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    An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 005::page 51007-1
    Author:
    Jiang, Boyan
    ,
    Yang, Xiaopei
    ,
    Wang, Jun
    ,
    Lin, Zhiliang
    ,
    Hu, Jinkang
    DOI: 10.1115/1.4064309
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An improved passage-flow turning model (IPTM) was developed in this study to design high-performance forward-curved blades for squirrel-cage fans. The flow separation in blade passages and the corresponding fan performance were compared between IPTM and traditional methods through computational fluid dynamics (CFD). The results show that correcting the blade inlet angle, based on the zero-incidence design, is crucial to prevent separation of the passage mainstream from the blade pressure surface. The blade shape with second-order smoothness also exhibits the thinnest separation and highest efficiency when other design parameters remain constant. Considering these findings, the blades designed by IPTM outperform traditional blades with the same inlet and outlet angles. The optimal values of the turning radius R¯T and the decelerating factor of the leading half blade ɛ were determined based on the CFD results. The designed blade achieves high pressure when these two parameters satisfy R¯T=−0.185ε+0.29175, while achieving high efficiency when they satisfy R¯T=−0.31ε+0.4425. To confirm the advantages of IPTM, an optimal IPTM-based blade was manufactured and measured. The results indicated that the maximum increase in fan pressure and efficiency reaches 10% and 6%, respectively.
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      An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan

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    contributor authorJiang, Boyan
    contributor authorYang, Xiaopei
    contributor authorWang, Jun
    contributor authorLin, Zhiliang
    contributor authorHu, Jinkang
    date accessioned2024-04-24T22:50:33Z
    date available2024-04-24T22:50:33Z
    date copyright1/16/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_146_5_051007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295971
    description abstractAn improved passage-flow turning model (IPTM) was developed in this study to design high-performance forward-curved blades for squirrel-cage fans. The flow separation in blade passages and the corresponding fan performance were compared between IPTM and traditional methods through computational fluid dynamics (CFD). The results show that correcting the blade inlet angle, based on the zero-incidence design, is crucial to prevent separation of the passage mainstream from the blade pressure surface. The blade shape with second-order smoothness also exhibits the thinnest separation and highest efficiency when other design parameters remain constant. Considering these findings, the blades designed by IPTM outperform traditional blades with the same inlet and outlet angles. The optimal values of the turning radius R¯T and the decelerating factor of the leading half blade ɛ were determined based on the CFD results. The designed blade achieves high pressure when these two parameters satisfy R¯T=−0.185ε+0.29175, while achieving high efficiency when they satisfy R¯T=−0.31ε+0.4425. To confirm the advantages of IPTM, an optimal IPTM-based blade was manufactured and measured. The results indicated that the maximum increase in fan pressure and efficiency reaches 10% and 6%, respectively.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan
    typeJournal Paper
    journal volume146
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4064309
    journal fristpage51007-1
    journal lastpage51007-16
    page16
    treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 005
    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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