scaling factor coefficients heuristically, in order to obtain the optimum scaling factor functions. Such search ranges may be difficult to obtain and in many off-design adaption cases, it may be very time consuming due to the nature of the trial and error process. In this paper, an improvement on the present adaptation method is presented using a least square method where the search range can be selected deterministically. In the new method, off-design adaptation is applied to individual off-design point first to obtain individual off-design point scaling factors. Then plots of the scaling factors against the off-design conditions are generated. Using the least square method, the relationship between each scaling factor and the off-design operating condition is generated. The regression coefficients are then used to determine the search range of the scaling factor coefficients before multiple off-design points performance adaptation is finally applied. The developed adaptation approach has been applied to a model single-spool turboshaft engine and demonstrated a simpler and faster way of obtaining the optimal scaling factor coefficients compared with the original off-design adaptation method.
    keyword(s): Turbines , Errors , Functions , Genetic algorithms , Engines , Compressors , Measurement AND Design ,
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      Improved Multiple Point Nonlinear Genetic Algorithm Based Performance Adaptation Using Least Square Method

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    http://yetl.yabesh.ir/yetl1/handle/yetl/148893
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorY.G. Li
    contributor authorM. F. Abdul Ghafir
    contributor authorK. Huang
    contributor authorX. Feng
    contributor authorL. Wang
    contributor authorR. Singh
    contributor authorW. Zhang
    date accessioned2017-05-09T00:50:30Z
    date available2017-05-09T00:50:30Z
    date copyrightMarch, 2012
    date issued2012
    identifier issn1528-8919
    identifier otherJETPEZ-27186#031701_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148893
    description abstractAt off-design conditions, engine performance model prediction accuracy depends largely on its component characteristic maps. With the absence of actual characteristic maps, performance adaptation needs to be done for good imitations of actual engine performance. A nonlinear multiple point genetic algorithm based performance adaptation developed earlier by the authors using a set of nonlinear scaling factor functions has been proven capable of making accurate performance predictions over a wide range of operating conditions. However, the success depends on searching the right range of scaling factor coefficients heuristically, in order to obtain the optimum scaling factor functions. Such search ranges may be difficult to obtain and in many off-design adaption cases, it may be very time consuming due to the nature of the trial and error process. In this paper, an improvement on the present adaptation method is presented using a least square method where the search range can be selected deterministically. In the new method, off-design adaptation is applied to individual off-design point first to obtain individual off-design point scaling factors. Then plots of the scaling factors against the off-design conditions are generated. Using the least square method, the relationship between each scaling factor and the off-design operating condition is generated. The regression coefficients are then used to determine the search range of the scaling factor coefficients before multiple off-design points performance adaptation is finally applied. The developed adaptation approach has been applied to a model single-spool turboshaft engine and demonstrated a simpler and faster way of obtaining the optimal scaling factor coefficients compared with the original off-design adaptation method.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImproved Multiple Point Nonlinear Genetic Algorithm Based Performance Adaptation Using Least Square Method
    typeJournal Paper
    journal volume134
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4004395
    journal fristpage31701
    identifier eissn0742-4795
    keywordsTurbines
    keywordsErrors
    keywordsFunctions
    keywordsGenetic algorithms
    keywordsEngines
    keywordsCompressors
    keywordsMeasurement AND Design
    treeJournal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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