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    Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 008::page 81012-1
    Author:
    Zhang, Hanzhi
    ,
    Yang, Ce
    ,
    Wang, Wenli
    ,
    Yang, Changmao
    ,
    Li, Yanzhao
    DOI: 10.1115/1.4053838
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Stall and surge behaviors deteriorate the compressor performance and stability of the operating range. To avoid the effect of stall and surge behaviors, the characteristics of the pre-stall disturbance have been considered in recent years. However, investigations of the pre-stall and stall disturbances in centrifugal compressors remain insufficient owing to the various geometric structures in centrifugal compressors. In this study, a centrifugal compressor with a volute and vaneless diffuser was studied using high-response static pressure measurements and numerical simulations. The pressure disturbance evolution from near-choke to near-surge conditions was obtained, and the characteristics of the pre-stall and stall disturbances were analyzed. The results showed that the compressor instability route could be divided into pre-stall and stall stages, which could be accurately predicted based on the periodic static pressure irregularity and skewness. The pre-stall stage was dominated by the rotating instability (RI) phenomenon, and the frequency of the RI was 43% of the blade passing frequency at 70% Nmax. The experimental results demonstrated that the first onset of RI occurred at the 120 deg–180 deg circumferential position and maintained a local pattern
     
    then, RI occurred over the whole annulus when the flowrate was decreased. RI was induced by the vortex structure attached to the casing wall, leading to a sharp pressure trough in the static pressure trace. The RI exhibited an evolution pattern of initially increasing and then fading, which can be explained by the enlargement and movement of the impeller inlet vortex. The large blockage effect of RI triggered a stall with disturbances at 20% and 80% of the impeller shaft frequency, and these disturbance frequencies had a trend of shifting to one dominant frequency of 22% the impeller shaft frequency. Furthermore, stall cell merging and the coexistence of RI/stall phenomena occurred during the stall stage.
     
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      Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4284559
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    contributor authorZhang, Hanzhi
    contributor authorYang, Ce
    contributor authorWang, Wenli
    contributor authorYang, Changmao
    contributor authorLi, Yanzhao
    date accessioned2022-05-08T08:57:49Z
    date available2022-05-08T08:57:49Z
    date copyright3/4/2022 12:00:00 AM
    date issued2022
    identifier issn0889-504X
    identifier otherturbo_144_8_081012.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284559
    description abstractStall and surge behaviors deteriorate the compressor performance and stability of the operating range. To avoid the effect of stall and surge behaviors, the characteristics of the pre-stall disturbance have been considered in recent years. However, investigations of the pre-stall and stall disturbances in centrifugal compressors remain insufficient owing to the various geometric structures in centrifugal compressors. In this study, a centrifugal compressor with a volute and vaneless diffuser was studied using high-response static pressure measurements and numerical simulations. The pressure disturbance evolution from near-choke to near-surge conditions was obtained, and the characteristics of the pre-stall and stall disturbances were analyzed. The results showed that the compressor instability route could be divided into pre-stall and stall stages, which could be accurately predicted based on the periodic static pressure irregularity and skewness. The pre-stall stage was dominated by the rotating instability (RI) phenomenon, and the frequency of the RI was 43% of the blade passing frequency at 70% Nmax. The experimental results demonstrated that the first onset of RI occurred at the 120 deg–180 deg circumferential position and maintained a local pattern
    description abstractthen, RI occurred over the whole annulus when the flowrate was decreased. RI was induced by the vortex structure attached to the casing wall, leading to a sharp pressure trough in the static pressure trace. The RI exhibited an evolution pattern of initially increasing and then fading, which can be explained by the enlargement and movement of the impeller inlet vortex. The large blockage effect of RI triggered a stall with disturbances at 20% and 80% of the impeller shaft frequency, and these disturbance frequencies had a trend of shifting to one dominant frequency of 22% the impeller shaft frequency. Furthermore, stall cell merging and the coexistence of RI/stall phenomena occurred during the stall stage.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute
    typeJournal Paper
    journal volume144
    journal issue8
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4053838
    journal fristpage81012-1
    journal lastpage81012-13
    page13
    treeJournal of Turbomachinery:;2022:;volume( 144 ):;issue: 008
    contenttypeFulltext
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