Study on Mechanism of Unstable Flow Inception at Small Flow Rates in a Centrifugal Blower
Study on Mechanism of Unstable Flow Inception at Small Flow Rates in a Centrifugal Blower
批准号:
14550154
负责人:
ISHIDA Masahiro
金额:
$2.3万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2002
资助国家:
日本
项目状态:
已结题
起止时间:
2002 至 2003
中文摘要
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英文摘要
In order to clarify the mechanism of the unstable flow inception in a high specific speed type open shrouded centrifugal impeller, and to analyze the effect of the ring groove arrangement on inducer stall and/or that of the diffuser width on diffuser stall, the 3-D turbulent flow simulation and the experimental work were performed. It was found that the steady flow simulation was very helpful for understanding unsteady stall phenomena, and the following concluding remarks were obtained.(1)The incipient unstable flow is caused by the rolling-up vortex flow near the pressure side of the adjacent blade, resulting from the interaction between the tip leakage flow and the accumulated reverse flow zone, in which the strong streamwise vorticity component seems to be included due to the tip leakage vortex.(2)The formation of inlet recirculation is very effective for suppression of the unstable flow due to inducer stall, one factor is the suction of the tip leakage vortex together with the reve … More rse flow, and another one is a decrease in the flow incidence due to an increase in the inlet recirculation flow rate, which increases with a decrease in the through-flow rate.(3)The optimum location of the suction ring groove is in the region near the inducer tip throat, resulting i n suppression of inducer stall (without deterioration of the impeller characteristics even at the design flow rate.(4)The unstable flow due to diffuser stall occurs when the reverse flow zone extends to the diffuser exit.(5)The unstable flow occurring between φ=0.278 and 0.213 was suppressed by reducing the diffuser width from the impeller exit height to two-thirds between the diffuser inlet and R=1.2, by which the pressure recovery in the diffuser is not deteriorated.(6)The unstable flow range of the test blower was reduced significantly by about 45% in total from φ=0.316 to 0.174 by implementing the ring groove arrangement for the inducer inlet as well as the narrowed diffuser width for the diffuser exit. Less
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石田正弘: "遠心送風機の低流量域不安定流動の抑制;ディフューザ失速の抑制"日本機械学会2003年次大会講演会講演論文集. No. 03-1. 29-30 (2003)
Masahiro Ishida:“离心式鼓风机低流量区域的不稳定流动的抑制;扩散器失速的抑制”日本机械工程学会2003年年会论文集第03-1号(2003年)。
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Ishida, Masahiro: "Numerical Investigation of Inducer Stall at Small Flow Rates in a Centrifugal Blower (Effect of Blade Leading Shape on Flow Separation)"Proc.of the 4th International Conference on Pumps and Fans. 206-212 (2002)
Ishida, Masahiro:“离心鼓风机中小流量导流失速的数值研究(叶片引导形状对流动分离的影响)”第四届国际泵和风机会议论文集。
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石田正弘: "遠心送風機の低流量域不安定流動の抑制;インデューサ・ディフューザ失速の同時抑制"日本機械学会2003年次大会講演会講演論文集. No. 03-1. 31-32 (2003)
石田正宏:“离心式鼓风机低流量区域不稳定流动的抑制;诱导轮和扩压器失速的同时抑制”日本机械工程师学会2003年年会论文集第03-1号。 )
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Masahiro Ishida, Zixiang Sun, Taufan Surana, Daisaku Sakaguchi: "Numerical Investigation of Inducer Stall at Small Flow ate in a Centrifugal Blower (Effect of Blade Leading Shape on Flow Separation)"Proc. of 4^<th> International Conference on Pumps and Fu
Masahiro Ishida,Zixiang Sun,Taufan Surana,Daisaku Sakaguchi:“离心鼓风机小流量诱导器失速的数值研究(叶片引导形状对流动分离的影响)”Proc。
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石田正弘: "羽なしディフューザの不安定現象について"日本機械学会研究協会部会RC178研究分科会研究報告書. 125-135 (2002)
Masahiro Ishida:《关于无叶片扩压器的不稳定现象》日本机械工程学会研究会小组委员会RC178研究小组委员会研究报告125-135(2002)。
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共 32 条
Verification of Unstable Flow Mechanism due to Inducer Tip Leakage Vortex in a Centrifugal Blower
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批准号:16560152
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.05万
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财政年份:2004
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负责人:ISHIDA Masahiro
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依托单位:
SUPPRESSION OF UNSTABLE FLOW IN CENTRIFUGAL BLOWERS BY THREE-DIMENSIONAL SEPARATION CONTROL
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批准号:10650183
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.3万
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财政年份:1998
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负责人:ISHIDA Masahiro
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依托单位: