发明名称 |
Gas turbine rotor blade tip cooling device |
摘要 |
In a gas turbine hollow cooled rotor blade, a plurality of cooling holes 3 and 5 are provided which communicate between a cooling air passage in the blade and the tip squealer portion 1 on the pressure side and between the cooling air passage in the blade and a position in the vicinity of the suction side of a tip cap 4.
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申请公布号 |
US5564902(A) |
申请公布日期 |
1996.10.15 |
申请号 |
US19950426187 |
申请日期 |
1995.04.21 |
申请人 |
MITSUBISHI JUKOGYO KABUSHIKI KAISHA |
发明人 |
TOMITA, YASUOKI |
分类号 |
F01D5/18;F01D5/20;F02C7/18;(IPC1-7):F01D5/18 |
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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