发明名称 SHANK CAVITY AND COOLING HOLE
摘要 A turbine bucket is provided and includes a shank defining a cavity therein, which is connectible with a rotor such that wheelspace air having an initial pressure is permitted to flow into the cavity and a platform coupled to the shank and defining a cooling hole therein, the shank and the platform each further defining the cavity and the cooling hole, respectively, as being fluidly communicative with one another, such that the wheelspace air permitted to flow into the cavity is deliverable from the cavity and through the cooling hole at a second pressure greater than the initial pressure.
申请公布号 US2012070305(A1) 申请公布日期 2012.03.22
申请号 US20100783028 申请日期 2010.05.19
申请人 AMMANN LUKE JOHN;SAMPAYO CAMILO ANDRES;GENERAL ELECTRIC COMPANY 发明人 AMMANN LUKE JOHN;SAMPAYO CAMILO ANDRES
分类号 F01D5/18 主分类号 F01D5/18
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