| 发明名称 |
Cooled blade for a gas turbine engine |
| 摘要 |
A cooled blade for a gas turbine engine comprises an aerofoil portion having a longitudinally extending hollow. An air entry tube is mounted within the hollow and is pressed against a locating surface within the hollow by a resilient member such as a spring tube.
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| 申请公布号 |
US4162136(A) |
申请公布日期 |
1979.07.24 |
| 申请号 |
US19750563144 |
申请日期 |
1975.04.01 |
| 申请人 |
ROLLS ROYCE (1971) LTD |
发明人 |
PARKES, ROGER J |
| 分类号 |
F01D5/18;F02C;(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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