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    On the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002::page 271
    Author:
    M. Ishida
    ,
    Y. Senoo
    DOI: 10.1115/1.3230717
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The pressure distribution along the shroud is measured for three types of centrifugal impeller at seven different values of tip clearance each. The change of input power due to a change of tip clearance is related to the effective blockage at the impeller tip. Since the change of input power is little for the test cases, the variation of local pressure gradient along the shroud is mostly attributed to the change of local pressure loss. The local pressure loss is related to the local tip clearance ratio and to the local pressure gradient based on the deceleration of relative velocity in the impeller. Since the local pressure gradient is largest near the throat of the impeller, for many impellers the clearance ratio at the throat is used as the representative value. The tip clearance loss is related to the clearance ratio and the pressure rise based on the deceleration of relative velocity in the impeller. A good correlation is observed in all cases at various flow rate.
    keyword(s): Pressure , Clearances (Engineering) , Impellers , Pressure gradient AND Flow (Dynamics) ,
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      On the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/94520
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorM. Ishida
    contributor authorY. Senoo
    date accessioned2017-05-08T23:11:05Z
    date available2017-05-08T23:11:05Z
    date copyrightApril, 1981
    date issued1981
    identifier issn1528-8919
    identifier otherJETPEZ-26765#271_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94520
    description abstractThe pressure distribution along the shroud is measured for three types of centrifugal impeller at seven different values of tip clearance each. The change of input power due to a change of tip clearance is related to the effective blockage at the impeller tip. Since the change of input power is little for the test cases, the variation of local pressure gradient along the shroud is mostly attributed to the change of local pressure loss. The local pressure loss is related to the local tip clearance ratio and to the local pressure gradient based on the deceleration of relative velocity in the impeller. Since the local pressure gradient is largest near the throat of the impeller, for many impellers the clearance ratio at the throat is used as the representative value. The tip clearance loss is related to the clearance ratio and the pressure rise based on the deceleration of relative velocity in the impeller. A good correlation is observed in all cases at various flow rate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Pressure Losses Due to the Tip Clearance of Centrifugal Blowers
    typeJournal Paper
    journal volume103
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230717
    journal fristpage271
    journal lastpage278
    identifier eissn0742-4795
    keywordsPressure
    keywordsClearances (Engineering)
    keywordsImpellers
    keywordsPressure gradient AND Flow (Dynamics)
    treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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