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公开(公告)号：FR2619868B1
公开(公告)日：1990-07-20
申请号：FR8811123
申请日：1988-08-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ZIPPS ROBERT H , LYONS KENT A , GRIFFIN EVANS E
Abstract: 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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公开(公告)号：GB2208898B
公开(公告)日：1992-02-19
申请号：GB8819735
申请日：1988-08-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ZIPPS ROBERT HOWARD , LYONS KENT A , GRIFFIN EVANS E
Abstract: 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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公开(公告)号：FR2619868A1
公开(公告)日：1989-03-03
申请号：FR8811123
申请日：1988-08-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ZIPPS ROBERT H , LYONS KENT A , GRIFFIN EVANS E
Abstract: 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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公开(公告)号：GB2208898A
公开(公告)日：1989-04-19
申请号：GB8819735
申请日：1988-08-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ZIPPS ROBERT HOWARD , LYONS KENT A , GRIFFIN EVANS E
Abstract: 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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