| 发明名称 |
DE-COUPLE GEARED TURBO-FAN ENGINE AND AIRCRAFT |
| 摘要 |
A turbofan engine includes a core engine section including a compressor section feeding air to a combustor to generate high speed exhaust gases that drive a turbine section all disposed about an engine axis, a geartrain driven by the core engine section, a fan section driven by the geartrain about a fan axis spaced apart from the engine axis, and an accessory gearbox driven by the geartrain and mounted apart from the core engine section and the fan section. |
| 申请公布号 |
US2014252161(A1) |
申请公布日期 |
2014.09.11 |
| 申请号 |
US201414188989 |
申请日期 |
2014.02.25 |
| 申请人 |
United Technologies Corporation |
发明人 |
Gukeisen Robert L. |
| 分类号 |
B64D27/14;F02C7/36;B64D27/12 |
主分类号 |
B64D27/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbofan engine comprising:
a core engine section including a compressor section feeding air to a combustor to generate high speed exhaust gases that drive a turbine section all disposed about an engine axis; a geartrain driven by the core engine section; a fan section driven by the geartrain about a fan axis spaced apart from the engine axis; and an accessory gearbox driven by the geartrain and mounted apart from the core engine section and the fan section. |
| 地址 |
Hartford CT US |
