发明名称 Turbine vane for a gas turbine and casting core for the production of such
摘要 A turbine vane or blade including an interior structure is provided. In addition, turbulence elements connected directly upstream of openings disposed at the rear edge of the blade of the turbine vane or blade are also provided. These are disposed in a sequence, each having a flow side against which a coolant flows and which is at least partially arched in a concave manner. Preferably, the turbulence elements are configured in a crescent-shaped manner. This makes it possible to enlarge the openings without resulting in an increased consumption of coolant. A casting core is also provided. The openings required in the casting core for the production of the webs of a turbine vane or blade may now be placed at further distances than before.
申请公布号 US2011176930(A1) 申请公布日期 2011.07.21
申请号 US200913002986 申请日期 2009.05.19
申请人 AHMAD FATHI;BOLMS HANS-THOMAS;LERNER CHRISTIAN 发明人 AHMAD FATHI;BOLMS HANS-THOMAS;LERNER CHRISTIAN
分类号 F01D5/18;B28B7/28 主分类号 F01D5/18
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