| 发明名称 |
RETURN FLUID AIR COOLER SYSTEM FOR TURBINE COOLING WITH OPTIONAL POWER EXTRACTION |
| 摘要 |
In an aircraft including a gas turbine engine, a system for cooling the gas turbine engine includes a tank provided in a wing of the aircraft, the tank being configured to store a cooling fluid supply; and a heat exchanger provided in the gas turbine engine configured to exchange heat from the compressor discharge air to the cooling fluid. |
| 申请公布号 |
US2014345292(A1) |
申请公布日期 |
2014.11.27 |
| 申请号 |
US201313900189 |
申请日期 |
2013.05.22 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
Diaz Carlos Enrique;Carretero Benignos Jorge Alejandro |
| 分类号 |
F02C7/143;F02C7/047 |
主分类号 |
F02C7/143 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. In an aircraft including a gas turbine engine having a compressor and a turbine, a system for cooling compressor discharge air provided to the turbine to cool the turbine, the system comprising:
a tank provided in a wing of the aircraft, the tank being configured to store a cooling fluid supply; and a heat exchanger provided in the gas turbine engine configured to exchange heat from the compressor discharge air to the cooling fluid. |
| 地址 |
Schenectady NY US |
