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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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