发明名称 COMPRESSOR BLADE TIP SEAL
摘要 The trench inner wall surrounding the tips (28) of axial flow fan/compressor blades (26) in a turbine type power plant is angularly disposed relative to the gas path wall (20) to allow deeper penetration into the trench and minimize leakage around the tips (28). Gap closure between the inner wall (37) of the trench and tip (28) is contemplated by the contour of the blade/trench.
申请公布号 EP0194957(B1) 申请公布日期 1990.01.31
申请号 EP19860630032 申请日期 1986.03.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HARTER, FRANZ
分类号 F01D5/20;F01D11/08 主分类号 F01D5/20
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