An airfoil of a turbine engine includes pressure and suction sides and extends in a radial direction from a 0% span position to a 100% span position. The airfoil has a relationship between a stagger angle and span position that defines a curve with a stagger angle that is greater than 32° from 90% span to 100% span.
申请公布号
WO2015178974(A2)
申请公布日期
2015.11.26
申请号
WO2015US15575
申请日期
2015.02.12
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
GALLAGHER, EDWARD J.;BRILLIANT, LISA I.;STRACCIA, JOSEPH C.;BALAMUCKI, STANLEY J.;STEPHENS, MARK A.;HUDON, KATE
