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    Phenomenon and Mechanism of Two Regime Surge in a Centrifugal Compressor

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 008::page 81007
    Author:
    Zheng, Xinqian
    ,
    Liu, Anxiong
    DOI: 10.1115/1.4029547
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: “Tworegimesurgeâ€‌ is a special instability behavior of compressors, which was investigated in this paper. When the compressor operates at medium rotor speed, mild surge happens first, where the transient pressure signals show sinusoidal form with Helmholtz frequency of the compressor system. Reducing the mass flow rate, the mild surge vanishes and gets replaced by the local stall. Further reducing the mass flow rate, deep surge breaks out suddenly. During tworegimesurge, two distinct surge patterns exit and vastly narrow stable flow range, which highlights the characteristics of tworegimesurge. It is found that the impeller leadingedge stall is a necessary part of the mild surge, while the diffuser rotating stall incepts the deep surge. At higher speeds, the mild surge oscillation prompts the early occurrence of the diffuser stall so that the mild surge transforms and the deep surge happens in advance. As a result, both regimes of mild surge and deep surge are going to merge, and the stable flow range at high rotational speed is greatly narrowed. Impeller casing treatment is considered as an effective method for flow range extension because the impeller leadingedge stall is removed and the mild surge is avoided as well.
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      Phenomenon and Mechanism of Two Regime Surge in a Centrifugal Compressor

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    contributor authorZheng, Xinqian
    contributor authorLiu, Anxiong
    date accessioned2017-05-09T01:24:41Z
    date available2017-05-09T01:24:41Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_08_081007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159957
    description abstract“Tworegimesurgeâ€‌ is a special instability behavior of compressors, which was investigated in this paper. When the compressor operates at medium rotor speed, mild surge happens first, where the transient pressure signals show sinusoidal form with Helmholtz frequency of the compressor system. Reducing the mass flow rate, the mild surge vanishes and gets replaced by the local stall. Further reducing the mass flow rate, deep surge breaks out suddenly. During tworegimesurge, two distinct surge patterns exit and vastly narrow stable flow range, which highlights the characteristics of tworegimesurge. It is found that the impeller leadingedge stall is a necessary part of the mild surge, while the diffuser rotating stall incepts the deep surge. At higher speeds, the mild surge oscillation prompts the early occurrence of the diffuser stall so that the mild surge transforms and the deep surge happens in advance. As a result, both regimes of mild surge and deep surge are going to merge, and the stable flow range at high rotational speed is greatly narrowed. Impeller casing treatment is considered as an effective method for flow range extension because the impeller leadingedge stall is removed and the mild surge is avoided as well.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePhenomenon and Mechanism of Two Regime Surge in a Centrifugal Compressor
    typeJournal Paper
    journal volume137
    journal issue8
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4029547
    journal fristpage81007
    journal lastpage81007
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 008
    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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