| 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 (120) includes providing access from a forward section of the gas turbine engine (120) to a gearbox (148) contained within a bearing compartment (B). |
| 申请公布号 |
EP2597292(A3) |
申请公布日期 |
2016.12.21 |
| 申请号 |
EP20120192792 |
申请日期 |
2012.11.15 |
| 申请人 |
United Technologies Corporation |
发明人 |
Davis, Todd A.;Reinhardt, Gregory E.;DiBenedetto, Enzo |
| 分类号 |
F02K3/06;F01D25/16;F02C3/107 |
主分类号 |
F02K3/06 |
| 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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