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US09358643B2 Method for building a gas turbine engine component 有权
燃气涡轮发动机部件的构成方法

Method for building a gas turbine engine component
Abstract:
A method, including: providing a layer of powder material (106) on a substrate (12) having protruding rib material (26); and traversing an energy beam (100) across the layer of powder material to form a cladding layer (10) around and bonded to the protruding rib material, wherein the cladding layer defines a layer of an airfoil skin (94).
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