| 发明名称 |
VENTILATION SYSTEM USING THRUST REVERSER LINKAGES |
| 摘要 |
A gas turbine engine includes a fan duct, an inner fixed structure, and a thrust reverser assembly. The inner fixed structure forms an inner diameter of the fan duct and encloses a core compartment. The thrust reverser assembly includes a linkage assembly mounted to the inner fixed structure within the fan duct. The linkage assembly is adapted to act as a ventilation system that allows for communication between the fan duct and the core compartment. |
| 申请公布号 |
US2015369171(A1) |
申请公布日期 |
2015.12.24 |
| 申请号 |
US201414765917 |
申请日期 |
2014.03.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PAPA Federico;VIVAR Pilar Del Carmen |
| 分类号 |
F02K1/70;F02C7/18;F02K1/76 |
主分类号 |
F02K1/70 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An gas turbine engine comprising:
a fan duct; an inner fixed structure forming an inner diameter of the fan duct and enclosing a core compartment; and a thrust reverser assembly including a linkage assembly mounted to the inner fixed structure within the fan duct, wherein the linkage assembly is adapted to act as a ventilation system that allows for communication between the fan duct and the core compartment. |
| 地址 |
Hartford CT US |
