Method of manufacturing a turbomachine component, an airfoil and a gas turbine engine
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United States of America Patent
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Mar 20, 2018
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app pub date -
Jun 27, 2014
filing date -
Dec 30, 2011
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Abstract
One embodiment of the present invention is a unique method of manufacturing a component for a turbomachine, such as an airfoil. Another embodiment is a unique airfoil. Yet another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for cooled gas turbine engine components. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
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