US20160123637A1

US20160123637A1 - Two-phase heat exchanger for cooling electrical components

Info

Publication number: US20160123637A1
Application number: US14/926,594
Authority: US
Inventors: Gilbert Moreno; Jana R. JEFFERS; Kevin Bennion; Charles King; Sreekant Narumanchi
Original assignee: Alliance for Sustainable Energy LLC
Current assignee: Alliance for Sustainable Energy LLC
Priority date: 2014-10-29
Filing date: 2015-10-29
Publication date: 2016-05-05

Abstract

Described herein are passive cooling systems utilizing two-phase heat-transfer fluids for transferring heat from one or more heat sources.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims priority to and the benefit of U.S. Provisional Application No. 62/069,983, filed on Oct. 29, 2014, entitled “Two-Phase Heat Exchanger for Power Electronics Cooling” and is herein incorporated by reference in its entirety.

CONTRACTUAL ORIGIN

The United States Government has rights in this invention under Contract No. DE-AC36-08GO28308 between the United States Department of Energy and the Alliance for Sustainable Energy, LLC, the Manager and Operator of the National Renewable Energy Laboratory.

BACKGROUND

The size, weight, and cost of power electronic components are factors that influence the cost of hybrid and electric vehicles. According to a report from the Oak Ridge National Laboratory (Energy and Environmental Analysis, Inc., 2007, “Technology and Cost of the MY2007 Toyota Camry HEV—Final Report,” Technical Report No. ORNL/TM-20071132), power electronics accounts for up to 40% of the total traction drive cost in hybrid vehicles. Increasing vehicle electrification, in an effort to reduce the nation's dependence on foreign oil, requires making electric drive vehicles cost competitive with conventional gasoline powered vehicles. For these reasons, the Department of Energy (DOE) has defined cost, power density, specific power, and efficiency technical targets aimed at decreasing the cost and increasing the efficiency of these components. According to the DOE, reaching these cost targets requires a 4.1-fold and 2.5-fold reduction to the cost of power electronics and electric motors, respectively. Additionally, the DOE has highlighted three strategies to enable reaching their technical targets: 1) fully integrated components (i.e., integrating the power electronics with the motor), 2) using wide-bandgap (WBG) semiconductors, and 3) using non-rare earth element motors. One means of reducing the cost of hybrid and electric vehicles is through reduced cost, weight, and size of automotive power electronics.
However, heat dissipation is a limiting factor in reducing the size and cost of the power electronic devices. Current power electronic semiconductor devices are sized larger to spread heat and thus allow for reliable operation. Significant cost reductions can be achieved by decreasing the size of these semiconductor electronic devices. Increasing the heat dissipation through the use of highly efficient cooling schemes allows for greater power density (heat per volume), which in turn reduces the size, weight, and cost of power electronics.
It is estimated that almost 6 million hybrid electric vehicles (HEV) have been sold worldwide and their sales are expected to grow in future years. This increasing trend towards vehicle electrification has also increased the demands for plug-in hybrid electric (PHEVs) and electric vehicles (EVs). All electric vehicles (e.g., HEV, PHEV, and EV) require power electronic systems and thus could benefit from improved cooling technology methods and systems. Two-phase cooling offers some of the highest heat-transfer rates, higher than those possible with conventional, single-phase liquid cooling systems typical of automotive heat exchangers. Although some researchers have developed two-phase cooling systems for automotive electronics (see U.S. Pat. No. 6,993,924 and U.S. Patent Application Publication No. 2012/0267077), none of these concepts are currently used in automotive power electronics cooling systems. Thus, there remains a need for improved two-phase cooling system designs that can meet technical requirements, while also reducing cost, to enable electric vehicles a more effective entry into current automotive markets.

SUMMARY

An aspect of the present invention is an evaporator having a first wall, where the first wall has an external surface, a first edge, and a second edge. The first wall, the first edge, and the second edge are substantially parallel to a plane, and the first edge and the second edge are substantially parallel to each other. The evaporator also has a second wall extending from the first edge and the external surface, and the second wall is substantially perpendicular to the plane, and substantially parallel to the first edge. The evaporator also has a third wall extending from the second edge and the external surface, and the third wall is substantially perpendicular to the plane, and substantially parallel to the second edge. The external surface of the first wall, the second wall, and the third wall form a passage substantially parallel to the first edge. The passage is configured to contain at least one heat source, and at least the first wall is configured to be in thermal communication with the at least one heat source.
In some embodiments of the present invention, the evaporator may have a conducting element, where the conducting element is positioned within the passage. The conducting element is configured to be in thermal communication with the at least one heat source, and the conducting element is in thermal communication with at least one of the second wall or the third wall. In some embodiments of the present invention, a conducting element may be a block of material with a substantially triangular cross-section, where the block of material has a first side that is in thermal communication with either the second wall or the third wall, and the block has a second side that is configured to be in thermal communication with the at least one heat source.
In some embodiments of the present invention, a conducting element may include a first block of material with a substantially triangular cross-section, and a second block of material with a substantially triangular cross-section. The first block of material may have a first side that is in thermal communication with the second wall, and a second side that is configured to be in thermal communication with the at least one heat source. The second block of material may have a first side that is in thermal communication with the third wall, and a second side that is configured to be in thermal communication with the at least one heat source.
In some embodiments of the present invention, a first wall of an evaporator may have an internal surface with a surface area extender extending from the internal surface. The internal surface may be substantially parallel to the external surface, and the surface area extender may be substantially perpendicular to the plane. In some embodiments of the present invention, a surface area extender may be a fin, where the fin is substantially parallel to the first edge. In some embodiments of the present invention, the internal surface and the external surface may define a width of the first wall, where the fin may be at a height that is approximately equal to the width.
In some embodiments of the present invention, the second wall may terminate with an edge, the third wall may terminate with an edge, and the edge of the second wall and the edge of the third wall may be positioned below the external surface. The evaporator may also include a first tab extending from the edge of the second wall, where the first tab is substantially perpendicular to the second wall, and extends away from the passage. The evaporator may also include a second tab extending from the edge of the third wall, where the second tab is substantially perpendicular to the third wall, and extends away from the passage.
In some embodiments of the present invention, an evaporator may have a housing where the housing has a first end connected to the first tab, a second end connected to the second tab, and at least one wall physically connecting the first end to the second end. The housing may form a first interior channel between the interior surface of the first wall and the housing. The housing may form a second interior channel between the second wall and the housing, and the housing may form a third channel between the third wall and the housing. In some embodiments of an evaporator, the first wall, the second wall, the third wall, the first tab, the second tab, and the housing may be a single piece of material. A single piece of material may be aluminum.
In some embodiments of the present invention, the first wall, the second wall, the third wall, the first tab, and the second tab of an evaporator may all be a first single piece of material. The first single piece of material may be aluminum. The housing may be a second single piece of material. The second single piece of material may be copper.
A further aspect of the present invention is a cooling system having an evaporator configured to cool a first heat source, a condenser in fluid communication with the evaporator, a refrigerant contained within the condenser and the evaporator, and a circulating liquid system. The circulating liquid system may include a liquid contained within the circulating liquid system, a liquid reservoir, a pump in liquid communication with the liquid reservoir, and a first heat exchanger in liquid communication with the pump, where the first heat exchanger is configured to deliver heat from the liquid to the refrigerant. The circulating liquid system may also include a second heat exchanger in liquid communication with the first heat exchanger. The second heat exchanger may be configured to deliver heat from a second heat source to the liquid, and the second heat exchanger may be in liquid communication with the liquid reservoir. The pump may circulate the liquid through the first heat exchanger, the second heat exchanger, and the liquid reservoir.
In some embodiments of the present invention, the second heat exchanger may have a spray nozzle, such that the liquid may be sprayed onto the second heat source. The liquid reservoir may have a liquid collection pan configured to collect oil heated by the second heat source. In some further embodiments of the present invention, the evaporator and the circulating liquid system may be fluid-sealed within a container operating at a first average temperature. In still further embodiments, the condenser may operate at a second average temperature that is less than the first average temperature.

BRIEF DESCRIPTION OF THE DRAWINGS

Exemplary embodiments are illustrated in referenced figures of the drawings. It is intended that the embodiments and figures disclosed herein are to be considered illustrative rather than limiting.

FIG. 1 illustrates a cooling system for removing heat from one or more heat sources, for example power electronics, according to exemplary embodiments of the present invention.

