发明名称 TURBINE BLADES WITH PLATFORM COOLING AND CORRESPONDING GAS TURBINE
摘要 <p>A turbine blade generally includes a platform having a pressure side, a suction side, a leading edge, a trailing edge, a pressure side slash face and a suction side slash face. A platform cooling circuit extends within the platform. The platform cooling circuit may extend from the suction side of the platform to the pressure side of the platform. The platform cooling circuit generally defines a fluid flow path that directs a cooling medium from the platform suction side to the platform pressure side.</p>
申请公布号 WO2014055811(A1) 申请公布日期 2014.04.10
申请号 WO2013US63359 申请日期 2013.10.04
申请人 GENERAL ELECTRIC COMPANY 发明人 BOYER, BRADLEY TAYLOR;GOOD, RANDALL RICHARD
分类号 F01D5/18 主分类号 F01D5/18
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