Patent ID: 8371814

Claim:
A turbine engine component, comprising: a wall comprising a portion of a combustor liner and including a cool air side and a hot air side; a main opening extending between the cool air side and the hot air side, the main opening having an inlet and an outlet, the inlet formed on the cool air side, and the outlet formed on the hot air side; a first cluster of two or more auxiliary openings extending from the main opening to the hot air side; and a second cluster of two or more auxiliary openings extending from the main opening to the hot air side, wherein: the first cluster of two or more auxiliary openings includes a first auxiliary opening and a second auxiliary opening, the first auxiliary opening of the first cluster of two or more auxiliary openings disposed at a first location on a first axis that is substantially parallel to a centerline through the main opening, and the second auxiliary opening the first cluster of two or more auxiliary openings disposed at a second location on the first axis.