Abstract:
Arrangements described herein relate to apparatuses, systems, and methods for a housing of an unmanned aerial vehicle (UAV), the housing includes but is not limited to a metallic porous material having a shape of an enclosure of the UAV, and a phase change material (PCM) provided in at least a portion of the metallic porous material. The metallic porous material and the PCM are configured to passively cool the UAV.
Abstract:
A device that includes a region comprising a heat generating device, and an energy harvesting device coupled to the region comprising the heat generating device. The energy harvesting device includes a first thermal conductive layer, a thermoelectric generator (TEG) coupled to the first thermal conductive layer, and a second thermal conductive layer coupled the thermoelectric generator (TEG) such that the thermoelectric generator (TEG) is between the first thermal conductive layer and the second thermal conductive layer. In some implementations, the energy harvesting device includes an insulation layer.
Abstract:
A package-on-package (PoP) device includes a first package, a second package, and a bi-directional thermal electric cooler (TEC). The first package includes a first substrate and a first die coupled to the first substrate. The second package is coupled to the first package. The second package includes a second substrate and a second die coupled to the second substrate. The TEC is located between the first die and the second substrate. The TEC is adapted to dynamically dissipate heat back and forth between the first package and the second package. The TEC is adapted to dissipate heat from the first die to the second die in a first time period. The TEC is further adapted to dissipate heat from the second die to the first die in a second time period. The TEC is adapted to dissipate heat from the first die to the second die through the second substrate.