发明名称 TURBINE AIRFOIL
摘要 FIELD: transport.SUBSTANCE: turbine airfoil comprises aerodynamic body, heat protection system existing in coated surface zone and uncoated surface zone with no heat protective coat. Uncoated surface zone extends on airfoil outer surface lower pressure side from trailing edge to leading edge up to interface between surface coated zone and surface uncoated zone. Said interface is located at lower pressure side between leading edge and trailing edge while airfoil body comprises step in outer surface extending along said interface. Another invention of the set relates to turbine guide or working vane with abode described turbine airfoil.EFFECT: better aerodynamics, longer life.24 cl, 3 dwg
申请公布号 RU2554737(C2) 申请公布日期 2015.06.27
申请号 RU20120139957 申请日期 2011.02.15
申请人 SIMENS AKTSIENGEZELL'SHAFT 发明人 BATT STEFEN;MAGGLSTOUN DZHONATAN;VONG LI SHING
分类号 F01D5/28 主分类号 F01D5/28
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