发明名称 Airfoil for a second stage nozzle guide vane
摘要 The present invention provides an airfoil a second 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 US2007183898(A1) 申请公布日期 2007.08.09
申请号 US20060644133 申请日期 2006.12.22
申请人 ROLLS-ROYCE POWER ENGINEERING PLC 发明人 HURST ANDREW J.;HARDING SIMON C.
分类号 B64C27/46 主分类号 B64C27/46
代理机构 代理人
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