FIGS. 2a and 2b illustrate evaporators for removing heat from one or more heat sources, for example a power electronics module, according to exemplary embodiments of the present invention.

FIGS. 3a and 3b illustrate evaporators for removing heat from one or more heat sources, for example power electronics modules, according to exemplary embodiments of the present invention.

FIG. 4 illustrates an evaporator for removing heat from one or more heat sources, for example a power electronic module, according to exemplary embodiments of the present invention.

FIG. 5 illustrates an evaporator for removing heat from two or more heat sources where the evaporator includes multiple parallel internal channels, and constructed from more than one single piece of material joined together, according to exemplary embodiments of the present invention.

FIG. 6 illustrates an evaporator having two external passages configured to receive six heat-generating elements, according to exemplary embodiments of the present invention.

FIG. 7 illustrates a system for simultaneously removing heat from two different heat sources, for example a power electronics module and a motor, according to exemplary embodiments of the present invention.

FIG. 8 illustrates a system for simultaneously removing heat from two different heat sources, for example a power electronics module and a motor, utilizing recirculating cooling oil, where the oil is sprayed onto the motor, according to exemplary embodiments of the present invention.

FIGS. 9a and 9b illustrate systems for simultaneously removing heat from both power electronics and a motor, utilizing a recirculating cooling oil loop, according to exemplary embodiments of the present invention.

FIG. 10 illustrates a system for simultaneously removing heat from both power electronics and a motor, utilizing a recirculating cooling oil system, according to exemplary embodiments of the present invention.

FIG. 11 illustrates a schematic of a passive, two-phase cooling system, according to exemplary embodiments of the present invention.

FIG. 12 illustrates images of a finned-tube condenser (top left), a rifled tube condenser (top right), and a louvered-fin condenser (bottom), according to exemplary embodiments of the present invention.

FIG. 13 illustrates a cross-sectional view of an evaporator incorporating an interchangeable cold plate design, according to exemplary embodiments of the present invention.

FIG. 14 illustrates experimental data for thermal resistances to heat flow versus heat dissipated for two refrigerants for an evaporator.

FIG. 15 illustrates mechanical drawings of two evaporators for cooling one or more heating sources, according to exemplary embodiments of the present invention.

FIG. 16 illustrates experimental data of thermal resistances to heat flow versus heat dissipated for two evaporators.

FIG. 17 illustrates estimates of condenser sizing requirements for various two-phase heat-transfer fluid operating temperatures, according to exemplary embodiments of the present invention.

REFERENCE NUMBERS

100 . . . cooling system
110 . . . evaporator
120 . . . condenser
130 . . . heat source
140 . . . vapor/condensate line
150 . . . manifold
160 . . . tube
170 . . . bend
180 . . . fins
200 . . . housing
210 . . . main channel
220 . . . first wall
230 . . . surface area extender
300 . . . first side channel
305 . . . second side channel
310 . . . passage
320 . . . second wall
325 . . . third wall
330 . . . first tab
335 . . . second tab
340 . . . first edge
345 . . . second edge
347 . . . connecting tab
350 . . . shared side channel
400 . . . first conducting element
410 . . . second conducting element
500 . . . spanning wall
510 . . . first side wall
515 . . . second side wall
520 . . . dividing wall
530 . . . insert
700 . . . power electronics module
705 . . . cooling fluid
710 . . . first heat exchanger
720 . . . first return line
730 . . . motor
740 . . . second heat exchanger
750 . . . second return line
760 . . . liquid reservoir
770 . . . first supply line
780 . . . pump
790 . . . second supply line
800 . . . refrigerant
802 . . . outside environment
805 . . . containment system
807 . . . evaporator reservoir
810 . . . refrigerant vapor
820 . . . refrigerant condensate
830 . . . first surface area extenders
840 . . . second surface are extenders
845 . . . oil
850 . . . oil spray
860 . . . heated oil
870 . . . oil collection pan
880 . . . third supply line
890 . . . spray nozzle

