| 发明名称 |
Gas Turbine Engine With Accessory Gear Box |
| 摘要 |
A nacelle for incorporation into a gas turbine engine has an inner wall defining a bypass duct, and an outer wall. At least one drive shaft extends through the inner wall. The at least one drive shaft is connected to a gas turbine engine receiving the nacelle. The at least one drive shaft is connected to drive at least two accessory gear boxes, with the at least two accessory gear boxes being received between the inner and outer walls of the nacelle. A gas turbine engine is also disclosed. |
| 申请公布号 |
US2014165589(A1) |
申请公布日期 |
2014.06.19 |
| 申请号 |
US201213719303 |
申请日期 |
2012.12.19 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Cloft Thomas G.;Gukeisen Robert L.;Mercier Claude |
| 分类号 |
F02C7/26 |
主分类号 |
F02C7/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A nacelle for incorporation into a gas turbine engine, comprising:
a nacelle having an inner wall defining a bypass duct, and an outer wall, at least one drive shaft extending through said inner wall, said at least one drive shaft to be connected to a gas turbine engine receiving the nacelle, said at least one drive shaft being connected to drive at least two accessory gear boxes, with said at least two accessory gear boxes being received between said inner and outer walls of said nacelle.
|
| 地址 |
Hartford CT US |
