发明名称 MULTISTAGE TURBOCOMPRESSOR WITH MIXEDFLOW IMPELLERS
摘要 <p>The majority of the impellers of a multistage turbocompressor are diagonal-flow or "mixed-flow" type impellers with exit flow angles which are increased from the initial stage impellers toward the final stage impellers, whereby the specific speed of each impeller falls with the optimal range for that impeller.</p>
申请公布号 GB2018359(B) 申请公布日期 1982.11.17
申请号 GB19790007957 申请日期 1979.03.07
申请人 KAWASAKI JUKOGYO KK 发明人
分类号 F04D17/12;F04D25/16;(IPC1-7):04D17/06 主分类号 F04D17/12
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