发明名称 Turbine airfoil platform cooling circuit
摘要 An airfoil assembly includes an airfoil extending away from a platform. One or more cooling circuits are formed through the platform in order to provide cooling of the platform. The cooling circuit may include a downwardly directed inlet receiving cooling air from below the platform. The cooling air is then directed in a direction generally parallel to the outer surface of the platform and through exits formed through the outer surface of the platform. The cooling circuit may optionally include a plurality of pedestals extending from an outer wall to an inner wall of the cooling circuit to increase the rigidity and the cooling function of the cooling circuit.
申请公布号 SG127789(A1) 申请公布日期 2006.12.29
申请号 SG20060001656 申请日期 2006.03.14
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 CUNHA, FRANK, J.;COUCH ERIC;SANTELER, KEITH, A.;GAYMAN, SCOTT, W.;HUDSON, ERIC, A.;JOE CHRISTOPHER;LETIZIA ERIC
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