Invention Application
US20150118045A1 METHOD AND SYSTEMS FOR PROVIDING COOLING FOR A TURBINE ASSEMBLY 有权
用于为涡轮组件提供冷却的方法和系统

METHOD AND SYSTEMS FOR PROVIDING COOLING FOR A TURBINE ASSEMBLY
Abstract:
A system for providing cooling of a turbine rotor wheel includes a rotor wheel including a plurality of dovetail slots spaced circumferentially about a peripheral surface of the rotor wheel. Each of the dovetail slots includes a pair of opposite upper slot tangs and a pair of opposite lower slot tangs. The system also includes at least one turbine blade. The turbine blade includes an airfoil, a platform, and a dovetail. The dovetail includes a pair of opposite upper dovetail tangs and a pair of opposite lower dovetail tangs. The dovetail further includes at least one inlet aperture extending longitudinally therethrough. The pair of upper dovetail tangs include a first cooling hole extending therethrough and coupled in flow communication with the at least one inlet aperture.
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