| 发明名称 |
AIRCRAFT HEAT EXCHANGE SYSTEM INCLUDING A THERMOELECTRIC DEVICE |
| 摘要 |
A heat exchange system for an aircraft includes an aircraft controller for controlling an operation of an aircraft, a thermoelectric device having a low temperature side and a high temperature side, an inlet line that carries fluid through the low temperature side of the thermoelectric device and to the aircraft controller; and an outlet line that carrier the fluid away from the and aircraft controller through the high temperature side of the thermoelectric device. Heat is transferred away from the inlet line to the outlet line through the thermoelectric device when a predetermined condition is met. |
| 申请公布号 |
US2017027082(A1) |
申请公布日期 |
2017.01.26 |
| 申请号 |
US201514808523 |
申请日期 |
2015.07.24 |
| 申请人 |
Hamilton Sundstrand Corporation |
发明人 |
Rhoden William E.;Lents Charles E. |
| 分类号 |
H05K7/20;B64D37/34;B64D37/02 |
主分类号 |
H05K7/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A heat exchange system for an aircraft comprising:
an aircraft controller for controlling an operation of an aircraft; a thermoelectric device having a low temperature side and a high temperature side; an inlet line that carries fluid through the low temperature side of the thermoelectric device and to the aircraft controller, and an outlet line that carries the fluid away from the and aircraft controller through the high temperature side of the thermoelectric device; wherein heat is transferred away from the inlet line to the outlet line through the thermoelectric device when a predetermined condition is met. |
| 地址 |
Charlotte NC US |
