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    Effects of Geometry on Brush Seal Pressure and Flow Fields—Part II: Backing Plate Configurations

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 002::page 379
    Author:
    Yahya Dogu
    ,
    Mahmut F. Aksit
    DOI: 10.1115/1.2101858
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Brush seal dynamic behavior is strongly related to pressure and flow fields. Developments in brush seal design have led to geometric modifications to control flow field and consequent brush seal issues including blow-down, hang-up, and pressure stiffening. Some of the geometric enhancements have been found to have common use as backing plate modifications. Over the two decades of brush seal evolution, many backing plate configurations have been suggested in numerous patent disclosures. Even so, literature on the effects of geometric modifications on pressure and flow fields remains limited. This study numerically investigates brush seal pressure and flow fields for such common conceptual backing plate configurations as single and multiple grooves, with and without by-pass passages. The CFD analysis presented employs a bulk porous medium approach for the bristle pack. The effectiveness of various backing plate configurations outlining important flow features is discussed. Results indicate that backing plate configurations have a decisive role in shaping seal pressure fields. In general, it has been found that all cases having bypass configuration leak more. Moreover, the major portion of the seal leakage through fence height is fed from the backing plate cavity. The single backing plate groove forms a constant pressure behind the bristle pack. In contrast, multiple grooves form multiple constant pressure regions.
    keyword(s): Pressure , Flow (Dynamics) , Clearances (Engineering) , Cavities , Geometry AND Leakage ,
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      Effects of Geometry on Brush Seal Pressure and Flow Fields—Part II: Backing Plate Configurations

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    https://yetl.yabesh.ir/yetl1/handle/yetl/134856
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    contributor authorYahya Dogu
    contributor authorMahmut F. Aksit
    date accessioned2017-05-09T00:21:59Z
    date available2017-05-09T00:21:59Z
    date copyrightApril, 2006
    date issued2006
    identifier issn0889-504X
    identifier otherJOTUEI-28728#379_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134856
    description abstractBrush seal dynamic behavior is strongly related to pressure and flow fields. Developments in brush seal design have led to geometric modifications to control flow field and consequent brush seal issues including blow-down, hang-up, and pressure stiffening. Some of the geometric enhancements have been found to have common use as backing plate modifications. Over the two decades of brush seal evolution, many backing plate configurations have been suggested in numerous patent disclosures. Even so, literature on the effects of geometric modifications on pressure and flow fields remains limited. This study numerically investigates brush seal pressure and flow fields for such common conceptual backing plate configurations as single and multiple grooves, with and without by-pass passages. The CFD analysis presented employs a bulk porous medium approach for the bristle pack. The effectiveness of various backing plate configurations outlining important flow features is discussed. Results indicate that backing plate configurations have a decisive role in shaping seal pressure fields. In general, it has been found that all cases having bypass configuration leak more. Moreover, the major portion of the seal leakage through fence height is fed from the backing plate cavity. The single backing plate groove forms a constant pressure behind the bristle pack. In contrast, multiple grooves form multiple constant pressure regions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Geometry on Brush Seal Pressure and Flow Fields—Part II: Backing Plate Configurations
    typeJournal Paper
    journal volume128
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2101858
    journal fristpage379
    journal lastpage389
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsClearances (Engineering)
    keywordsCavities
    keywordsGeometry AND Leakage
    treeJournal of Turbomachinery:;2006:;volume( 128 ):;issue: 002
    contenttypeFulltext
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