发明名称 COOLED BLADE OF GAS TURBINE
摘要 PURPOSE:To improve turbine efficiency by mounting turbulence promotors between an insert in a blade and an inner coat of the blade. CONSTITUTION:An insert 5 is provided in a blade and a spacer 7 is provided between the insert 5 and the inner coat of the blade. Turbulance promotors 8 are mounted to the circumference of the spacer 7 and the promotor 8 and brought in contact with the inner coat of the blade by contact members 9 in the insert 5. Thus, heat transfer amount from the inner coat of the blade to a cooling passage is increased around twice as much and cooling fluid amount is reduced, then turbine efficiency can be improved.
申请公布号 JPS60182304(A) 申请公布日期 1985.09.17
申请号 JP19840036209 申请日期 1984.02.29
申请人 TOSHIBA KK 发明人 OKAMOTO YASUO
分类号 F01D5/18;(IPC1-7):F01D5/18 主分类号 F01D5/18
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