| 发明名称 |
Aircraft auxiliary gas turbine engine and method for operating the same |
| 摘要 |
<p>A non-aircraft-propelling auxiliary gas turbine engine (10) installable in an aircraft (12) having a cabin (16) adapted to be pressurized. The auxiliary gas turbine engine includes an auxiliary-gas-turbine-engine compressor (18) having an inlet (20), wherein the inlet is adapted to receive pressurized air (22) from the cabin.</p> |
| 申请公布号 |
EP1816071(A2) |
申请公布日期 |
2007.08.08 |
| 申请号 |
EP20070101566 |
申请日期 |
2007.02.01 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BALAN, CHELLAPPA;SHELDON, KARL EDWARD |
| 分类号 |
B64D33/02;B64D41/00;F01D13/02 |
主分类号 |
B64D33/02 |
| 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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