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    Application of a Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001::page 25
    Author:
    H. Hayami
    ,
    Y. Senoo
    ,
    K. Utsunomiya
    DOI: 10.1115/1.2927416
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Low-solidity circular cascades, conformally transformed from high-stagger linear cascades of double-circular-arc vanes with solidity 0.69, were used as a part of the diffuser system of a transonic centrifugal compressor. Performance test results were compared with data of the same compressor with a vaneless diffuser. Good compressor performance and a wider flow range as well as a higher pressure ratio and a higher efficiency, superior to those with a vaneless diffuser, where the flow range was limited by choke of the impeller, were demonstrated. The test circular cascade diffusers demonstrated a good pressure recovery over a wide range of flow angles, even when the inflow Mach number to the cascade was over unity.
    keyword(s): Compressors , Cascades (Fluid dynamics) , Diffusers , Flow (Dynamics) , Vaneless diffusers , Pressure , Inflow , Testing performance , Mach number AND Impellers ,
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      Application of a Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/107780
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    • Journal of Turbomachinery

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    contributor authorH. Hayami
    contributor authorY. Senoo
    contributor authorK. Utsunomiya
    date accessioned2017-05-08T23:34:09Z
    date available2017-05-08T23:34:09Z
    date copyrightJanuary, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28600#25_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107780
    description abstractLow-solidity circular cascades, conformally transformed from high-stagger linear cascades of double-circular-arc vanes with solidity 0.69, were used as a part of the diffuser system of a transonic centrifugal compressor. Performance test results were compared with data of the same compressor with a vaneless diffuser. Good compressor performance and a wider flow range as well as a higher pressure ratio and a higher efficiency, superior to those with a vaneless diffuser, where the flow range was limited by choke of the impeller, were demonstrated. The test circular cascade diffusers demonstrated a good pressure recovery over a wide range of flow angles, even when the inflow Mach number to the cascade was over unity.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleApplication of a Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor
    typeJournal Paper
    journal volume112
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927416
    journal fristpage25
    journal lastpage29
    identifier eissn1528-8900
    keywordsCompressors
    keywordsCascades (Fluid dynamics)
    keywordsDiffusers
    keywordsFlow (Dynamics)
    keywordsVaneless diffusers
    keywordsPressure
    keywordsInflow
    keywordsTesting performance
    keywordsMach number AND Impellers
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 001
    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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