DETAILED DESCRIPTION OF SOME EMBODIMENTS

The present disclosure may address one or more of the problems and deficiencies of the prior art discussed above. However, it is contemplated that some embodiments as disclosed herein may prove useful in addressing other problems and deficiencies in a number of technical areas. Therefore, the embodiments described herein should not necessarily be construed as limited to addressing any of the particular problems or deficiencies discussed herein.
The methods and systems described herein utilize a two-phase cooling strategy with other unique features (e.g. dual-side cooling, increased heat spreading, and extrudable fabrication design) that have the potential to significantly increase power densities and thus reduce the size and cost of power electronics. The high heat-transfer capacity and isothermal characteristics of two-phase heat-transfer enables the cooling systems described herein to outperform conventional automotive cooling systems that employ single-phase liquid cooled heat exchangers. This has been demonstrated through a combination of experimental work and modeling analysis. The two-phase cooling concepts described herein utilize a passive cooling approach (e.g. no pumping or compression of the two-phase heat-transfer fluid contained within the condenser and the evaporator) and an evaporator design that increases heat dissipation, reliability, and efficiency, resulting in reduced cooling system size and/or weight. The increased heat dissipation provided by the two-phase based cooling system has the potential to increase power density and reliability. Increasing the power density and reliability of automotive power electronics are paths to reducing the cost of electric-drive vehicles (e.g., hybrids, plug-in hybrids, all electric, and fuel cell).
The cooling systems described herein utilize a two-phase heat-transfer fluid cooling system. The term “two-phase heat-transfer fluid” refers to a fluid that is reversibly cycled between the fluid's liquid phase and vapor phase. By utilizing a two-phase heat-transfer fluid within a cooling system having an evaporator and a condenser, heat may be removed from a heat-generating element (e.g. power electronics) by vaporizing the heat-transfer fluid in the evaporator and subsequently condensing the fluid in the condenser. Since this process utilizes the latent heat of vaporization of the two-phase heat-transfer fluid, such a system can be very efficient in terms of energy removed from the heat-generating element per unit mass of heat-transfer fluid utilized, and in terms of energy removed per unit surface area of the evaporator and/or condenser. Examples of two-phase heat-transfer fluids that may be used in cooling systems described herein include various refrigerants/coolants including but not limited to R-134a, R-1234yf, R-245fa, HFE-7000, HFE-7100, Novec 649, and/or any other suitable fluid capable of reversibly vaporizing and condensing.
FIG. 1 illustrates an exemplary cooling system 100 that includes an evaporator 110 and a condenser 120, connected by two vapor/condensate lines 140, and configured to cool a plurality of heat sources 130 (e.g. electronics). In this example, the condenser 120 is constructed using multiple tubes 160, with each tube oriented in a substantially vertical position (e.g. along the y-axis and relative to the XZ-plane). However, the vertical position is for illustrative purposes, and other examples of cooling systems may position condenser tubes at an angle other than 90 degrees from horizontal (where horizontal corresponds to the XZ-plane in FIG. 1). For example, a condenser may be provided with tubes at an angle of about 45 degrees to about 90 degrees, relative to horizontal. In other embodiments, a two-phase evaporative cooling system may have a condenser that is slanted to reduce the height of the system while increasing the frontal condenser area. This exemplary design may also induce liquid flow to the evaporator during time of need, for example, during high acceleration situations and/or during hill-climbing. Each tube 160 may be a hollow tube, pipe, duct and/or any other conduit suitable for transferring vapor and/or liquid through a hollow, internal portion of the conduit. For example, a condenser may include one or more substantially parallel conduits, where each conduit has at least one outside wall defining a closed, cross-sectional shape including a circle, an ellipse, a square, a rectangle, and/or any other suitable cross-sectional shape configured to contain and/or transfer vapor and liquid within the conduit.
FIG. 1 illustrates that a first end of teach tube 160 may begin at a common manifold 150, with a hollow, internal portion that runs the length of the manifold 150, so that the manifold 150 disperses vapor flowing from the evaporator 110 through all or most of the tubes 160 of the condenser 120. A manifold 150 may be utilized to maximize vapor distribution across all of the tubes 160 to increase the surface area available for condensing vapor within the condenser 120. FIG. 1 shows each tube 160 terminating with a second end that is physically attached to a bend 170 that connects each tube 160 to an adjacent tube 160. Thus, the condenser 120 pictured in FIG. 1 has multiple tubes 160, where each tube 160 is in fluid communication with a manifold 150, and pairs of tubes are joined and in fluid communication at a high point (e.g. along the y-axis) by a bend 170.
FIG. 1 illustrates a condenser 120 that utilizes bends 170 to connect neighboring tubes 160 to one another. Alternatively, the tubes 160 of a condenser may terminate at a second common manifold. Or each tube 160 may terminate with a plug or cap. In other cases, the bends 170 may be solid bends (versus hollow) to provide structural support only, and which do not allow fluid communication between neighboring tubes 160. In still other embodiments, each tube 160 may terminate with a capping block that is common to all of the tubes 160.
FIG. 1 illustrates that each tube 160 may be positioned with a space or gap between itself and its neighboring tubes 160. In some cases, spaces (or gaps) may be provided between neighboring tubes 160 of a condenser 120 to enable a cooling fluid to flow between the tubes 160; e.g. natural or forced convective flow. In same examples, the cooling fluid used may be air and/or any other suitable gas. Spaces between the tubes 160 may increase the surface area available for heat-transfer and/or help maximize the fluid velocity, which in turn, may increase the heat-transfer rate achievable by the condenser, resulting in more efficient heat-transfer, condensation, and allow for smaller condenser sizes. In addition, the outside surface area available by a condenser 120 for contact with a cooling fluid may be increased by the use of fins 180. Gaps are provided between neighboring fins 180, so as to provide a flow path for a cooling fluid to pass over and between the fins.
In still other examples, a condenser for a cooling system may include any suitable heat-exchanger configured to be cooled by an external cooling fluid flowing over one or more outside surfaces of the condenser. For example, condenser types include brazed folded-fin, finned-tube, flat plate, shell and tube, dimpled, and/or any other suitable heat exchanger. However, all of these condenser examples are provided for illustrative purposes and the specific design of a condenser will be determined by the specific application and environment.
FIG. 1 illustrates two vapor/condensate lines 140 physically connecting the evaporator 110 and the condenser 120. Again, this is for illustrative purposes, for example when the condenser 120 and the evaporator 110 are provided as separate units, which are installed in different locations within a vehicle. In this case, one or more vapor/condensate lines 140 may be used to provide a fluid path for the two-phase heat-transfer fluid between the condenser 120 and the evaporator 110. A vapor/condensate line 140 may be a cylindrical pipe or tube and/or any other conduit suitable for transferring vapor and/or condensate between the condenser 120 and the evaporator 110. To minimize pressure drops and/or liquid entrainment by the vapor produced in the evaporator 110, a plurality of vapor/condensate lines 140 may be utilized to increase the total open surface area available for vapor and/or condensate flow between the condenser 120 and evaporator 110 (e.g. to lower the fluid velocity through the vapor/condensate line 140.) However, in other applications, a single vapor/condensate line 140 may connect the condenser 120 and the evaporator. For example a single vapor/condensate line 140 may have essentially the same length (z-axis) and width (x-axis) as the condenser 120 and/or the evaporator 110, and have a height (y-axis) necessary to link the condenser 120 to the evaporator 110. FIG. 1 illustrates the vapor/condensate lines 140 as straight, vertical conduits. However, this is not intended to be limiting, and a vapor/condensate line 140 may include one or more bends or turns, as needed, for a specific vehicle's configuration and/or space limitations. FIG. 1 illustrates an example where the condenser 120 is positioned above (in the y-axis direction) the evaporator 130. Other embodiments of cooling systems may reverse the position where the condenser 120 is positioned below the evaporator 110 or at substantially the same height. In some cases, a wicking material may be provided to assist with the transfer of condensate from the condenser 120 to a higher-positioned evaporator 110.
