发明名称 Blade for a gas turbine engine
摘要 A main body is provided for a gas turbine engine comprising an outer structure, a first internal partition and a second internal partition. The outer structure and the first internal partition may define an entrance leg of a cooling circuit for receiving a cooling fluid. The second internal partition may include a metering slot. The outer structure, the first internal partition and the second internal partition may define an intermediate leg of the cooling circuit. The intermediate leg may communicate with the entrance leg. The second internal partition and the outer structure may define an exit leg of the cooling circuit. The metering slot meters cooling fluid as it passes from the intermediate leg into the exit leg.
申请公布号 US8202054(B2) 申请公布日期 2012.06.19
申请号 US20070804426 申请日期 2007.05.18
申请人 LIANG GEORGE;SIEMENS ENERGY, INC. 发明人 LIANG GEORGE
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
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