发明名称 Spool for turbo machinery
摘要 A spool (14) for turbo machinery comprises a fluid flow path (16) defined by an axial compressor stage (18) adjacent to a mixed flow compressor stage (20) to thereby provide a compression system which has a relatively high ratio of efficiency to compressor diameter.
申请公布号 GB2503495(B) 申请公布日期 2014.12.03
申请号 GB20120011537 申请日期 2012.06.29
申请人 ROLLS-ROYCE PLC 发明人 STEPHEN JOHN BRADBROOK;BRIAN DAVIS
分类号 F02C3/08;F02C3/04;F04D1/02;F04D13/12;F04D17/02 主分类号 F02C3/08
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