The evaporators shown in FIGS. 2a and 2b may be visualized as cross-sectional views, in the XY-plane, of the evaporator 110 shown in FIG. 1. FIG. 2a illustrates an embodiment of an evaporator 110, which includes a housing 200 defining an internal channel, referred to herein as a main channel 210. This exemplary evaporator 110 has a rectangular cross-section with two relatively long, horizontal walls (along the x-axis) and two shorter vertical walls (along the y-axis). Each wall has an internal surface facing the main channel 210 and an external surface facing the outside environment of the evaporator 110. Thus, each wall has a thickness defined by its respective internal surface and external surface. For example, depending on the system's operating pressure, a wall thickness may be about 1 mm to about 10 mm. Both FIGS. 2a and 2b show a heat source 130 in thermal communication with a first wall 220. The term “thermal communication” is used to indicate that the heat source 130 and the first wall 220 may exchange heat between each other and are not necessarily in direct physical contact with each other. For example, there may be an intervening layer positioned between the heat source 130 and the first wall 220, for example a thermal grease, a thermal interface material, a bonding interface material, an adhesive, and/or any other suitable material to facilitate contacting the heat source 130 to the evaporator housing 200. Examples of bonding interface materials that may be placed between the heat source 130 and the first wall 220 of the housing 200 of the evaporator 110 include thermoplastics, solder, brazing, and/or sintered silver. In other cases, there may be no intervening layer positioned between the heat source 130 and the first wall 220, and the heat source 130 may be in direct contact and thermal communication with the first wall 220 of the evaporator 110. Heat-transfer between the heat source 130 and the first wall 220 may occur by conductive and/or radiant heat-transfer.
A condenser 120 for a cooling system 100 may either be cooled using air forced convection cooling (i.e., fan), liquid cooling, or natural convection cooling. In a liquid cooling configuration, the heat absorbed by the two-phase heat-transfer fluid may be utilized to provide heating to the cabin of a vehicle during cold environmental conditions. This configuration may be more suited to electric vehicles where there is no combustion engine to provide the heating capacity. In some embodiments of a natural cooling configuration, the condenser fins 180 may be integrated into the transmission/transaxle body to make use of the larger surface areas of the transmission/transaxle.
FIGS. 2a and 2b illustrate the first wall 220 as being a longer, horizontal wall (relative to the vertical wall). However, this is for illustrative purposes only. The heat source 130 may alternatively be placed along a shorter, vertical wall. In addition, the housing 200 is not limited to rectangular cross-sectional shapes. Any other suitable cross-sectional shape may be utilized, depending on the application, and includes square, triangular, hexagonal, circular, elliptical, and/or any other suitable cross-sectional shape. FIGS. 2a and 2b also illustrate a single heat source 130 associated with an evaporator 110. However, an evaporator 110 may be in thermal communication with and cool one or more heat sources 130, and multiple heat sources 130 may be in thermal communication with more than wall of the evaporator 110. For example, multiple heat sources 130 may be placed in thermal communication and/or physical contact with substantially all or most of the outer periphery of the housing 200 of an evaporator 110.
Comparing FIGS. 2a and 2b , FIG. 2b illustrates a vapor/condensate line 140, for connecting the evaporator 110 to a condenser (not shown). Thus, the example of FIG. 2b may include two additional walls (not shown), one at each end of the evaporator 110 along the z-axis to provide a fluid seal. FIG. 2a does not illustrate a vapor/condensate line 140, although one could be included, as shown in FIG. 2b . FIG. 2a illustrates an evaporator 110 where the main channel 210 is the conduit for transferring vapor and condensate between the evaporator 110 and the condenser (not shown). This concept will be described in more detail when describing FIG. 8 below. FIG. 2b also illustrates that the inside surface of the first wall 220 may include one or more surface area extenders 230. Surface area extenders 230 increase the surface area available for heat-transfer from the heat source 130, through the first wall 200, to the two-phase heat-transfer fluid (not shown) contained within the evaporator 110. Increasing the surface area of the internal surface of the first wall 220 may increase the heat-transfer rate achievable by the evaporator 110, and thus, reduce the evaporator's size and/or cost. The surface area extenders 230 of FIG. 2b are shown as relatively short, rectangular blocks of material positioned substantially parallel to the long-axis (z-axis) of the evaporator 110. In addition, the surface area extenders 230 of FIG. 2b are shown as having heights (y-axis) and widths (x-axis) that are relatively equal. However, these characteristics are not intended to be limiting. For example, the height to width ratio of a surface area extender 230 may be about 0.1 to about 10. In other examples, the height to width ratio of a surface area extender 230 may be about 0.5 to about 5. In other examples, a surface area extender 230 may take a different shape. For example, a surface area extender 230 may have a rounded surface at its apex (see FIG. 3a ) versus the sharp-corned, squared apex as shown in FIG. 2b . Or a surface area extender 230 may be positioned parallel to a different axis, for example, parallel to the x-axis (the shorter axis) instead of the y-axis (the longer axis) as shown in FIG. 2b . In yet other cases, a plurality of surface area extenders may be provided that are aligned along two or more axes such that the surface area extenders intersect each other; e.g. in a cross-hatch pattern. In still other cases, a surface area extender 230 may be substantially the same dimension in all or most directions in the XZ-plane. For example, instead of being longer in the z-axis direction and relatively short in the x-axis direction (e.g. rectangular strips) as shown in FIG. 2b , a surface area extender 230 may be in a shape that is substantially equal in length in the x-axis direction, the z-axis direction, and all or most other directions in the XZ-plane. Examples of such an embodiment include a surface area extender 230 in the shape of a bump, wedge, pyramid, knob, cylinder, cone, and/or any other suitable 3-dimensional shape extending from the internal surface of the first wall 220 into the main channel 210 of the housing 200 of the evaporator 110.
FIGS. 2a and 2b illustrate a housing 200 constructed of a single piece of material. This is for illustrative purposes only, and in some cases, a housing 200 may be constructed from more than one piece of material that are joined together such that the connecting points of the various pieces make a fluid seal; e.g. welded, soldered, glued, etc. This concept will be discussed in more detail when describing FIG. 5. However, FIGS. 2a and 2b illustrate an evaporator 110 where the housing 200 is constructed from a single piece of material made, for example, by an extrusion process. The evaporator 110 may also be fabricated through a machining or casting process or by using 3D printing technology. Examples of suitable materials for the housing 200 include aluminum, aluminum alloys, and/or copper.
FIG. 3a illustrates another embodiment of an evaporator 110 for a cooling system. A heat source 130 is in thermal communication with the external surface of a first wall 220 and the first wall 220 has an internal surface facing a main channel 210 of an evaporator 110. In addition, as in previous examples, a plurality of surface area extenders 230, in the form of rounded projections extend from the internal surface of the first wall 220 into the main channel 210. However, in this example, the first wall 220 does not take the shortest path, in the x-axis direction, to intersect with the vertical walls (in the y-axis direction) of the housing 200. Instead, the first wall 220 terminates at a first edge 340 and a second edge 345 before intersecting/contacting the vertical side walls of the housing 200. Both the first edge 340 and the second edge 345 are positioned substantially parallel to the long-axis (z-axis) of the housing 200 of the evaporator 110. Thus, FIG. 3a illustrates a first wall 220 that is not in direct physical contact with the vertical side walls of the housing 200. Instead, the first wall 220 is joined to the housing 200 indirectly, first by a downward and outward extending second wall 320 that begins at, and is joined to, the first edge 340 of the first wall 220, and a first tab 330 that extends horizontally from the second wall 320 to intersect with the housing 200. Thus, the second wall 320 and the first tab 330 complete one connection from the first wall 220 to the housing 200 (in this example on the left side of FIG. 3a ). A complementary set of elements is also provided for connecting the first wall 220 to the housing 200 to provide an evaporator 110 this is fluid-sealed from the outside environment. Thus, the first wall 220 is also connected to the housing 200 by a third wall 325 that begins at, and is joined to, the second edge 345 of the first wall 220, and a second tab 335 that begins at, and is joined to, the third wall 325 that extends horizontally from the third wall 325 to intersect with the opposite side of the housing 200 (in this case on the right side of FIG. 3a ).
