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US09052707B2 Turbomachine component machining method 有权
涡轮机组件加工方法

Turbomachine component machining method
Abstract:
An exemplary component manufacturing method includes scanning a first surface of a component to determine a location of pocket surfaces of the first surface. The method machines apertures in the component from a second, opposite surface of the component. The apertures each have a cooling air inlet within one of the pocket surfaces and a cooling air outlet within the first surface.
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