发明名称 Closed circuit blade-cooled turbine
摘要 In a closed circuit moving blade cooled turbine, holes in the radial direction formed in the outer periphery of a second stage wheel are led to cooling air supply holes to second stage moving blades and to prevent the cooling air from leaking into the junction, the holes in the radial direction and the cooling air supply holes are interconnected and the supply members covering the junction are fit into them. The cooling air after cooling the second stage moving blades is introduced into the collection holes formed in the outer periphery of the spacer via the cooling air collection holes and to prevent the cooling air from leaking into the boundary, the cooling air collection holes and collection holes are interconnected and the collection members covering the boundary are fit into them. To make the sum of minimum sectional areas of the respective paths of the second stage moving blades smaller than the sum of minimum sectional areas of the respective paths of the first stage moving blades, the minimum sectional member is incorporated into the supply member.
申请公布号 US2004170494(A1) 申请公布日期 2004.09.02
申请号 US20040793771 申请日期 2004.03.08
申请人 HITACHI, LTD. 发明人 MARUSHIMA SHINYA;ANZAI SHUNICHI;NODA MASAMI;MATSUMOTO MANABU;KIZUKA NOBUAKI;TAKANO TSUYOSHI
分类号 F01D5/08;F02C7/18;(IPC1-7):F01D5/14 主分类号 F01D5/08
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