发明名称 |
HEAT DISSIPATING ASSEMBLY |
摘要 |
A heat dissipating assembly includes a substrate configured to support at least one heat producing component and a thermally conductive cooling fin extending from the substrate, wherein heat is conducted away from the heat producing component. |
申请公布号 |
US2016047604(A1) |
申请公布日期 |
2016.02.18 |
申请号 |
US201414460655 |
申请日期 |
2014.08.15 |
申请人 |
GE Aviation Systems LLC |
发明人 |
Engelhardt Michel;Swanson Judd Everett |
分类号 |
F28D15/04 |
主分类号 |
F28D15/04 |
代理机构 |
|
代理人 |
|
主权项 |
1. A heat dissipating assembly, comprising:
a substrate configured to support at least one heat producing component; a thermally conductive cooling fin extending from the substrate; and a thermally conductive heat pipe conductively coupled to the heat producing component, extending within at least a portion of the cooling fin, and defining a fluid reservoir containing a phase change fluid; wherein the phase change fluid changes between a liquid and a gas in response to heat conducted from the heat producing component to the heat pipe. |
地址 |
Grand Rapids MI US |