Referring again to FIG. 3a , the second wall and the third wall (320 and 325), the pair of tabs (330 and 335) and the housing 200 together form a pair of side channels (300 and 305) that are positioned on either side (either edge 340 and 345) of the first wall 220. The side channels (300 and 305) also extend below the main channel 210 and the internal surface of the first wall 220. Thus, the side channels (300 and 305) and the second and third walls (320 and 325) extend the surface area available for heat-transfer from the heat source 130 to the two-phase heat-transfer fluid (not shown) contained within the evaporator 110. The evaporator 110 embodiments illustrated in FIGS. 3a and 3b provide additional pathways for heat removal from the heat source 130 to the two-phase heat-transfer fluid (not shown) contained within both the main channel 210 and the side channels (300 and 305). In other words, in addition to transferring heat from the heat source 130 through the first wall 220 to the two-phase heat-transfer fluid (not shown), heat may also be transferred from the heat source 130, through the second and third walls (320 and 325) to the two-phase heat-transfer fluid contained in both of the side channels (300 and 305). A “main channel” may also be referred to herein as a “first channel”. A “first side channel” may also be referred to herein as a “second channel”. A “second side channel” may also be referred to herein as a “third channel”.
Referring again to FIG. 3a , the first wall 220, the second wall 320, and the third wall 325 also define the boundaries of a passage 310 positioned on the exterior of the housing 200 of the evaporator 110. This passage 310 provides a space in which one or more heat sources 130 may be positioned. In the example of FIG. 3a , the width (in the x-axis direction) of the heat source 130 is about the same, or slightly smaller, than the width of the passage 310. By setting these widths to about the same amount insures that the lateral edges of the heat source 130 (left and right edges of FIG. 3a ) are in thermal communication, and possibly in direct physical contact, with the second wall 320 and third wall 325 of the evaporator 110. Gaps (e.g. air gaps) between the lateral edges of the heat source 130 and the second wall 320 and/or third wall 325 may increase the thermal resistances between these elements and, as a consequence, reduce the potential heat-transfer benefits of the side channels (300 and 305) and the second wall 320 and third wall 325. Thus, in some cases, the lateral edges of the heat source 130 may be in direct physical contact (and thermal communication) with the second wall 320 and the third wall 325. In other cases, the lateral edges of the heat source 130 may be in thermal communication, where conductive heat-transfer is increased through the use of a material positioned between the lateral edges of the heat source 130 and the second wall 320 and third wall 325. For example, there may be an intervening layer positioned between the lateral edges of the heat source 130 and the second wall 320 and third wall 325, for example a thermal grease, a thermal interface material, a bonding material, an adhesive, and/or any other suitable material to help facilitate contacting the heat source 130 to the second wall 320 and third wall 325. Other examples of materials that may be placed between a heat source 130 and the second wall 320 and third wall 325 of an evaporator 110 include thermoplastics, solder, and/or sintered silver. In still other examples, a small gap may be provided between the second wall 320 and the lateral edge of a heat source 130 and/or between the third wall 325 and the lateral edge of a heat source 130 to allow for thermal expansion/contraction of the cooling system 100 components.
FIG. 3b illustrates another exemplary embodiment of an evaporator 110. In this example, the evaporator 110 has a housing 200 with a substantially cylindrical shape and substantially circular cross-section and two passages (310 a and 310 b) for placing a plurality of heat sources (130 a and 130 b). A vapor-condensate line 140 is also provided so that vapor and condensate may flow between the evaporator 110 and the condenser (not shown). The two passages (310 a and 310 b) are aligned substantially parallel to one another and aligned with each other along the long axis (z-axis) of the cylindrical housing 200. Both passages (310 a and 310 b) are configured to contain at least one heat source (130 a and 130 b). Heat source 130 a is in thermal communication with a first wall 220 a, a second wall 320 a, and a third wall 325 a such that heat is removed from heat source 130 a through at least one of the walls, and transferred to the two-phase heat-transfer fluid contained within the evaporator 110. Similarly, heat source 130 b is in thermal communication with a first wall 220 b, a second wall 320 b, and a third wall 325 b such that heat is removed from heat source 130 b through at least one of the three walls, and transferred to the two-phase heat-transfer fluid contained within the evaporator 110. Further, the housing 200, first tab 330 a, and second wall 320 a form the boundaries of first side channel 300 a. In addition, the housing 200, first tab 330 b, and second wall 320 b form the boundaries of first side channel 300 b. In addition, both heat sources (130 a and 130 b) may transfer heat through their respective third side walls (325 a and 325 b) to a shared side channel 350, whose boundaries are defined by the third side walls (325 a and 325 b) and connecting tab 347.
Thus, heat-transfer in the evaporator 110 of FIG. 3b may occur from the heat sources (130 a and 130 b) through their respective first walls (220 a and 220 b) to the two-phase heat-transfer fluid contained in the main channel 210, and also through each heat source's respective second wall (320 a and 320 b) and third wall (325 a and 325 b) to the two-phase heat-transfer fluid contained within their corresponding first side channel (300 a and 300 b) and the shared side channel 350. FIG. 3b also illustrates a plurality of surface area extenders 230 projecting vertically from the first walls (220 a and 220 b) and projecting horizontally from the second walls (320 a and 320 b) and the third walls (325 a and 325 b) into the side channels (300 a, 300 b, and 350).
Referring again to FIG. 3b , the lower portion (in the y-axis direction) of the housing begins (starting at the left) with a first tab 330 a horizontally connected to the housing 200 and a second wall 320 a. The second wall 320 a extends vertically and connects with a first edge of a horizontally oriented first wall 220 a. The first wall 220 a extends horizontally to terminate at a second edge from which a third wall 325 a extends downward and vertically to terminate at a horizontally oriented connecting tab 347. The connecting tab 347 connects the third wall 325 a to the third wall 325 b. Third wall 325 b extends vertically and connects at a second edge of first wall 220 b, which extends horizontally to terminate at a second edge. Second wall 320 b then extends vertically and downward from the second edge to connect with first tab 330 b, which extends in the horizontal direction to connect with the housing 200. All of these elements are shown in FIG. 3b as being constructed from a single piece of material, including the housing 200. This may be achieved by forming the evaporator 110 using an extrusion process utilizing materials such as copper, aluminum, and/or aluminum alloys. Alternatively two or more of the elements shown in FIG. 3b may be manufactured as individual pieces, which are subsequently joined together; e.g. welded, soldered, glued, etc.
FIGS. 3a and 3b illustrate embodiments that have one and two passages 310 respectively. Other embodiments may have more than two substantially parallel passages, for example 3, 4, 5, 6, 7, 8, 9, or 10 passages, to provide additional space for a greater number of heat sources, or to provide space for physically larger heat sources. Further, the embodiment of FIG. 3b may include caps or plugs positioned at the ends of the evaporator 110 (in the z-axis direction) so as to seal the evaporator 110 from the external environment.
FIG. 4 illustrates another element of a cooling system to further increase the heat-transfer capabilities of a cooling system: conducting elements (400 and 410). As in previous figures, the exemplary embodiment of FIG. 4 shows an evaporator 110 with a housing 200 with external walls that define a main channel 210, a first side channel 300, and a second side channel 305. The first side channel 300 is defined by the housing 200, a first tab 330, and a second wall 320. The second side channel 305 is defined by the housing 200, a second tab 335, and a third wall 325. A first wall 220 is positioned between the second wall 320 and the third wall 325 at connecting edges 340 and 345, respectively. Thus, heat generated by the heat source 130 may be transferred through three separate contact surfaces to the two-phase heat-transfer fluid: the first wall 220, the second wall 320, and the third wall 325. However, as in previous examples, the heat source 130 of FIG. 4 has a relatively large width in the x-axis direction and relatively short thickness in the y-axis direction. Thus, more surface area (per unit length in the z-axis direction) is available for heat-transfer through the first wall 220 of the evaporator 110, and significantly less surface area (per unit length in the z-axis direction) is available through the remaining two pathways: through the second wall 320 and the third wall 325.
However, placement of one or more conducting elements, two in this case (a first conducting element 400 and a second conducting element 410) takes advantage of a fourth remaining surface of the heat source 130, the downward facing surface of the heat source 130 (in the XZ-plane). In the example of FIG. 4, the first conducting element 400 and the second conducting element 410 are positioned within the passage 310 such that the heat source 130 is positioned between the external surface of the first wall 220 and the conducting elements (400 and 410). The first conducting element 400 and the second conducting element 410 may be in direct physical contact with the lower surface of the heat source 130. Alternatively, the first conducting element 400 and the second conducting element 410 may be in thermal communication with the heat source 130, where another material is placed between the conducting elements (400 and 410) and the lower surface of the heat source 130. For example, a thermal grease, a thermal interface material, a bonding interface material, an adhesive, and/or any other suitable material to facilitate contacting the heat source 130 to the first conducting element 400 and the second conducting element 410 may be used. Examples of bonded interface materials that may be placed between the heat source 130 and the conducting elements (400 and 410) include thermoplastics, solder, and/or sintered silver.
