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    The Impact of Hole Depth on the Rotordynamic and Leakage Characteristics of Hole Pattern Stator Gas Annular Seals

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 004::page 42501
    Author:
    Childs, Dara W.
    ,
    Arthur, Stephen
    ,
    Mehta, Naitik J.
    DOI: 10.1115/1.4025888
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Test results are presented for rotordynamic characteristics of holepatternstator annular gas seals at a 70 bar supply pressures with a running speed of 20,200 rpm. Leakage results are presented for these conditions and the additional speeds: 10,200 and 15,300 rpm. Holedepth is the principal test variable of interest. Most published annular test data for these seals have a hole diameter of 3.175 mm and a hole depth of 3.302 mm. For this work, with the 3.175 mm hole diameter, additional results are presented for shallow (1.905 mm) and deep (6.604 mm) hole depths. Test results show a pronounced dependence of leakage and rotordynamic behavior on hole depth. Test results show much better leakage performance for the shallowholedepth seal in both leakage and rotordynamic performance. Compressor manufacturers and users will need to decide whether this observed performance improvement is worth trying in real machines.
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      The Impact of Hole Depth on the Rotordynamic and Leakage Characteristics of Hole Pattern Stator Gas Annular Seals

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/154684
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorChilds, Dara W.
    contributor authorArthur, Stephen
    contributor authorMehta, Naitik J.
    date accessioned2017-05-09T01:07:32Z
    date available2017-05-09T01:07:32Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_04_042501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154684
    description abstractTest results are presented for rotordynamic characteristics of holepatternstator annular gas seals at a 70 bar supply pressures with a running speed of 20,200 rpm. Leakage results are presented for these conditions and the additional speeds: 10,200 and 15,300 rpm. Holedepth is the principal test variable of interest. Most published annular test data for these seals have a hole diameter of 3.175 mm and a hole depth of 3.302 mm. For this work, with the 3.175 mm hole diameter, additional results are presented for shallow (1.905 mm) and deep (6.604 mm) hole depths. Test results show a pronounced dependence of leakage and rotordynamic behavior on hole depth. Test results show much better leakage performance for the shallowholedepth seal in both leakage and rotordynamic performance. Compressor manufacturers and users will need to decide whether this observed performance improvement is worth trying in real machines.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Impact of Hole Depth on the Rotordynamic and Leakage Characteristics of Hole Pattern Stator Gas Annular Seals
    typeJournal Paper
    journal volume136
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4025888
    journal fristpage42501
    journal lastpage42501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;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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