发明名称 COOLED GAS TURBINE BLADE
摘要 An improved cooling system for a gas turbine is disclosed. A plurality of V-shaped notch weirs are utilized to meter a coolant liquid from a pool of coolant into a plurality of platform and airfoil coolant channels formed in the buckets of the turbine. The V-shaped notch weirs are formed in a separately machined cylindrical insert and serve to desensitize the flow of coolant into the individual platform and airfoil coolant channels to design tolerances and non-uniform flow distribution.
申请公布号 GB2051256(B) 申请公布日期 1983.01.19
申请号 GB19800016341 申请日期 1980.05.16
申请人 GEC US 发明人
分类号 F01D5/08;F01D5/18 主分类号 F01D5/08
代理机构 代理人
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