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公开(公告)号:US20240240646A1
公开(公告)日:2024-07-18
申请号:US18410173
申请日:2024-01-11
Inventor: Weiwei CUI , Fei YAO , Xiaonan WANG , Changlong RUAN , Haobo CAO , Laishun YANG , Guozhang CHANG , Cuiping WANG , Guangxi YUE
CPC classification number: F04D29/284 , F04D17/10
Abstract: A subsonic compressor, a rotor blade and a method for flow stability enhancement are provided. The subsonic compressor includes a hub and a casing, a tip clearance is formed between a tip of the rotor blade and an inner wall of the casing. The tip clearance is formed as a circumferential diverging leakage passage expanding from a pressure surface side of the rotor blade of the subsonic compressor at the tip to a suction surface side of the rotor blade at the tip.