发明名称 Aerofoil configuration
摘要 A turbine blade comprising a pressure wall and a suction wall joined together at leading and trailing edges and having a root portion and a blade tip region, the walls further define a hollow chamber and through which cooling air is directed in use from the root portion to the blade tip region only, characterized in that at least one of the walls defines at least one cooling rib that extends outwardly from the wall into the chamber and at least a portion of the rib tapers between the root portion and a blade tip region.
申请公布号 US8297925(B2) 申请公布日期 2012.10.30
申请号 US20070000867 申请日期 2007.12.18
申请人 BARRETT DAVID W.;ROLLS-ROYCE PLC 发明人 BARRETT DAVID W.
分类号 F01D5/18 主分类号 F01D5/18
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