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    A Method of Map Extrapolation for Unequal and Partial Admission in a Double Entry Turbine

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 006::page 61019
    Author:
    Newton, Peter
    ,
    Romagnoli, Alessandro
    ,
    Martinez
    ,
    Copeland, Colin
    ,
    Seiler, Martin
    DOI: 10.1115/1.4025763
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a method for prediction of the unequal admission performance of a double entry turbine based on the full admission turbine maps and a minimal number of unequal admission points. The double entry turbine has two separate inlet ports which feed a single turbine wheel: this arrangement can be beneficial in a turbocharger application; however the additional entry does add complexity in producing a complete turbine map which includes unequal admission behavior. When a double entry turbine is operated under full admission conditions, with both entries feeding the turbine equally, this will act effectively as a single entry device and the turbine performance can be represented by a standard turbine map. In reality a multiple entry turbine will spend the majority of time operating under varying degrees of unequal admission, with each entry feeding the turbine different amounts; the extent of this inequality can have a considerable impact on turbine performance. In order to produce a full map which extends from full admission through to the partial admission case (where one inlet has no flow) a large number of unequal admission data points are required. The paper starts by discussing previous attempts to describe the partial and unequal admission performance of a double entry turbine. The full unequal admission performance is then presented for a nozzled, double entry turbine. The impact of unequal admission on turbine performance is demonstrated. Under some conditions of operation, the turbine efficiency may be less than half that of the equivalent full admission case based on the average turbine velocity ratio. A method of using the steady, equal admission maps, with a limited number of unequal admission data points, to predict the full unequal admission behavior is presented. A good agreement is found when the map extension method is validated against the full unequal admission turbine performance measured on a test stand. In the prediction of efficiency a mean error of approximately 0.39% is found between the test stand data and the proposed extrapolation method, with a standard deviation of 2.79%. A better agreement is generally found at conditions of higher power.
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      A Method of Map Extrapolation for Unequal and Partial Admission in a Double Entry Turbine

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    contributor authorNewton, Peter
    contributor authorRomagnoli, Alessandro
    contributor authorMartinez
    contributor authorCopeland, Colin
    contributor authorSeiler, Martin
    date accessioned2017-05-09T01:13:40Z
    date available2017-05-09T01:13:40Z
    date issued2014
    identifier issn0889-504X
    identifier otherturbo_136_06_061019.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156622
    description abstractThis paper presents a method for prediction of the unequal admission performance of a double entry turbine based on the full admission turbine maps and a minimal number of unequal admission points. The double entry turbine has two separate inlet ports which feed a single turbine wheel: this arrangement can be beneficial in a turbocharger application; however the additional entry does add complexity in producing a complete turbine map which includes unequal admission behavior. When a double entry turbine is operated under full admission conditions, with both entries feeding the turbine equally, this will act effectively as a single entry device and the turbine performance can be represented by a standard turbine map. In reality a multiple entry turbine will spend the majority of time operating under varying degrees of unequal admission, with each entry feeding the turbine different amounts; the extent of this inequality can have a considerable impact on turbine performance. In order to produce a full map which extends from full admission through to the partial admission case (where one inlet has no flow) a large number of unequal admission data points are required. The paper starts by discussing previous attempts to describe the partial and unequal admission performance of a double entry turbine. The full unequal admission performance is then presented for a nozzled, double entry turbine. The impact of unequal admission on turbine performance is demonstrated. Under some conditions of operation, the turbine efficiency may be less than half that of the equivalent full admission case based on the average turbine velocity ratio. A method of using the steady, equal admission maps, with a limited number of unequal admission data points, to predict the full unequal admission behavior is presented. A good agreement is found when the map extension method is validated against the full unequal admission turbine performance measured on a test stand. In the prediction of efficiency a mean error of approximately 0.39% is found between the test stand data and the proposed extrapolation method, with a standard deviation of 2.79%. A better agreement is generally found at conditions of higher power.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Method of Map Extrapolation for Unequal and Partial Admission in a Double Entry Turbine
    typeJournal Paper
    journal volume136
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025763
    journal fristpage61019
    journal lastpage61019
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 006
    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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