CPC F01D 5/20 (2013.01) [F05D 2240/307 (2013.01); F05D 2260/941 (2013.01)] | 12 Claims |
1. An airfoil for a turbomachine, comprising:
a leading edge and a trailing edge joined to each other by a suction side and a pressure side and which, in a least one region, extends in a curved manner from an airfoil root to an airfoil tip, wherein the airfoil tip has a squealer tip, which is arranged along a centroid curve at the airfoil tip, wherein the centroid curve passes through the centroidal axes of the airfoil.
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