Turbine engine component and corresponding manufacturing method

摘要

A turbine engine component (120) has an airfoil portion (123) with a tip portion (129) and the tip portion (129) has at least one chamfered edge (140, 142) on one side. If desired, the tip portion (129) may have a first chamfered edge (140) on a first side (145) and a second chamfered edge (142) on a second side (146) opposed to the first side (145). A flattened tip portion (144) may extend between the first and second chamfered edges (140, 142). A tip treatment (132) may be applied to the flattened tip portion (144). A corresponding method of creating such a turbine engine component is also described.