Line replaceable unit with universal heat sink receptacle
View Patent ↗A line replaceable unit includes a universal heat sink receptacle formed in an inner surface of a wall of an enclosure. The universal heat sink receptacle is configured to receive a heat spreader for any standard or custom COM Express module so that the line replaceable unit may be efficiently reconfigured with different COM Express modules if needed.
1. A wall for a line replaceable unit, the wall comprising: an inner surface and an outer surface; at least one heat radiating fin disposed on the outer surface; and a universal heat sink receptacle formed on the inner surface, the universal heat sink receptacle being configured to receive a heat spreader of a COM module, the universal heat sink receptacle being sized and shaped to receive more than one type of COM module, wherein the universal heat sink receptacle is configured to remove heat from the heat spreader without a fan by conducting heat from the heat spreader, through the inner and outer surfaces of the wall, and into the at least one heat radiating fin; wherein a second heat conducting tower is spaced apart from the primary recessed slot, the second heat conducting tower being configured to remove heat from a heat sink of another component; wherein the second heat conducting tower is configured to receive a plurality of applications of thermally conducting paste arranged in a T-formation on the second heat conducting tower, wherein the second heat conducting tower is configured to receive two sets of two applications of thermally conductive paste disposed on the second heat conducting tower, each set of applications being arranged in a line that is substantially perpendicular to the other set of applications.
2. The wall of claim 1 , wherein the universal heat sink receptacle includes a primary recessed slot that is sized and shaped to accept a heat spreader of any standard COM module.
3. The wall of claim 2 , wherein the universal heat sink receptacle is configured to receive a plurality of applications of thermally conductive paste between the wall and a COM module.
4. The wall of claim 3 , wherein the universal heat sink receptacle is configured to receive an application of thermally conductive paste arranged in a three by four grid of applications.
5. The wall of claim 4 , wherein the universal heat sink receptacle further comprises a first heat conducing tower disposed adjacent to the primary recessed slot, the first heat conducting tower being sized and shaped to contact another heat generating component.
6. The wall of claim 5 , wherein the first heat conducing tower is configured to receive a set of three applications of thermally conductive paste arranged in a line on the first heat conducing tower.
7. The wall of claim 1 , wherein the second heat conducting tower is T-shaped.
8. The wall of claim 1 , wherein the outer surface includes a plurality of heat dissipating elements.
9. The wall of claim 8 , wherein at least one of the heat dissipating elements is a heat radiating fin.
10. The wall of claim 8 , wherein heat is conducted from the universal heat sink receptacle to the heat dissipating element through the outer wall.
11. The wall claim 1 , wherein the universal heat sink receptacle is configured to be coupled to two or more types of COM modules that are selected from the group consisting of a mini module, a compact module, a basic module, and an extended module.
12. The wall of claim 1 , wherein the universal heat sink receptacle is rectangular in shape measuring approximately 125 mm by approximately 95 mm.
13. An aircraft local area network system with internet access, the system comprising: a radio antenna on an aircraft; a line replaceable unit operatively connected to the radio antenna, the line replaceable unit including a container having opposing outer walls, the opposing outer walls having an inner surface and an outer surface, a plurality of heat radiating fins disposed on the outer surface of at least one of the outer walls, a carrier board disposed between the outer walls, a COM module operatively connected to the carrier board, and a heat spreader operatively connected to the COM module, wherein the inner surface of the at least one outer wall includes a universal heat sink receptacle that is configured to remove heat from the heat spreader without a fan by conducting heat from the heat spreader through the at least one outer wall and into the heat radiating fins, the universal heat sink receptacle being configured to receive the heat spreader, and the universal heat sink receptacle also being configured to receive more than one type of COM module; and a wireless transceiver for transmitting and receiving wireless signals within the aircraft, the wireless transceiver being communicatively connected to the line replaceable unit;
wherein the universal heat sink receptacle is configured to receive a plurality of applications of thermally conducting paste between the universal heat sink receptacle and the COM module.
14. The system of claim 13 , wherein the applications of thermally conducting paste are configured in a three by four grid.