| 发明名称 |
GAS TURBINE ENGINE ARCHITECTURE WITH LOW PRESSURE COMPRESSOR HUB BETWEEN HIGH AND LOW ROTOR THRUST BEARINGS |
| 摘要 |
A method for servicing a gas turbine engine includes providing access from a forward section of the gas turbine engine to a gearbox contained within a bearing compartment. |
| 申请公布号 |
CA2794888(A1) |
申请公布日期 |
2013.05.23 |
| 申请号 |
CA20122794888 |
申请日期 |
2012.11.07 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
DAVIS, TODD A.;REINHARDT, GREGORY E.;DIBENEDETTO, ENZO |
| 分类号 |
F01D25/16;F01D25/24;F02C7/36 |
主分类号 |
F01D25/16 |
| 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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