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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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