The first conducting element 400 and the second conducting element 410 of FIG. 4 are illustrated as opposing triangular wedges. However, alternative embodiments could utilize one or more conducting wedges positioned within the passage 310. For the case of a single conducting element, the conducting element could be sized to substantially fill the passage 310. Generally, it is desirable to maximize the amount of surface area of the heat source 130 that is in thermal communication and/or in direct physical contact with the adjacent surface(s) of the conducting element(s) (400 and 410). Therefore, in some embodiments, the exposed surface area (in the XZ-plane) of the heat source 130 and the adjacent surface area (in the XZ-plane) of a conducting element may be substantially equal. In addition, it is generally desirable to maximize the amount of surface area (in the YZ-plane) of the external surfaces of the second wall 320 and the third wall 325 that is available for heat transfer from the heat source 130. Thus, triangularly-shaped conducting elements (400 and 410) achieve both of these criteria, while also reducing the amount of material used to construct the conducting elements (400 and 410). Such a triangular configuration may be achieved using two separate, opposing conducting elements (400 and 410) as shown, or alternatively, the same triangular shape may be achieved using a single piece of material. Use of more than one conducting element may provide easier placement of the conducting elements within the passage 310 by providing some “room” for movement of the conducting elements (400 and 410) relative to each other and within the passage 310. Alternatively, conducting elements (400 and 410) may be placed in close contact with the outside surfaces that define the passage 310 and the heat source 130. A space or gap may be left between the neighboring conducting elements (400 and 410). Such a gap may be provided to account for differences in thermal expansion and/or to allow for electrical connections from the heat source 130 to a control module (not shown). Conducting elements may be constructed from any suitable material with higher thermal conductivities, including but not limited to copper and/or aluminum. Thermally conductive ceramics such as aluminum nitride and/or silicon nitride may also be used as the conductive elements (400 and/or 410).
As shown in FIG. 4, one or more conducting elements (e.g. 400 and 410) may be positioned along the x-axis within the passage 310 to increase heat-transfer from the one or more heat sources (e.g. 130) positioned within the passage 310. Alternatively, or in addition to, one or more conducting elements may also be positioned within the passage 310 along the long axis of the housing 200 (z-axis direction), with or without out spaces between neighboring heat sources along the long axis of the housing 200.
FIG. 5 illustrates that an evaporator 110 may include one or more main channels positioned substantially parallel to one another; e.g. where each long axis of each main channel are parallel (relative to the z-axis). In addition, FIG. 5 illustrates that an evaporator 110 may be constructed from individual pieces that are later connected together; e.g. welded, soldered, glued, etc. For example, as shown in FIG. 5, a housing 200 may be constructed as a first piece that defines some of the boundaries of two separate main channels, 210 a and 210 b, where the two main channels share a spanning wall 500 and are divided vertically from each other by a dividing wall 520. Each main channel (210 a and 210 b) has a lower boundary defined by an insert, 530 a and 530 b, respectively. Each insert (530 a and 530 b respectively) includes a first tab (330 a and 330 b respectively) in physical contact with a side wall (510 and 515) of the housing 200. Both first tabs (330 a and 330 b) extend horizontally from the respective side walls (510 and 515) and terminate at a second wall (320 a and 320 b) which extend upwards into its respective main channel (210 a and 210 b) to terminate at a first edge of a first wall (220 a and 220 b). Each first wall (220 a and 220 b) extends horizontally to end at a second edge and connects with a third wall (325 a and 325 b), which extends vertically downward to contact a second tab (335 a and 335 b), where each second tabs (335 a and 335 b) extends horizontally to contact the dividing wall 520. As a result, each insert (530 a and 530 b) provides three walls, the first wall (220 a and 220 b), the second wall (320 a and 320 b), and the third wall (325 a and 325 b), that provide surfaces for contacting with one or more heat sources (not shown). In addition, each insert provides surfaces that, together with the housing 200, define the side channels of the evaporator 110; e.g. a first side channel (300 a and 300 b) and a second side channel (305 a and 305 b).
Referring again to FIG. 5, the inserts (530 a and 530 b) may be provided as separate components to the housing 200 if, for example, the material used for the inserts is significantly more expensive than the material used for the housing. For example, the housing 200 may be fabricated using aluminum, while the inserts (530 a and 530 b) may be fabricated using copper. FIG. 5 shows the concept of using two inserts (530 a and 530 b) in conjunction with a housing 200 to yield two parallel main channels (210 a and 210 b) within a single evaporator 110. However, a single insert or more than one insert could alternatively be used, together with one or more housings to produce an evaporator with one more main channels. Regardless of the complexity of the evaporator and/or number of component pieces used, the inserts are attached to the housing to create a fluid seal. Methods for attaching include welding, soldering, and/or gluing.
Further, one or all of the internal surfaces of an evaporator may have one or more coatings and/or surface treatments to further enhance heat-transfer. Coatings that may be added to the boiling/condensing surfaces (wetted area) of an evaporator that may increase phase change heat-transfer include microporous and nanoporous coatings. These coatings may be sintered, brazed or epoxied to surfaces and may be constructed from copper and aluminum nano- or micron-sized materials.
FIG. 6 illustrates a perspective view of the lower portion of an evaporator 110 similar to that shown in FIG. 5, with inserts and a housing 200 constructed from a single piece of material (e.g. copper or aluminum). FIG. 6 illustrates two substantially parallel passages, 310 a and 310 b, aligned along the z-axis direction. There are three heat sources 130 positioned within each passage, each separated from its neighbors by gaps.
The features and elements of some of the embodiments described herein, provide a number of advantages and benefits, some of which are described in more detail below
1. Dual-Sided Cooling of the Heat Source (e.g. One or More Power Modules) Utilizing an Indirect Two-Phase Cooling Scheme for Increased Heat Dissipation.
The cooling systems described herein enable heat to be removed from multiple sides of the power modules to increase heat dissipation and to allow for smaller cooling systems. The heat on the top-side of the modules may be transferred to the evaporator through direct contact with the evaporator and the conducting elements also provide a heat conduction path through the backside of the power modules to the evaporator.
2. Increased Heat Spreading within the Evaporator for Increased Heat-Transfer.
The cooling systems described herein combine the use of a two-phase heat-transfer with increased surface due to the incorporation of side channels positioned within the evaporator on both lateral sides of the power modules. These side channels allow the two-phase heat-transfer fluid (e.g. refrigerant) to evaporate/boil on the lateral sides of the power modules, which promotes heat spreading through the evaporator housing and increases the wetted surface area in contact with the two-phase heat-transfer fluid. Therefore heat is removed, within the evaporator, via evaporation/boiling through the top and lateral sides of the power modules (and bottom sides due to the use of conducting elements), which significantly increases heat-transfer rates, allowing for a more compact cooling system.
3. Passive (e.g. No Pumping) Two-Phase Scheme Allows for Increased Efficiency and Reliability
The two-phase cooling systems may dissipate large amounts of heat without the need for a pump or compressor (e.g. passive). The two-phase heat-transfer fluid within the system may be transported via gravity, vapor pressure and capillary wicking through an enhanced surface (e.g., microporous coating). Current vehicle cooling systems require a pump to circulate fluid between and/or through their heat exchangers to provide cooling of the heat sources (e.g. power electronics). Alternatively, a passive two-phase cooling system may provide better cooling capacity without the need for a mechanical device to circulate the heat-transfer fluid. Eliminating a pump from a cooling system may result in increased efficiency (e.g. reduced power consumption by the system), increased reliability (e.g. no moving parts), and reduced manufacturing and operating costs.

