Axial field rotary energy device with segmented PCB stator having thermally conductive layer
An axial field rotary energy device has a PCB stator panel assembly between rotors with an axis of rotation. Each rotor has a magnet. The PCB stator panel assembly includes PCB panels. Each PCB panel can have layers, and each layer can have conductive coils. The PCB stator panel assembly can have a thermally conductive layer that extends from an inner diameter portion to an outer diameter portion thereof. Each PCB panel comprises discrete, PCB radial segments that are mechanically and electrically coupled together to form the respective PCB panels.
1. An axial field rotary energy device, comprising:
rotors having an axis of rotation, and each rotor comprises a magnet;
a stator assembly located axially between the rotors, the stator assembly comprises a plurality of printed circuit board (PCB) panels, each PCB panel comprises a plurality of layers, each layer comprises a plurality of coils, and at least one outer portion of the stator assembly comprises an external thermally conductive layer that extends from an inner diameter portion to an outer diameter portion of the stator assembly; and
each PCB panel comprises discrete, PCB radial segments that are mechanically and electrically coupled together to form the respective PCB panels.
2. The device of claim 1 , wherein both major outer sides of the stator assembly comprise respective external thermally conductive layers that are thermally coupled to each other.
3. The device of claim 2 , wherein the external thermally conductive layers are thermally coupled with a plurality of vias.
4. The device of claim 2 , wherein at least one surface of each external thermally conductive layer comprises a treatment to increase emissivity thereof.
5. The device of claim 3 , wherein the vias are located adjacent the inner and outer diameter portions.
6. The device of claim 1 , further comprising heat sinks comprising thermally conductive material coupled adjacent at least one of the inner and outer diameter portions.
7. The device of claim 6 , wherein each heat sink comprises discrete heat sink segments.
8. The device of claim 6 , wherein each heat sink comprises fingers that extend from a plane of the heat sink.
9. The device of claim 8 , wherein some of the fingers are oriented at a first angle and other ones of the fingers are oriented at a second angle that differs from the first angle.
10. The device of claim 1 , further comprising an internal thermally conductive layer located inside the stator assembly.
11. The device of claim 10 , wherein the internal thermally conductive layer is thermally coupled to the external thermally conductive layer with vias.
12. The device of claim 11 , wherein the vias are located adjacent at least one of the inner and outer diameter portions.
13. The device of claim 10 , further comprising heat sinks comprising thermally conductive material coupled adjacent to at least one of the inner and outer diameter portions.
14. The device of claim 13 , wherein each heat sink comprises discrete heat sink segments.
15. The device of claim 14 , wherein each heat sink comprises fingers that extend from a plane of the heat sink.
16. The device of claim 15 , wherein some of the fingers are oriented at a first angle and other ones of the fingers are oriented at a second angle that differs from the first angle.
17. The device of claim 1 , further comprising a plurality of internal thermally conductive layers.
18. The device of claim 17 , wherein the internal thermally conductive layers are evenly spaced apart from each other.
19. The device of claim 17 , wherein the internal thermally conductive layers are unevenly spaced apart from each other.
20. The device of claim 1 , wherein the thermally conductive layers comprise radial thermal traces that are thermally coupled at ends thereof adjacent the outer diameter portion with a continuous thermal coupler.
21. The device of claim 20 , wherein the continuous thermal coupler comprises an internal continuous thermal coupler.
22. The device of claim 20 , wherein the continuous thermal coupler comprises an external continuous thermal coupler.
23. The device of claim 20 , wherein the continuous thermal coupler comprises internal and external continuous thermal couplers.
24. The device of claim 23 , wherein the internal and external continuous thermal couplers are thermally coupled together with vias that are thermally conductive.
25. The device of claim 20 , wherein the radial thermal traces comprise a linear pattern.
26. The device of claim 20 , wherein the radial thermal traces comprise a non-linear pattern.
27. The device of claim 20 , wherein the radial thermal traces comprise a serrated pattern.
28. The device of claim 20 , wherein the radial thermal traces comprise discontinuities that disrupt circulation of eddy currents.
29. The device of claim 28 , wherein the radial thermal traces are thermally coupled at ends thereof adjacent the inner diameter portion with a continuous thermal coupler.
30. The device of claim 29 , wherein the thermally conductive traces have a non-linear pattern.
31. The device of claim 29 , wherein the thermally conductive traces have a serrated pattern.
32. The device of claim 20 , where at least one pair of radial thermal traces is not connected to any thermal couplers, and the at least one pair of radial thermal traces is connected adjacent the inner diameter portion of the stator assembly and are further connected to a voltage sensor of a motor monitoring system.
33. The device of claim 2 , wherein the external thermally conductive layers are galvanically coupled to a machine housing of the device and configured to provide electrical grounding for the stator assembly.