Invention Application
US20150300258A1 COOLING HOLE ARRANGEMENT FOR ENGINE COMPONENT 审中-公开
用于发动机部件的冷却孔安装

COOLING HOLE ARRANGEMENT FOR ENGINE COMPONENT
Abstract:
A component for a gas turbine engine according to an exemplary aspect of this disclosure includes a surface having a plurality of cooling holes. The surface includes a first region and a second region each having a plurality of cooling holes. The cooling holes within the first region are arranged differently than the cooling holes in the second region.
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