4. Extrudeable Evaporator Design for Low-Cost Manufacturing

The one-dimensional features of the evaporator and the use of appropriate metals (e.g. aluminum) may allow for the evaporators described herein to be fabricated using an extrusion process. Extruding is a cost-effective method for fabricating components.

5. Limited Inclination Effects on Performance

The compact designs and configurations of the cooling systems described herein, combined with the placement of an evaporator below the condenser, may minimize the effect of vehicle inclination on cooling performance. This is especially true for inclination/rotation along the z-axis (see FIG. 3b ).

6. Condenser and Evaporator May be Constructed as One Unit or Split to Allow for Flexibility.

Some of the cooling systems described herein may be provided with the evaporator and condenser as a single, combined unit, for example, with the evaporator may be the lower manifold on the condenser. Alternatively, a cooling system may also be configured so that the condenser and evaporator are separate and are connected through tubing/piping. This flexibility (e.g. combined or separate) provides options on the placement of the condenser to suit different applications.

7. Increased Heat-Transfer Via the Use of Finned Surfaces and Enhanced Surface Coatings.

An evaporator may incorporate surface area extenders (e.g. finned structures) and boiling enhancement coatings strategically placed within the evaporator to further improve heat-transfer and reduce the size of the cooling system. Other embodiments may comprise boiling enhancement coatings and/or surface coating techniques that have been proven to enhance evaporation/boiling heat transfer coefficients and critical heat flux values by as much as 430% and 120%, respectively.
The power electronics and electric motor (PEEM) in most electric-drive vehicles are often cooled using a dedicated, low-temperature water-ethylene glycol (WEG) cooling loop. Therefore, in hybrid-electric vehicles, there are typically two WEG-based coolant loops—a low-temperature (65° C.) loop to cool the PEEM and a high-temperature (105° C.) loop to cool the internal combustion engine (ICE). These systems tend to be relatively complex, inefficient, and prone to operation issues. Thus, a two-phase cooling system that cools both the power electronics and the electric motor (PEEM) of an electric-drive vehicle would be advantageous. Thus, some of the condenser/evaporator embodiments described herein may be well suited to replace the low-temperature pumped coolant system currently used in electric-drive vehicles with a smaller, lighter, more cost-effective passive (no pump or compressor), two-phase-based cooling system. Some of the cooling systems described herein may increase power densities and lower component operating temperatures by utilizing higher heat-transfer rates of two-phase cooling. For power electronics, increased power densities may result in smaller semiconductor sizes and numbers. For the motor, lower operating temperatures may decrease or eliminate expensive, rare-earth elements used in the motor's permanent magnets. A reduction in the semiconductor size and number and a reduction in rare-earth motor materials may reduce the cost of the electric traction-drive system in electric-drive vehicles. Additionally, an efficient thermal management strategy may be an effective means of improving performance and reliability.
FIG. 7 illustrates a cooling system 100 that utilizes an evaporator 110 and a condenser 120 similar to those described previously for FIGS. 1-6. A cooling fluid 705 is shown for the transfer of heat from the condensing two-phase heat-transfer fluid (not shown) to the external environment. For example, a cooling fluid 705 may be a relatively low temperature air flow passing over an external surface of the condenser 120. In this example, the evaporator 110 and the condenser 120 are illustrated as separate units fluidly connected by a vapor/condensate line 140. The evaporator 110, condenser 120, and vapor/condensate line 140 contain the two-phase heat-transfer fluid (not shown) for transferring heat from a power electronics module 700, which has at least one surface in thermal communication with an external surface of the evaporator 110.
In addition, FIG. 7 illustrates a cooling system 100 that cools a motor 730, in addition to the power electronics module 700. The motor 730 is cooled using a heat-transfer liquid (not shown), where the heat-transfer liquid is circulated through a loop by a pump 780. Examples of heat-transfer liquids that may be used to cool the motor 730 include oils such as mineral oils, and synthetic materials. Examples of oils typically used to cool the electric motor include lubricating transmission oil. The suction side of the pump 780 is connected to a liquid reservoir 760 by a first supply line 770. The discharge side of the pump 790 circulates the heat-transfer liquid through a first heat exchanger 710 that is in thermal communication with the two-phase heat-transfer fluid contained in the evaporator 110. Thus, heat may be transferred from the heat-transfer liquid (circulated by the pump 780) to the two-phase heat-transfer fluid (contained in the evaporator 110) such that the two-phase heat-transfer fluid vaporizes and travels through the vapor/condensate line 140 to condense in the condenser 120. Cooled heat-transfer liquid then exits the first heat exchanger 710 and circulates through a first return line 720 to a second heat exchanger 740 that is configured to be in thermal communication with the motor 730. The motor 730 is at a higher temperature than the heat-transfer liquid flowing through the second heat exchanger 740 and, therefore, heat is transferred from the motor 730 to the heat-transfer liquid by the second heat exchanger 740. The heated heat-transfer liquid is then delivered back to the liquid reservoir 760 through a second return line 750 where the process may be repeated.
The first heat exchanger 710 may be a tube, pipe, and/or coil with an inlet that passes through a sidewall of the evaporator 110 to a portion of the first heat exchanger 710 that is within an inside volume of the evaporator 110 and at least partially submerged in the two-phase heat-transfer fluid. Thus, the heat-transfer fluid (not shown) may pass through an inlet into the submerged portion of a tube, pipe, and/or coil to transfer heat to the two-phase heat-exchange fluid, and then exit from the evaporator 110 through an exit to the first return line 720. In some examples, the first heat exchanger 710 may have fins to increase the surface are available for heat exchange. In still other embodiments, at least a portion of the evaporator 110 may be positioned directly in the liquid reservoir 760 such that at least a portion of the outside surface of the evaporator 110 may be submerged and in direct physical contact with the heat-transfer liquid present within the liquid reservoir 760. Alternatively, a heat-transfer liquid may be circulated through a first heat exchanger 710 that shares a surface with the evaporator 110 such that heat may be transferred from the heat-transfer liquid to the two-phase heat-transfer fluid contained in the evaporator 110. In some case, the pump 780 may be positioned within the liquid reservoir 760 and may be partially or completely submerged in the heat-transfer liquid. Examples of types of pumps that may be used include positive-displacement pumps such as gear pumps, piston pumps, and/or any other suitable pump.
The second heat exchanger 740 may be a closed system, for example, a heat exchanger that is built to be an integral part of the motor 730, such as a volume or space in thermal communication with at least one surface of the motor 730. For example, the heat-transfer liquid may be passed through a volume or space created by an external housing positioned around at least one outside surface of the motor 730, where the housing has an inlet and an outlet for directing the heat-transfer liquid into the housing, and across at least one outside surface of the motor 730 to receive heat from the motor. The heated heat-transfer liquid may then be directed out of the volume or space through an exit to the second return line 750 leading to the liquid reservoir 760. Alternatively, the second heat exchanger 740 may be, or include, an open system. For example, an open system design for a second heat exchanger 710 may include a first return line 720 that terminates with at least one spray nozzle, jet, and/or opening, which may direct the heat-transfer liquid onto at least one outside surface of the motor 730. Thus, the heat-transfer liquid may exit the at least one spray nozzle, jet, and/or opening as a spray at a relatively high exit velocity and/or at a high pressure drop. Alternatively, the heat-transfer liquid may exit the at least one spray nozzle, jet, and/or opening at a relatively low velocity and low pressure drop, for example as a liquid that essentially falls by the influence of gravity to impinge on an outside surface of the motor 730.
The first supply line 770, second supply line 790, first return line 720, and the second return line 750 may be constructed from one or more pipes, tubes, ducts, channels, and/or any other suitable conduit for transferring liquid from one point to another. These conduits may be constructed from copper, aluminum, stainless steel, and/or any other suitable material of construction.
A liquid reservoir 760 may be a closed container, such as a tank. In such a case, the second return line 750 may be connected to the liquid reservoir 760 by a fitting. Similarly, the first supply line 770 may be connected to the liquid reservoir 760 by a fitting. Heat transfer liquid may then enter and exit the tank through these nozzles. Alternatively, a liquid reservoir 760 may be an open-toped tank, such as an oil pan. A liquid reservoir 760 in the form of an oil pan may be well suited for open-system embodiments of the second heat exchanger 740, where for example, the heat-transfer liquid is sprayed onto at least one outside surface of a motor 730.
In summary, FIG. 7 illustrates a cooling system 100 where heat is removed from a motor 730, transferred by a heat-transfer liquid to a two-phase heat-transfer fluid, which also removes heat from a power electronics module 700. Subsequently, the total heat removed from the motor 730 and from the power electronics module 700 may be transferred from the cooling system 100 to the environment by heat-transfer from the condensing two-phase heat-transfer liquid in the condenser 120 to the external environment (e.g. to cooling fluid 705).
FIG. 8 illustrates one embodiment of the general cooling system illustrated in FIG. 7. In the example of FIG. 8, most of the elements of the cooling system are positioned within a containment system 805, which provides a volume that is separated from the outside environment 802. So, a motor 730, an oil collection pan 870, a pump 780, an evaporator 110, a first heat exchanger 710, a second heat exchanger (e.g. spray nozzle 890), and a power electronics module 700 are positioned within the containment system 805. The power electronics module 700 is positioned to be in thermal communication with at least one outside surface of the evaporator 110 to enable the removal of the heat generated by the power electronics module 700. In addition, the power electronics module 700 is positioned between the evaporator 110 and at least one conducting mass 400, which has a set of first surface area extenders 830 to promote the transfer of at least some heat generated by the power electronics module 700 to the internal volume of the containment system 805. The evaporator 110 has at least one main channel 210 positioned vertically and in fluid communication with a condenser 120 and an evaporator reservoir 807. A refrigerant 800 (a two-phase heat-transfer fluid) is contained within the evaporator 110. A portion of the main channel 210 extends out of the containment system 805 into the outside environment, and terminates in fluid communication with a condenser 120. At least one outside surface of the condenser 120 may be contacted by a cooling fluid 705 (e.g. a relatively cool flow of air), causing the refrigerant vapor 810 to condense within the condenser 120 to produce refrigerant condensate 820, which is then transferred by gravity back to the evaporator 110. A first wall 220 of the evaporator 110, corresponding to a portion of the evaporator 110 that is in thermal communication with the power electronics module 700, may have a second set of surface area extenders 840 that project into the liquid volume of the refrigerant 800 (e.g. two-phase heat-transfer fluid). This second set of surface area extenders 840 may increase the surface area available for transferring heat from the power electronics module 700 to the refrigerant 800.
The cooling system 100 of FIG. 8 also illustrates a recirculating oil system for removing the heat generated by a motor 730. The recirculating oil system includes an oil collection pan 870 configured to receive heated oil 860 that has been applied to the outside surfaces of the motor by a spray nozzle 890. The spray nozzle 890 applies an oil spray 850 onto at least one outside surface of the motor. Thus, the motor transfers heat to the oil, cooling the motor, and the heated oil 860 then falls by gravity into the oil collection pan 870. The oil 845 in the collection pan 870 is then pulled into a first supply line 770 by the suction created by pump 780. The first supply line 770 directs the oil through a first heat exchanger 710. This exemplary first heat exchanger 710 is constructed from a length of pipe and/or tubing positioned within the evaporator reservoir 807, and is at least partially submerged in the refrigerant 800. Thus, the heat removed from the motor by the oil 845 is transferred to the refrigerant 800, which vaporizes and is transferred to the condenser 120 and transferred to the cooling fluid 705 in the outside environment 802.
After transferring heat from the oil 845 to the refrigerant 800, the oil is transferred to the pump 780 by suction through the second supply line 790. The pump 780 then discharges the oil into the third supply line 880, which transfer the oil to the spray nozzle 890, which distributes the oil spray 850 onto the motor 730.
Thus, some embodiments of a two-phase cooling system may provide cooling of both the power electronics and the electric motor (PEEM) of an electric-drive vehicle, where the cooling system includes a condenser and an evaporator with a two-phase heat-transfer fluid contained therein and a recirculating heat-transfer liquid system. Such a system may provide the following benefits:
1. Two-phase cooling may increase heat transfer and thus decrease the temperature of the heat-transfer liquid utilized to cool the motor. Lowering the operating temperature of the heat-transfer liquid may allow the motor to operate at lower temperatures which may enable reducing or eliminating rare-earth (expensive) elements used in permanent magnet motors. Eliminating rare-earth elements may result in significant cost reductions. Some of the proposed cooling concepts may allow for lower temperature heat-transfer oil to be used to cool the PEEM while still maintaining a more-elevated bulk temperature for the lubricating oil; higher heat-transfer oil temperatures are beneficial to the transmission/transaxle gears and bearing because of lower heat-transfer liquid viscosities).
2. The combination of two-phase cooling and heat-transfer liquid jet-impingement cooling may increase heat dissipation and thus increase power densities. Higher power densities may reduce the mass of semiconductor material used and the quantity of semiconductor units, which may reduce the costs of such systems.
3. In some embodiments, a cooling system may be combined with and cool high-temperature, wide-bandgap (WBG) power electronic modules. The increased efficiency and high-temperature capabilities of WBG-based power electronics makes them a promising technology for future electric-drive vehicles.
4. In further embodiments, a cooling system may be applied to electric traction-drive systems where the power electronics are integrated into the motor. The trend in electric-drive vehicles is to place the power electronics closer to the motor since this offers advantages in terms of system packaging and performance.
5. Some embodiments of a cooling system may eliminate the typical pumped, low-temperature WEG coolant loop and replace it with an efficient, passive (no pump or compressor) two-phase heat-transfer fluid cooling system.
6. In still further embodiments, a cooling system may provide an option of using the waste heat from the APEEM, for cabin heating. This option would likely require a liquid-cooled condenser. This strategy may be more suited for all electric vehicles where there is no ICE to provide the heating capacity.
Thus, some embodiments of cooling systems include a two-phase heat-transfer fluid cooling system that cool the PEEM and is integrated within the vehicles transmission/transaxle. Further examples of the present invention are provided below.

