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    Design Control of Overcompression in Rotary-Vane Compressors

    Source: Journal of Engineering for Gas Turbines and Power:;1960:;volume( 082 ):;issue: 003::page 221
    Author:
    E. O. Bransford
    ,
    R. A. Stein
    DOI: 10.1115/1.3672771
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In its simplest terms, the design of a rotary-vane compressor of a given displacement consists of selecting a particular combination of rotor and cylinder radius, cylinder length, and number of vanes. A study of the rotary-vane compressor has shown that the choice is not entirely arbitrary since thermodynamic and mechanical losses occurring in the compressor are intimately associated with these basic dimensions. One of the more important of these geometrically dependent losses was found to be potentially severe overcompression during the discharge process. In this paper, an equation is developed that describes in generalized form the relation of overcompression to the dimensions of the compressor. This equation is used to evolve an energy-loss criterion for design control of this loss. An example of the application of the criterion to a refrigeration compressor is included.
    keyword(s): Compressors , Design , Cylinders , Dimensions , Equations , Displacement , Refrigeration , Rotors AND Energy dissipation ,
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      Design Control of Overcompression in Rotary-Vane Compressors

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    https://yetl.yabesh.ir/yetl1/handle/yetl/100501
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorE. O. Bransford
    contributor authorR. A. Stein
    date accessioned2017-05-08T23:21:22Z
    date available2017-05-08T23:21:22Z
    date copyrightJuly, 1960
    date issued1960
    identifier issn1528-8919
    identifier otherJETPEZ-26609#221_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100501
    description abstractIn its simplest terms, the design of a rotary-vane compressor of a given displacement consists of selecting a particular combination of rotor and cylinder radius, cylinder length, and number of vanes. A study of the rotary-vane compressor has shown that the choice is not entirely arbitrary since thermodynamic and mechanical losses occurring in the compressor are intimately associated with these basic dimensions. One of the more important of these geometrically dependent losses was found to be potentially severe overcompression during the discharge process. In this paper, an equation is developed that describes in generalized form the relation of overcompression to the dimensions of the compressor. This equation is used to evolve an energy-loss criterion for design control of this loss. An example of the application of the criterion to a refrigeration compressor is included.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign Control of Overcompression in Rotary-Vane Compressors
    typeJournal Paper
    journal volume82
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3672771
    journal fristpage221
    journal lastpage226
    identifier eissn0742-4795
    keywordsCompressors
    keywordsDesign
    keywordsCylinders
    keywordsDimensions
    keywordsEquations
    keywordsDisplacement
    keywordsRefrigeration
    keywordsRotors AND Energy dissipation
    treeJournal of Engineering for Gas Turbines and Power:;1960:;volume( 082 ):;issue: 003
    contenttypeFulltext
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