发明名称 COOLED GAS TURBINE BLADE
摘要 The airfoil shaped body has a separate leading edge portion (14) spaced from the main body (12). Slots (40) thereby formed, discharge film cooling air parallel to surface (38) of the main body. A plurality of axially extending fines (42) may interconnect lip (36) and surface (38), thus providing flow straightening means and a means for maintaining a consistant flow area of the discharge slots (40).
申请公布号 EP0330601(B1) 申请公布日期 1992.01.02
申请号 EP19890630018 申请日期 1989.01.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HALL, KENNETH B.;LANDIS, KENNETH K.
分类号 F01D5/18 主分类号 F01D5/18
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