发明名称 PRODUCTION OF AIR COOLED TYPE GAS TURBINE BLADE
摘要 PURPOSE:To cast the gas turbine blade having the cooling holes of high cooling effect by using the glass tubes of rough surfaces as cores. CONSTITUTION:Part or the whole of the surfaces of the glass tubes 6 used as cores for providing cooling holes 5 of the turbine blade are roughly formed such as to satin skin form. The glass tubes 6 are mounted to the metal mold for pattern and a wax pattern 9 is made. The wax pattern 9 is coated with casting material to make a mold. After the turbine blade is cast by using this mold, it is dipped in a hot alkali solution to let the glass tubes 6 remained in the casting elute. By this method, the air cooled type gas turbine blade formed with the cooling holes 5 having suitable roughness on the inside surfaces is perfected. The inside surface shapes of these cooling holes 5 result in increased heat transfer area and increased disturbance of the velocity of flow of the cooling air 7, thereby improving the cooling effect of the blade.
申请公布号 JPS55114435(A) 申请公布日期 1980.09.03
申请号 JP19790020220 申请日期 1979.02.24
申请人 ISHIKAWAJIMA HARIMA HEAVY IND 发明人 KOBAYASHI HIDEO;KATSUMATA ICHIROU
分类号 F01D5/18;B22C1/00;B22C7/06;B22C9/10;B22D19/00;B22D27/04 主分类号 F01D5/18
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