The present invention provides an airfoil for a first 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
WO2007085912(A2)
申请公布日期
2007.08.02
申请号
WO2006IB04190
申请日期
2006.12.22
申请人
ROLLS-ROYCE POWER ENGINEERING PLC;SALTMAN, IVOR;WALTERS, SEAN, ALAN;NAPPER, ANDREW, THOMAS
发明人
SALTMAN, IVOR;WALTERS, SEAN, ALAN;NAPPER, ANDREW, THOMAS