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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.
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公开(公告)号:US20230287890A1
公开(公告)日:2023-09-14
申请号:US18065359
申请日:2022-12-13
Inventor: Weiwei CUI , Kai ZHANG , Fei YAO , Xinglu WANG , Cuiping WANG , Laishun YANG
CPC classification number: F04D19/024 , F04D29/324
Abstract: A vaneless contra-rotating compressor with multiple contra-rotating interfaces and application of the vaneless contra-rotating compressor is provided, which includes at least two vaneless contra-rotating interfaces. For each of the at least two contra-rotating interfaces, the contra-rotating interface corresponds to two of vaneless contra-rotating rotors. A rotating direction of an upstream rotor of the two vaneless contra-rotating rotors and a rotating direction of a downstream rotor of the two vaneless contra-rotating rotors are opposite. Rectifier stator vanes are not provided among all the rotors to supply sufficient inlet negative pre-swirl for the downstream rotors through the upstream rotors. Only the outlet guide vanes of the last stage, of the vaneless contra-rotating rotors are provided. The number of stages and the number of vaneless contra-rotating interfaces may be set flexibly according to the actual pressurization requirements.
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