发明名称 GAS TURBINE BLADE COOLING ARRANGEMENT
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 air foil coolant channels formed in the buckets of the turbine. The V-shaped notch weirs serve to desensitize the flow of coolant into the individual platform and air foil coolant channels to design tolerances and non-uniform flow distribution.
申请公布号 GB2021699(A) 申请公布日期 1979.12.05
申请号 GB19790012918 申请日期 1979.04.12
申请人 GENERAL ELECTRIC CO 发明人
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
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