发明名称 Airfoil for a third stage nozzle guide vane
摘要 The present invention provides an airfoil for a third stage nozzle guide vane having an external surface with first and second sides. The external surface extends spanwise between a hub and a tip and streamwise between a leading edge and a trailing edge of the airfoil. The external surface includes a contour substantially defined by Table 1 as listed in the specification.
申请公布号 GB2448085(B) 申请公布日期 2011.06.08
申请号 GB20080007797 申请日期 2006.12.21
申请人 ROLLS-ROYCE POWER ENGINEERING PLC 发明人 SAMUEL JOHN CLARKE
分类号 F01D5/14;F01D9/02;F01D9/04 主分类号 F01D5/14
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