Invention Grant
US09458725B2 Method and system for providing cooling for turbine components 有权
为涡轮机部件提供冷却的方法和系统

Method and system for providing cooling for turbine components
Abstract:
A method and system for providing cooling of a turbine component that includes a region to be cooled is provided. A recess is defined within the region to be cooled, and includes an inner face. At least one support projection extends from the inner face. The at least one support projection includes a free end. A cover is coupled to the region to be cooled, such that an inner surface of the cover is coupled to the free end of the at least one support projection, such that at least one cooling fluid passage is defined within the region to be cooled.
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