发明名称 Compressor part span shroud
摘要 A compressor blade assembly for a compressor operating at transonic or supersonic blade speeds has a part span shroud. The shroud is twisted having a first angle in the direction of airflow on one side of the shock wave and a second angle in the direction of airflow on the other side of the shock wave.
申请公布号 US4798519(A) 申请公布日期 1989.01.17
申请号 US19870088776 申请日期 1987.08.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ZIPPS, ROBERT H.;LYONS, KENT A.;GRIFFIN, EVANS E.
分类号 F01D5/22;F04D21/00;F04D29/32;(IPC1-7):F01D5/22 主分类号 F01D5/22
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