Invention Grant
US09316104B2 Film cooling channel array having anti-vortex properties 有权
具有防涡流特性的薄膜冷却通道阵列

Film cooling channel array having anti-vortex properties
Abstract:
A cooling channel array carried by a component wall of a gas turbine engine is provided. The cooling channel array comprises a diffusion cavity and a metering section. The metering section comprises a main hole and two or more side holes. The side holes may be separate from the main hole or may branch off of the main hole. The diffusion cavity may incorporate a lobed configuration to help diffuse cooling fluid as it exits the cooling channel array.
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