发明名称 COOLING STRUCTURE OF MOVING BLADE FOR GAS TURBINE
摘要 PURPOSE:To aim at equalization of the temperature at a blade effective part by forming a hollow blade-effective part from a plurality of cylindrical cooling- medium conduit tubes bonded together in series, and then feeding a cooling medium into the conduit tubes by means of an orifice plate. CONSTITUTION:A plurality of cylindrical cooling-medium conduit tubes 3 are bonded together with an adhesive 5 so that a hollow blade-effective part 2 is formed. The conduit tubes 3 are connected by means of an orifice plate 9 to a cooling-medium inlet passage 8 at a blade root part 1. The orifice plate 9 is used to adjust the velocity of flow within the conduit tubes. Thereby, the temperatures at the blade effective part 2 can be equalized.
申请公布号 JPS62282102(A) 申请公布日期 1987.12.08
申请号 JP19860124376 申请日期 1986.05.29
申请人 TOSHIBA CORP 发明人 HIJIKATA TSUNEO
分类号 F01D5/18 主分类号 F01D5/18
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