发明名称 Turbine blade with actively cooled head platform
摘要 The turbine blade(10) has cooling holes(17) in the blade's shroud element(11) running from the inside outwards and parallel to the direction of the blade's movement. Each cooling hole opens out into a surface recess(14) before the outer edge(25) of the shroud element and open to the outer space around the turbine blade. The recess may be located on the upper side(22) of the shroud element, with the cooling holes running into it at the side, or the recess may be on the side edge of the shroud element.
申请公布号 EP1013884(A3) 申请公布日期 2003.11.05
申请号 EP19990811187 申请日期 1999.12.21
申请人 ALSTOM (SWITZERLAND) LTD 发明人 BEECK, ALEXANDER DR.;EL-NASHAR, IBRAHIM DR.;VON ARX, BEAT;WEIGAND, BERNHARD
分类号 F01D5/18;F01D5/22 主分类号 F01D5/18
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