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    Optimization of a Centrifugal Compressor Impeller for Robustness to Manufacturing Uncertainties

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 011::page 112101
    Author:
    Javed, A.
    ,
    Pecnik, R.
    ,
    van Buijtenen, J. P.
    DOI: 10.1115/1.4033185
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressor impellers for massmarket turbochargers are diecasted and machined with an aim to achieve high dimensional accuracy and acquire specific performance. However, manufacturing uncertainties result in dimensional deviations causing incompatible operational performance and assembly errors. Process capability limitations of the manufacturer can cause an increase in part rejections, resulting in high production cost. This paper presents a study on a centrifugal impeller with focus on the conceptual design phase to obtain a turbomachine that is robust to manufacturing uncertainties. The impeller has been parameterized and evaluated using a commercial computational fluid dynamics (CFDs) solver. Considering the computational cost of CFD, a surrogate model has been prepared for the impeller by response surface methodology (RSM) using spacefilling Latin hypercube designs. A sensitivity analysis has been performed initially to identify the critical geometric parameters which influence the performance mainly. Sensitivity analysis is followed by the uncertainty propagation and quantification using the surrogate model based Monte Carlo simulation. Finally, a robust design optimization has been carried out using a stochastic optimization algorithm leading to a robust impeller design for which the performance is relatively insensitive to variability in geometry without reducing the sources of inherent variation, i.e., the manufacturing noise.
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      Optimization of a Centrifugal Compressor Impeller for Robustness to Manufacturing Uncertainties

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/161193
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJaved, A.
    contributor authorPecnik, R.
    contributor authorvan Buijtenen, J. P.
    date accessioned2017-05-09T01:28:51Z
    date available2017-05-09T01:28:51Z
    date issued2016
    identifier issn1528-8919
    identifier otherturbo_138_10_101004.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161193
    description abstractCompressor impellers for massmarket turbochargers are diecasted and machined with an aim to achieve high dimensional accuracy and acquire specific performance. However, manufacturing uncertainties result in dimensional deviations causing incompatible operational performance and assembly errors. Process capability limitations of the manufacturer can cause an increase in part rejections, resulting in high production cost. This paper presents a study on a centrifugal impeller with focus on the conceptual design phase to obtain a turbomachine that is robust to manufacturing uncertainties. The impeller has been parameterized and evaluated using a commercial computational fluid dynamics (CFDs) solver. Considering the computational cost of CFD, a surrogate model has been prepared for the impeller by response surface methodology (RSM) using spacefilling Latin hypercube designs. A sensitivity analysis has been performed initially to identify the critical geometric parameters which influence the performance mainly. Sensitivity analysis is followed by the uncertainty propagation and quantification using the surrogate model based Monte Carlo simulation. Finally, a robust design optimization has been carried out using a stochastic optimization algorithm leading to a robust impeller design for which the performance is relatively insensitive to variability in geometry without reducing the sources of inherent variation, i.e., the manufacturing noise.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimization of a Centrifugal Compressor Impeller for Robustness to Manufacturing Uncertainties
    typeJournal Paper
    journal volume138
    journal issue11
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4033185
    journal fristpage112101
    journal lastpage112101
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 011
    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
    yabeshDSpacePersian