| 发明名称 |
AIRCRAFT AUXILIARY GAS TURBINE ENGINE AND METHOD FOR OPERATING |
| 摘要 |
A non-aircraft-propelling auxiliary gas turbine engine (10) installable in a n aircraft (12) having a cabin (16) adapted to be pressurized. The auxiliary gas turbin e 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.
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| 申请公布号 |
CA2576683(A1) |
申请公布日期 |
2007.08.02 |
| 申请号 |
CA20072576683 |
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;B64D13/00;F02C7/045;F02C9/18 |
主分类号 |
B64D33/02 |
| 代理机构 |
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代理人 |
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