Turbomachine with e-machine controller having cooled bus bar member
A turbomachine includes a rotating group with a wheel supported on a shaft. The turbomachine includes a housing that houses the wheel for rotation therein about an axis of rotation. The turbomachine includes an e-machine section with an e-machine operatively connected to the shaft and configured to convert energy between the e-machine and the shaft as the shaft rotates. Furthermore, the turbomachine includes a controller configured for control of the e-machine. The controller has a bus bar member that includes a bus bar that is partly covered over by an electrically-insulative covering member. The bus bar includes a thermal terminal surface that is exposed from the covering member. The controller includes a heat sink member, wherein the thermal terminal surface is thermally connected to the heat sink member with the heat sink member configured to receive heat from the bus bar member.
1. A turbomachine comprising:
a rotating group with a wheel supported on a shaft;
a housing that houses the wheel for rotation therein about an axis of rotation;
an e-machine section with an e-machine operatively connected to the shaft and configured to convert energy between the e-machine and the shaft as the shaft rotates; and
a controller configured for control of the e-machine, the controller including a bus bar member that includes a bus bar that is partly covered over by an electrically-insulative covering member, the covering member having a first side and a second side that faces opposite the first side, the bus bar including a thermal pad and an electrical connector that extends from the thermal pad and that projects from the first side, the thermal pad having a thermal terminal surface that is exposed from the second side of the covering member, the controller including a heat sink member facing the second side, the thermal terminal surface being thermally connected to the heat sink member with the heat sink member configured to receive heat from the bus bar member.
2. The turbomachine of claim 1 , wherein the thermal terminal surface includes a flat surface that overlies the heat sink member.
3. The turbomachine of claim 2 , wherein the electrically-insulative covering member includes a cover surface that is adjacent the flat surface and that is substantially flush therewith.
4. The turbomachine of claim 1 , further comprising a fluid cooling system for a flow of a fluid coolant proximate the heat sink member to remove heat from the heat sink member.
5. The turbomachine of claim 4 , wherein the heat sink member includes a heat sink first side that faces away from the thermal terminal surface and a heat sink second side that faces the thermal terminal surface; and
wherein the fluid cooling system includes a passage that defines a flow axis for a coolant, the flow axis directed across the heat sink first side.
6. The turbomachine of claim 1 , further comprising a biasing member configured to bias the bus bar member toward the heat sink member.
7. The turbomachine of claim 6 , wherein the biasing member is a spring fastener that abuts the covering member to bias the thermal terminal surface toward the heat sink member.
8. The turbomachine of claim 7 , wherein the covering member includes a recess that receives the spring fastener.
9. The turbomachine of claim 8 , wherein the recess includes a flat surface that defines the recess.
10. The turbomachine of claim 1 , wherein the bus bar includes a terminal end; and
wherein the terminal end is also exposed from the covering member.
11. The turbomachine of claim 10 , wherein the thermal terminal surface is substantially planar; and
wherein the terminal end is disposed in a plane that is substantially parallel to the thermal terminal surface.
12. The turbomachine of claim 1 , wherein the bus bar is a first bus bar of the bus bar member, the first bus bar including the thermal terminal surface that is a first thermal terminal surface of the bus bar member; and
wherein the bus bar member includes a second bus bar that is partly covered over by the covering member, the second bus bar including a second thermal terminal surface that is exposed from the covering member, the thermal terminal surface being thermally connected to the heat sink member with the heat sink member configured to receive heat from the bus bar member.
13. A method of manufacturing a turbomachine comprising:
supporting a wheel of a rotating group on a shaft;
housing the wheel in a housing for rotation therein about an axis of rotation;
providing an e-machine section with an e-machine operatively connected to the shaft and configured to convert energy between the e-machine and the shaft as the shaft rotates; and
supporting a controller on the turbomachine, the controller configured for control of the e-machine, the controller including a bus bar member that includes a bus bar that is partly covered over by an electrically-insulative covering member, the covering member having a first side and a second side that faces opposite the first side, the bus bar including a thermal pad and an electrical connector that extends from the thermal pad and that projects from the first side, the thermal pad having a thermal terminal surface that is exposed from the second side of the covering member, the controller including a heat sink member facing the second side, the thermal terminal surface being thermally connected to the heat sink member with the heat sink member configured to receive heat from the bus bar member.
14. The method of manufacturing the turbomachine of claim 13 , further comprising forming the bus bar member by overmolding the covering member on the bus bar.
15. The method of manufacturing of claim 13 , wherein the thermal terminal surface includes a flat surface that overlies the heat sink member.
16. The method of manufacturing of claim 15 , wherein the electrically-insulative covering member includes a cover surface that is adjacent the flat surface and that is substantially flush therewith.
17. The method of manufacturing of claim 13 , further comprising attaching a fluid cooling system for a flow of a fluid coolant proximate the heat sink member to remove heat from the heat sink member.
18. The method of manufacturing of claim 17 , wherein the heat sink member includes a heat sink first side that faces away from the thermal terminal surface and a heat sink second side that faces the thermal terminal surface and; and
wherein the fluid cooling system includes a passage that defines a flow axis for a coolant, the flow axis directed across the heat sink first side.
19. The method of manufacturing of claim 13 , further comprising attaching a biasing member to bias the bus bar member toward the heat sink member.
20. A turbomachine comprising:
a rotating group with a wheel supported on a shaft;
a housing that houses the wheel for rotation therein about an axis of rotation;
an e-machine section with an electric motor operatively connected to the shaft and configured to drive the shaft in rotation;
a controller configured for control of the electric motor, the controller including a printed circuit board (PCB) with a circuit element and a bus bar member that includes a plurality of bus bars that are partly covered over by an electrically-insulative covering member, the covering member having a first side and a second side that faces opposite the first side, the first side facing the PCB, the bus bars respectively including a thermal pad and a PCB connector that extends from the thermal pad and that projects from the first side to electrically connect to the circuit element, the thermal pad having a thermal terminal surface that is exposed from the second side of the covering member, the controller including a heat sink member, the second side facing the heat sink member, the thermal terminal surface being thermally connected to the heat sink member with the heat sink member configured to receive heat from the bus bar member; and
a fluid cooling system for a flow of a fluid coolant proximate the heat sink member to remove heat from the heat sink member.