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    A Global Simulation Model for Hermetic Reciprocating Compressors

    Source: Journal of Vibration and Acoustics:;1991:;volume( 113 ):;issue: 003::page 395
    Author:
    M. A. de los Santos
    ,
    S. Cardona
    ,
    J. Sánchez-Reyes
    DOI: 10.1115/1.2930197
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article presents a simulation model for reciprocating hermetic compressors. The acoustical behavior of both admission and discharge circuits is analyzed by invoking the discrete element model. Cavities are considered as elastic elements and ducts as rigid elements with inertia according to this model. Reed valves are modeled as systems of three degrees of freedom, and are studied by using modal analysis. The percussive version of Lagrange equations is used to describe the impact between valves and stops or seats. Results from the theoretical model are checked with those experimentally obtained for a real compressor.
    keyword(s): Compressors , Simulation models , Valves , Cavities , Circuits , Ducts , Equations , Degrees of freedom , Inertia (Mechanics) AND Acoustics ,
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      A Global Simulation Model for Hermetic Reciprocating Compressors

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/109498
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    • Journal of Vibration and Acoustics

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    contributor authorM. A. de los Santos
    contributor authorS. Cardona
    contributor authorJ. Sánchez-Reyes
    date accessioned2017-05-08T23:37:10Z
    date available2017-05-08T23:37:10Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn1048-9002
    identifier otherJVACEK-28798#395_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109498
    description abstractThis article presents a simulation model for reciprocating hermetic compressors. The acoustical behavior of both admission and discharge circuits is analyzed by invoking the discrete element model. Cavities are considered as elastic elements and ducts as rigid elements with inertia according to this model. Reed valves are modeled as systems of three degrees of freedom, and are studied by using modal analysis. The percussive version of Lagrange equations is used to describe the impact between valves and stops or seats. Results from the theoretical model are checked with those experimentally obtained for a real compressor.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Global Simulation Model for Hermetic Reciprocating Compressors
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.2930197
    journal fristpage395
    journal lastpage400
    identifier eissn1528-8927
    keywordsCompressors
    keywordsSimulation models
    keywordsValves
    keywordsCavities
    keywordsCircuits
    keywordsDucts
    keywordsEquations
    keywordsDegrees of freedom
    keywordsInertia (Mechanics) AND Acoustics
    treeJournal of Vibration and Acoustics:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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