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 GB2445896(B) 申请公布日期 2011.06.22
申请号 GB20080007798 申请日期 2006.12.22
申请人 ROLLS-ROYCE POWER ENGINEERING PLC 发明人 ANDREW JAMES HURST;SIMON CHARLES HARDING
分类号 F01D5/14;F01D9/02;F01D9/04 主分类号 F01D5/14
代理机构 代理人
主权项
地址