| 发明名称 |
VARIABLE AREA BYPASS NOZZLE |
| 摘要 |
A gas turbine engine includes a first duct, a second duct, and a bladder. The bladder is disposed in the first duct and communicates with the second duct. A first gas flow is capable of passing through the first duct and a second gas flow is capable of passing through the second duct. The bladder is adapted to receive a bleed gas flow from the second duct and inflate within the first duct, thereby decreasing an area in the first duct through which the first gas flow is capable of traveling. |
| 申请公布号 |
US2015122339(A1) |
申请公布日期 |
2015.05.07 |
| 申请号 |
US201414203637 |
申请日期 |
2014.03.11 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Buey John R.;Martin Keegan M. |
| 分类号 |
F02K3/077 |
主分类号 |
F02K3/077 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine, comprising:
a first duct through which a first gas flow is capable of traveling; a second duct through which a second gas flow is capable of traveling; and a bladder disposed in the first duct and communicating with the second duct, wherein the bladder is adapted to receive a bleed gas flow from the second duct and inflate within the first duct, thereby decreasing an area in the first duct through which the first gas flow is capable of traveling. |
| 地址 |
HARTFORD CT US |
