| 发明名称 |
TURBINE COOLING AIR SUPPLY SYSTEM |
| 摘要 |
<p>Apparatus for supplying pressurized cooling air to the turbine blades (20) of a gas turbine engine is disclosed. Multiple nozzles (38 and 40) of a tangential on-board injection system for pressurizing the cooling air are staged to provide variable rates of cooling airflow to the blades.</p> |
| 申请公布号 |
GB8529998(D0) |
申请公布日期 |
1986.01.15 |
| 申请号 |
GB19850029998 |
申请日期 |
1985.12.05 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
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| 分类号 |
F01D5/08;F02C7/18;(IPC1-7):F02C7/18 |
主分类号 |
F01D5/08 |
| 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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