Patent ID: 11952912
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F | IPC F

Claim 12:
13. The airfoil of claim 12, wherein the cooling hole defines a cooling hole distance (dH) along the mean camber line between an aft edge of the cooling hole and the first location L1, wherein the cooling hole distance dH is between 0.048 cm and 0.533 cm (0.048 cm≤dH≤0.533 cm), wherein the cooling hole distance dH and the first thickness T1 define a second ratio (R2) as R2=dH/T1, wherein the second ratio R2 is between 0.31 and 2.37 (0.31≤R2≤2.37).