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    A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003::page 31014-1
    Author:
    Tamaki, Hideaki
    ,
    Yamaguchi, Satoshi
    DOI: 10.1115/1.4064083
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Centrifugal compressors require a wide operating range as well as high efficiency. Typical active control forms to enhance the operating range are suction throttling with a valve in a suction line, discharge throttling with a ring installed in a vaneless diffuser, variable inlet guide vanes, and variable geometry vaned diffuser (VVD). This study focuses on the design of a VVD whose vane rotates around a pivot to adjust its opening and proposes a method to estimate the main parameters of the VVD at the preliminary design stage. The design method here is based on matching the diffuser vane inlet angles with the flow angles at the diffuser inlet. If the designed VVD can maintain low incidence at the diffuser vane leading edge over the whole movable range of the vane is evaluated. A graph, which indicates the relation between the diffuser vane inlet angles and the flow angles at the diffuser inlet at diffuser choking and diffuser stalling, makes the evaluation easy. The proposed procedures were applied to select the number of vanes of the VVD for a turbocharger compressor. Tests for the validation of the design procedures were conducted by using fixed vaned diffusers that simulated the VVDs installed on the turbocharger with an 85 mm-diameter impeller. The results showed the effectiveness of the proposed design procedures. This paper first presents examples of applications of the typical active methods extending centrifugal compressors’ operating range for real machines and then discusses the design of VVD.
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      A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4295956
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    contributor authorTamaki, Hideaki
    contributor authorYamaguchi, Satoshi
    date accessioned2024-04-24T22:50:09Z
    date available2024-04-24T22:50:09Z
    date copyright12/14/2023 12:00:00 AM
    date issued2023
    identifier issn0889-504X
    identifier otherturbo_146_3_031014.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295956
    description abstractCentrifugal compressors require a wide operating range as well as high efficiency. Typical active control forms to enhance the operating range are suction throttling with a valve in a suction line, discharge throttling with a ring installed in a vaneless diffuser, variable inlet guide vanes, and variable geometry vaned diffuser (VVD). This study focuses on the design of a VVD whose vane rotates around a pivot to adjust its opening and proposes a method to estimate the main parameters of the VVD at the preliminary design stage. The design method here is based on matching the diffuser vane inlet angles with the flow angles at the diffuser inlet. If the designed VVD can maintain low incidence at the diffuser vane leading edge over the whole movable range of the vane is evaluated. A graph, which indicates the relation between the diffuser vane inlet angles and the flow angles at the diffuser inlet at diffuser choking and diffuser stalling, makes the evaluation easy. The proposed procedures were applied to select the number of vanes of the VVD for a turbocharger compressor. Tests for the validation of the design procedures were conducted by using fixed vaned diffusers that simulated the VVDs installed on the turbocharger with an 85 mm-diameter impeller. The results showed the effectiveness of the proposed design procedures. This paper first presents examples of applications of the typical active methods extending centrifugal compressors’ operating range for real machines and then discusses the design of VVD.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor
    typeJournal Paper
    journal volume146
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4064083
    journal fristpage31014-1
    journal lastpage31014-13
    page13
    treeJournal of Turbomachinery:;2023:;volume( 146 ):;issue: 003
    contenttypeFulltext
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    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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