Unsteady behavior and control of diffuser leading-edge vortex in a centrifugal compressor

Yutaka Ohta*, Takashi Goto, Eisuke Outa

*この研究の対応する著者

研究成果: Conference contribution

20 被引用数 (Scopus)

抄録

The unsteady behavior of a vortex generated on the diffuser leading-edge, which is called the leading-edge vortex (LEV), is discussed through experiments and numerical simulation. The LEV is different from the separating vortex of the diffuser leading-edge and passage vortex of the diffuser, develops rapidly with a decrease in the compressor mass flow rate, and forms a flow blockage in diffuser passages. Therefore, the evolution of the LEV may become a cause of diffuser stall. Additionally, in one attempt to control the LEV, two types of tapered diffuser vanes, which are shroud- or hub-side tapered diffuser vanes, were adopted. Though the shroud-side tapered diffuser vane can effectively reduce the compressor noise level, the compressor performance deteriorates remarkably. On the other hand, the hub-side tapered diffuser vane not only reduces the compressor noise level but also improves the compressor performance. According to the visualization results of the oil-film methods and numerical simulations, the hub-side tapered diffuser vane can suppress the evolution of the LEV in the compressor low-flow-rate operation.

本文言語English
ホスト出版物のタイトルASME Turbo Expo 2010
ホスト出版物のサブタイトルPower for Land, Sea, and Air, GT 2010
ページ1805-1813
ページ数9
PARTS A, B, AND C
DOI
出版ステータスPublished - 2010 12 1
イベントASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010 - Glasgow, United Kingdom
継続期間: 2010 6 142010 6 18

出版物シリーズ

名前Proceedings of the ASME Turbo Expo
番号PARTS A, B, AND C
7

Conference

ConferenceASME Turbo Expo 2010: Power for Land, Sea, and Air, GT 2010
国/地域United Kingdom
CityGlasgow
Period10/6/1410/6/18

ASJC Scopus subject areas

  • 工学(全般)

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