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    The Impact of Sliding Blades in a Rotary Compressor

    Source: Journal of Mechanical Design:;2001:;volume( 123 ):;issue: 004::page 583
    Author:
    Yuan Mao Huang
    ,
    Yung-Shane Liaw
    ,
    Research Assistant
    DOI: 10.1115/1.1416150
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this study was to analyze the impact of blades with slots in a rotary compressor. The equations for contact forces were derived from Newton’s law. Updated moving Lagrangian descriptions with the hybrid technique and the Newark time integration method were used to determine the nodal displacement vectors. The finite element method was used to analyze the contact forces and the stresses of blades. The maximum blade contact force of 2.3 KN was larger than the maximum static force of 1 KN. The maximum blade impact Von Mises stress of 12.3 Mpa that occurred at the contact point was greater than the previous calculated static stress of 5.15 Mpa. Hence, the impact effect was significant. Experimental modal analysis was also used to determine the first and second natural frequencies of blades.
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      The Impact of Sliding Blades in a Rotary Compressor

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    https://yetl.yabesh.ir/yetl1/handle/yetl/125592
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    contributor authorYuan Mao Huang
    contributor authorYung-Shane Liaw
    contributor authorResearch Assistant
    date accessioned2017-05-09T00:05:29Z
    date available2017-05-09T00:05:29Z
    date copyrightDecember, 2001
    date issued2001
    identifier issn1050-0472
    identifier otherJMDEDB-27707#583_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125592
    description abstractThe purpose of this study was to analyze the impact of blades with slots in a rotary compressor. The equations for contact forces were derived from Newton’s law. Updated moving Lagrangian descriptions with the hybrid technique and the Newark time integration method were used to determine the nodal displacement vectors. The finite element method was used to analyze the contact forces and the stresses of blades. The maximum blade contact force of 2.3 KN was larger than the maximum static force of 1 KN. The maximum blade impact Von Mises stress of 12.3 Mpa that occurred at the contact point was greater than the previous calculated static stress of 5.15 Mpa. Hence, the impact effect was significant. Experimental modal analysis was also used to determine the first and second natural frequencies of blades.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Impact of Sliding Blades in a Rotary Compressor
    typeJournal Paper
    journal volume123
    journal issue4
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.1416150
    journal fristpage583
    journal lastpage589
    identifier eissn1528-9001
    treeJournal of Mechanical Design:;2001:;volume( 123 ):;issue: 004
    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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