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|1. (WO2015126448) GAS TURBINE ENGINE AIRFOIL|
|Applicants:||UNITED TECHNOLOGIES CORPORATION
|Inventors:||GALLAGHER, Edward J.
BRILLIANT, Lisa I.
STRACCIA, Joseph C.
STEPHENS, Mark A.
BALAMUCKI, Stanley J.
|Title:||GAS TURBINE ENGINE AIRFOIL|
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.