Invention Application
US20160348517A1 INTERNALLY COOLED TURBINE BLISK AND METHOD OF MANUFACTURE 有权
内部冷却涡轮泡罩及其制造方法

INTERNALLY COOLED TURBINE BLISK AND METHOD OF MANUFACTURE
Abstract:
A method of manufacturing an internally cooled blisk by additive manufacturing processes to provide weight reduction and power-to-weight ratio improvement, leading to improved efficiency, a decrease in fuel burn and lifecycle costs in an engine employing the internally cooled blisk. The method of manufacturing including defining a configuration for the internally cooled blisk, the configuration comprising a disk, an annular array of angularly spaced blades extending about a periphery of the disk and one or more internal cooling features defined within the internally cooled blisk. The method further including the step of programming the configuration into an additive manufacturing system. A powder is deposited into a chamber and an energy source is applied to the deposited powder to consolidate the powder into a cross-sectional shape corresponding to the defined configuration. Additionally provided is an internally cooled blisk.
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