Noise reduction and surge margin improvement using tapered diffuser vane in a centrifugal compressor

被引:0
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作者
Takashi Goto
Eri Ohmoto
Yutaka Ohta
Eisuke Outa
机构
[1] Waseda University,Department of Applied Mechanics and Aerospace Engineering
[2] Waseda University,Graduate School of Applied Mechanical Engineering
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关键词
Centrifugal compressor; tapered diffuser vane; interaction tone noise; CFD;
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摘要
Improvement of surge margin and reduction of interaction tone noise radiated from a centrifugal compressor with a vaned diffuser is discussed from experiments and CFD analyses. Two types of one-side tapered diffuser vanes, which are shroud- and hub-side tapered vanes, were used in the experiments. The height of the leading edge of the tapered vanes varied from 100% to 10%. Both types of tapered vanes are effective for the reduction of the interaction tone noise radiated from the compressor, because of the smaller interaction area between impeller-discharge flow and diffuser vane surface. Especially, the hub-side tapered diffuser vane suppresses the evolution of the leading-edge vortex, which causes reverse-flow in the diffuser passage. Furthermore, the hub-side tapered diffuser vane, which has an optimized diffuser leading edge shape, can improve the compressor pressure-rise characteristics at low-flow operation and can enlarge the surge margin.
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页码:21 / 25
页数:4
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