发明名称 |
Small engine cooled cooling air system |
摘要 |
A system (32) for managing thermal transfer in an aircraft includes a fuel stabilization unit (44), a fuel-air heat exchanger (50), and a turbine (60). The fuel-air heat exchanger (50) is located downstream from the fuel stabilization unit (44). The fuel-air heat exchanger (50) places deoxygenized fuel in a heat exchange relationship with compressor (58) bleed air to produce heated deoxygenized fuel and cooled bleed air. The turbine (60) is operationally connected to the engine compressor (58) and receives cooled bleed air from the fuel-air heat exchanger (50) to cool the turbine (60). |
申请公布号 |
EP2617649(A2) |
申请公布日期 |
2013.07.24 |
申请号 |
EP20130152101 |
申请日期 |
2013.01.21 |
申请人 |
HAMILTON SUNDSTRAND CORPORATION |
发明人 |
RHODEN, WILLIAM E.;JALBERT, PETER L.;BEAUPRE, RUDOLPH THOMAS;SCOTT, DAVID RUSSELL |
分类号 |
B64D13/00;B64D37/34 |
主分类号 |
B64D13/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|