Patent ID: 8522558

Claim:
A gas turbine engine component comprising: a wall of the gas turbine engine component having first and second wall surfaces; a first cooling hole extending through the wall and comprising: an inlet located at the first wall surface; an outlet located at the second wall surface and comprising: first and second lateral ends; and a trailing edge; a metering section extending downstream from the inlet; and a diffusing section extending from the metering section to the outlet, the diffusing section comprising: first and second lobes, each lobe diverging longitudinally and laterally from the metering section; and a second cooling hole extending through the wall and comprising: an inlet located at the first wall surface; an outlet located at the second wall surface and comprising: first and second lateral ends; and a trailing edge; a metering section extending downstream from the inlet; and a diffusing section extending from the metering section to the outlet, the diffusing section comprising: first and second lobes, each lobe diverging longitudinally and laterally from the metering section, wherein one of the lateral ends of the outlet of the first cooling hole and one of the lateral ends of the outlet of the second cooling hole meet upstream of the trailing edge of the first cooling hole and the trailing edge of the second cooling hole.