发明名称 GAS TURBINE BLADE
摘要 PURPOSE:To reduce thermal stress on a blade by dividing a blade effective part into a web and a back portions, and providing a high temperature gas flow passage internally. CONSTITUTION:A blade effective part is divided into a web portion 1 and a back portion 9, and molded from a ceramic material. The web portion 1 and the back portion 9 are coupled to each other with an inset 10 placed internally and a high temperature gas flow passage is formed internally. The blade effective part is fitted to a pressurized division via internal and external cylinder surfaces 2 and 3 and insulation members 4 and 5. According to the aforesaid constitution, the blade effective part can be thinned and a temperature difference between blade inside and outside can be made small, thereby the thermal stress on the blade being reduced.
申请公布号 JPS62174501(A) 申请公布日期 1987.07.31
申请号 JP19860015924 申请日期 1986.01.29
申请人 TOSHIBA CORP 发明人 OKAMOTO YASUO
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
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