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