发明名称 METHOD AND APPARATUS FOR REDUCING AXIAL COMPRESSOR BLADE TIP FLOW
摘要 A turbine machine of the type having a high pressure compressor positioned in a casing is provided with a plurality of rotating compressor blades with at least one air channel formed in the blades for air flow communication from the base to the tip for extracting and pressurizing air from an inner area proximate the disk and conveying the extracted and pressurized air into an area between the blade tip and casing for blocking air flow across the tips of the blades.
申请公布号 US2007122280(A1) 申请公布日期 2007.05.31
申请号 US20050164636 申请日期 2005.11.30
申请人 GENERAL ELECTRIC COMPANY 发明人 DONG ZHIFENG;RAHAIM JOHN J.
分类号 F01D5/18 主分类号 F01D5/18
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