发明授权
US08739404B2 Turbine components with cooling features and methods of manufacturing the same 有权
具有冷却功能的涡轮机组件及其制造方法

Turbine components with cooling features and methods of manufacturing the same
摘要:
The present disclosure is directed to the use and manufacture of cooling features within a component used in a hot gas path, such as within a turbine. In one embodiment, channels are formed within an external surface of the component and filled with a removable material. The external surface and channels may then be coated with one or more layers, such as a structural layer and/or top coat. The removable material may then be removed to leave the channels free of the removable material.
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