Invention Grant
US09581028B1 Small turbine stator vane with impingement cooling insert 有权
小型涡轮定子叶片带有冲击冷却插件

Small turbine stator vane with impingement cooling insert
Abstract:
An air cooled turbine stator vane form a small gas turbine engine in which the vane has an airfoil of less than one inch in spanwise height, where the airfoil is a hollow airfoil having an insert that forms a sequential impingement cooling circuit for the pressure side wall and then the suction side wall. The insert includes a plurality of cooling air supply channels connected together by ribs where pressure side impingement holes are formed in the cooling air supply channels and suction side wall impingement cooling holes are formed in the ribs.
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