| 发明名称 |
ACCESSORY MOUNTING FOR A GAS TURBINE ENGINE |
| 摘要 |
A gas turbine engine assembly is connected to a pylon for mounting the gas turbine engine to an aircraft. The assembly has a frame supporting at least one accessory independently of the gas turbine engine. The frame is attached to the pylon at forward and rearward engine mounting locations. The frame comprises at least one hollow tube and at least one duct is arranged to supply coolant into the at least one hollow tube and the at least one hollow tube is arranged to supply coolant to the at least one accessory. |
| 申请公布号 |
US2014366555(A1) |
申请公布日期 |
2014.12.18 |
| 申请号 |
US201414284809 |
申请日期 |
2014.05.22 |
| 申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
BEIER Jürgen |
| 分类号 |
F02C7/20 |
主分类号 |
F02C7/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine assembly connected to a pylon structure for mounting the gas turbine engine to an aircraft,
the assembly having a frame supporting at least one accessory independently of the gas turbine engine, the frame being attached to the pylon at forward and rearward engine mounting locations, the frame comprising at least one hollow tube, a supply of coolant being arranged to supply coolant into the at least one hollow tube and the at least one hollow tube being arranged to supply coolant to the at least one accessory. |
| 地址 |
Dahlewitz DE |
