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 GB201211537(D0) 申请公布日期 2012.08.08
申请号 GB20120011537 申请日期 2012.06.29
申请人 ROLLS-ROYCE PLC 发明人
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