Axial field rotary energy device having pcb stator and variable frequency drive

Abstract

An axial field rotary energy device or system includes an axis, a PCB stator and rotors having respective permanent magnets. The rotors rotate about the axis relative to the PCB stator. A variable frequency drive (VFD) having VFD components are coupled to the axial field rotary energy device. An enclosure contains the axial field rotary energy device and the VFD, such that the axial field rotary device and the VFD are integrated together within the enclosure. In addition, a cooling system is integrated with the enclosure to cool the axial field rotary energy device and the VFD.

What is claimed is: 
     
         1 . A system, comprising:
 an axial field rotary energy device having an axis, a printed circuit board (PCB) stator and rotors having respective permanent magnets (PM), and the rotors are configured to rotate about the axis relative to the PCB stator;   a variable frequency drive (VFD) comprising VFD components coupled to the axial field rotary energy device;   an enclosure containing the axial field rotary energy device and the VFD, such that the axial field rotary device and the VFD are integrated together within the enclosure; and   a cooling system integrated within the enclosure and configured to cool the axial field rotary energy device and the VFD.   
     
     
         2 . The system of  claim 1 , wherein the cooling system comprises an impeller configured to cool the system. 
     
     
         3 . The system of  claim 1 , wherein the enclosure comprises an axial length, a radial width relative to the axis that is greater than the axial length, and the enclosure is substantially rectangular in shape when viewed axially. 
     
     
         4 . The system of  claim 3 , wherein a ratio of the radial width to the axial length is in a range of about 2:1 to about 20:1, and the enclosure is substantially square in shape when viewed axially. 
     
     
         5 . The system of  claim 1 , wherein, relative to the axis, the VFD components are mounted around and substantially co-planar with the axial field rotary energy device. 
     
     
         6 . The system of  claim 1 , wherein the VFD components comprise a rectifier module, direct current (DC) bus, inverter module, control module and input/output (I/O) module. 
     
     
         7 . The system of  claim 6 , wherein the VFD components comprise line inductors. 
     
     
         8 . The system of  claim 6 , wherein the inverter module comprises wide band gap switching devices. 
     
     
         9 . The system of  claim 6 , wherein the rectifier module and DC bus comprise a first printed circuit board assembly (PCBA), the inverter module and control module comprise a second PCBA, the I/O module comprises a third PCBA. 
     
     
         10 . The system of  claim 9 , wherein the VFD components comprise line inductors as a separate assembly from the first, second and third PCBAs. 
     
     
         11 . The system of  claim 9 , wherein the I/O module comprises a daughter PCBA configured to perform customized communication functions, and the daughter PCBA is removably coupled to the third PCBA. 
     
     
         12 . The system of  claim 6 , wherein the rectifier module, DC bus, inverter module, and control module comprise a first printed circuit board assembly (PCBA), and the I/O module comprises a second PCBA. 
     
     
         13 . The system of  claim 12 , wherein the I/O module comprises a daughter PCBA configured to perform customized communication functions, and the daughter PCBA is removably coupled to the second PCBA. 
     
     
         14 . The system of  claim 6 , wherein the rectifier module, DC bus, inverter module, control module and I/O module comprise a common printed circuit board assembly (PCBA). 
     
     
         15 . The system of  claim 14 , wherein the I/O module comprises a daughter PCBA configured to perform customized communication functions, and the daughter PCBA is removably coupled to the common PCBA. 
     
     
         16 . The system of  claim 1 , wherein the enclosure comprises respective housings for the axial field rotary energy device and VFD. 
     
     
         17 . The system of  claim 16 , wherein the housings are substantially axially aligned and coupled to each other. 
     
     
         18 . The system of  claim 17 , wherein the housings are axially spaced apart by an axial space, a cooling device is located in the axial space, and the VFD housing comprises an access port configured to provide access to the VFD. 
     
     
         19 . The system of  claim 18 , wherein the cooling device comprises a first impeller located between the rotors and configured to circulate a first air flow within the housing for the axial field rotary energy device, and a second impeller located in the axial space between the housings and configured to circulate radial air flow into and out of the axial space adjacent the VFD. 
     
     
         20 . The system of  claim 18 , wherein each housing comprises fins extending into the axial space between the housings. 
     
     
         21 . The system of  claim 20 , wherein a cooling device comprises an impeller and a baffle configured to circulate an air flow that, relative to the axis, radially enters and exits the axial space between the housings. 
     
     
         22 . The system of  claim 20 , wherein the air baffle comprises an axial component that extends in an axial direction along and around an exterior of the enclosure to define axial air passages between the axial component and the enclosure, the air baffle also having a radial component that extends in a radial direction in the axial space between the housings to define radial air passages between the radial component and the housings. 
     
     
         23 . The system of  claim 22 , wherein the cooling device is configured to circulate air flow that radially enters a first set of the radial air passages, flows through a second set of radial air passages, and the air flow axially exits via the axial air passages. 
     
     
         24 . The system of  claim 22 , wherein the cooling device is configured to circulate air flow that axially enters the axial air passages, flows through all radial air passages, and the air flow radially exits the system. 
     
     
         25 . The system of  claim 22 , wherein the cooling device is configured to circulate air flow that axially enters a first set of the axial air passages, flows through the radial air passages, and the air flow axially exits a second set of axial air passages.