发明名称 High suction performance and low cost inducer design blade geometry
摘要 An inducer having a hub and a plurality of blades is provided. In one embodiment, the thickness of the blades is defined such that during the operation of the inducer each of the blades is positioned underneath a cavitation vapor line so as to improve the performance of the inducer. In another embodiment, the hub is contoured or ramped according to a fifth order polynomial to provide improved performance. In another embodiment, the flow passage area of the inducer, as taken normal to the flow of fluid, is varied according to a fifth order polynomial to provide improved performance.
申请公布号 US6435829(B1) 申请公布日期 2002.08.20
申请号 US20000497578 申请日期 2000.02.03
申请人 THE BOEING COMPANY 发明人 MENG SEN YIH;PRUEGER GEORGE H.;CHEN WEI-CHUNG
分类号 F04D29/18;F04D29/22;(IPC1-7):F04D29/38 主分类号 F04D29/18
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