发明名称 |
Gas turbine with active tip clearance control |
摘要 |
A gas turbine engine includes a compressor, combustor, and turbine having a row of blades mounted inside a surrounding turbine shroud. A heat exchanger is used for cooling pressurized air bled from the compressor. A distribution network joins the heat exchanger to the turbine for selectively channeling air from the heat exchanger below the blades and above the shroud for controlling blade tip clearance. |
申请公布号 |
EP1923539(B1) |
申请公布日期 |
2016.11.02 |
申请号 |
EP20070120717 |
申请日期 |
2007.11.14 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SEITZER, KENNETH EDWARD;SAK, WOJCIECH;DONG, ZHIFENG;ZIEGLER, ROBERT PAUL;GLYNN, CHRISTOPHER CHARLES |
分类号 |
F01D11/24 |
主分类号 |
F01D11/24 |
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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