An airfoil of a turbine engine includes, pressure and suction sides extending in a radial direction from a 0% span to a 100% span position. The airfoil has a relationship between a gap/chord ratio and span position that defines a curve with a gap/chord ratio of less than 0.80 from 80% span to 100% span.
申请公布号
WO2015126448(A1)
申请公布日期
2015.08.27
申请号
WO2014US52080
申请日期
2014.08.21
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
GALLAGHER, EDWARD J.;BRILLIANT, LISA I.;STRACCIA, JOSEPH C.;STEPHENS, MARK A.;BALAMUCKI, STANLEY J.;HUDON, KATE