EXAMPLES

Example 1

Electric Motor Cooling

Two examples that illustrate some of the features of cooling systems 100 for simultaneously cooling both power electronic modules 700 and a motor 730 are shown below in FIGS. 9a and 9b . The configuration shown in FIG. 9a cools a heat-transfer liquid, oil 845, in an oil collection pan 870 using a natural convection heat exchanger, first heat exchanger 710, configured to exchange heat with the evaporator 110. The first heat exchanger 710 is illustrated as a horizontal extension of the evaporator 110, substantially submerged in the oil 845 contained within the oil collection pan 870, and includes fins for increasing the surface area in contact with the oil 845. In this example, a pump 780 draws oil 845 from the oil collection pan 870 and impinges it onto the motor 730 in the form of an oil spray 850. The example shown in FIG. 9b uses natural convective heat transfer in a first portion of the first heat-exchanger 710 a, similar to the example shown FIG. 9a . However, the example of FIG. 9b also utilizes forced convection in second portion of the first heat-exchanger 710 b to provide additional cooling of the oil 845 impinged onto the motor 730. The forced convection portion of the first heat-exchanger 710 b may be designed to more effectively reduce the temperature of the oil that is impinged onto the motor 730 (i.e., T_{oil, motor}<T_{oil, bulk}). The second portion of the first heat exchanger 710 b includes an inlet for drawing oil 845 from the oil collection pan 870 into a section of tubing or piping positioned within the two-phase heat-transfer fluid contained in the evaporator 110.
Decreasing the motor's operating temperature has the potential to decrease or eliminate expensive, rare-earth elements typically used in motors. Rare-earth elements are currently utilized in the motor magnets to increase the motor's operating temperature. The less-effective natural convection heat exchanger/evaporator allows the ATF at the reservoir to operate at higher temperatures (e.g., 70° C. −90° C.) which is beneficial to the gears and bearing due to lower ATF viscosities at higher temperatures.
FIGS. 9a and 9b illustrate most of the cooling system 100 components housed within a containment system 805, with the exception of the condenser 120 and a portion of the main channel 210 of the evaporator 110. These examples also show at least one power electronics module 700 positioned in thermal communication with a first wall 220 of the evaporator 110. The power electronics module 700 is sandwiched between the first wall 220 of the evaporator 110 and a conducting element 400 having one or more surface area extenders 830.

Example 2

Power Electronics Cooling

FIG. 10 illustrates further embodiments of a proposed cooling system 100 for cooling a power electronics module 700 and a motor 730. The majority of the heat generated by the power electronics module 700 may be dissipated an evaporator 110 in conjunction with a condenser 120, utilizing a two-phase heat-transfer fluid contained therein. A surface of the power electronics module 700 may be placed in thermal communication with a first wall 220 of the evaporator 110. Vaporized two-phase heat transfer fluid may travel through the evaporator's main channel 210 to deliver the vapor to the condenser 120 where it condenses. This two-phase cooling approach may provide the sole means of heat dissipation from the power electronics module 700, as is shown above in Example 1. However, additional cooling of the power electronics 700 may be provided by impinging oil 890 b onto an outside surface of the power electronics module 700. As shown in FIG. 10, an outside surface of the power electronics module 700 may include a thermally conductive element 400 in thermal communication with a plurality of surface area extenders 830. For example, a thermally conductive element 400 may include finned surfaces and/or enhanced surfaces to augment heat transfer. Impinging oil 890 b directly onto the thermally conductive element 400 may improve heat transfer (through the use of finned and enhanced surfaces) and/or prevent or minimize contacting the power electronic module 700 with the oil 845.
Impinging oil 890 b onto an outer surface of a power electronics module 700 may be accomplished using two pumps—a first pump 780 a for the motor and a second pump 780 b for the power electronics module 700. Such a configuration may provide additional cooling capacity during high peak power demand periods. However, a single pump may be provided in other embodiments to oil to both the power electronics module 700 and to the motor 730. For either cases (one or two oil pumps), it may be possible to further reduce the oil 845 temperature prior to contacting the power electronics, by contacting the oil with at least one outside surface of the evaporator 110 prior to contacting an outside surface of the power electronics module 700. For example, this may be accomplished by contacting the oil 845 on one or more outside surfaces of the evaporator 110 above the power electronics module 700, after which the oil flows by gravity over the power electronics module 700. The oil 845 may then transfer heat to the evaporator 110 and vaporize the two-phase heat-transfer fluid contained therein to reduce the oil temperature. The cooled oil 845 may then be sprayed 850 b onto the power electronics to provide additional cooling. The heated oil will then gravity drain back to the oil collection pan 870. Thus, the example of FIG. 10 illustrates one or more spray nozzles 890 a for distributing oil (e.g. in the form of an oil spray 850 a) onto surfaces of the motor 730 for cooling the motor.
FIG. 10 illustrates most of the cooling system 100 components housed within a containment system 805, with the exception of the condenser 120 and a portion of the main channel 210 of the evaporator 110. This example also shows at least one power electronics module 700 positioned in thermal communication with a first wall 220 of the evaporator 110. The power electronics module 700 is sandwiched between the first wall 220 of the evaporator 110 and a conducting element 400 having one or more surface area extenders 830.
In any of the examples described above, a feasible alternative may include replacing the oil spray/impingement concepts with a jet impingement, oil-dripping, or channel-flow type cooling strategy. In a channel flow configuration, a pump may circulate a heat-transfer liquid (e.g. oil) through a heat exchanger mounted on one or more external surfaces of the power electronics module. In other examples, oil spray concepts may be utilized in conjunction with a jet impingement, oil-dripping, or channel flow configurations.
In some embodiments, a cooling system having a condenser and an evaporator may operate at a pressure ranging from close to absolute vacuum to about 300 psia. In other embodiments, a cooling system having a condenser and an evaporator may operate at a pressure ranging from close to 200 psia to about 300 psia. A two-phase heat-transfer fluid, may have a boiling point of about 50° C. to about 100° C. at a pressure of one atmosphere. A heat-transfer liquid (e.g. oil) may operate at a temperature of about 90° C. to about 120° C. A heat-transfer liquid may have a high operating temperature, T_H, and a low operating temperature, T_L, where the difference between T_Hand T_Lis from about 1° C. to about 10° C. In some examples of a cooling system, the temperature difference between the operating temperature, T₁, of a two-phase heat-transfer fluid and the high operating temperature, T_H, of a heat-transfer liquid (e.g. oil), may be a ΔT of about 5° C. to about 20° (ΔT=T_H−T₁).
As used herein, the terms “about” and “substantially” refer to a plus and/or minus deviation of 5% around the numerical value stated. For example, “about 100° C.” refers to a temperature from 95° C. to 105° C. “About 200 psia” refers to a pressure from 190 psia to 210 psia. The term “substantially vertical” refers to an element positioned at an angle of 85.5 degrees to 94.5 degrees relative to a reference plane.

Example 3

Testing of a Passive, Two-phase Cooling System

Experimental Apparatus: FIG. 11 illustrates a schematic of a cooling system tested. Two different evaporator design were tested—a copper cold plate-based design and an aluminum-based design. Both evaporators were designed to cool six Delphi discrete power modules/switches. The six power modules represent a voltage source inverter system required to power an automotive electric machine/motor. Further details of the the evaporator designs tested are provided below.
Two condensers were tested, one with plain tubes and one with rifled tubes. The rifled features, shown in FIG. 12, were evaluated as a means of enhancing condensation heat transfer. Per the manufacturer, the condensation-side surface areas were 1,190 cm²and 1,250 cm²for the plain and rifled condensers, respectively. The two condensers were finned-tube, air-cooled type heat exchangers. The fins were louvered and fabricated from 0.15-mm-thick aluminum sheets. The total air-side surface area was calculated to be approximately 29,000 cm². Twenty 0.95-cm (⅜-in.) outer-diameter copper tubes were arranged in two rows (see FIG. 11). Two tubes, one from each row, were connected at the top via U-bend fittings. A manifold header connected all tubes at the lower end.
Heat from the system was rejected to air by means of a 17.8-cm (7-in.) diameter automotive axial fan mounted to the condenser. The fan operated on 12 V and consumed 38 W of power, calculated by voltage and current measurements. Two 2.54-cm-inner-diameter tubes connected the condenser manifold to the evaporator. The tubes were sized large enough to prevent falling liquid from restricting/blocking the rising vapor.
The system was designed with a maximum operating pressure of 1.03 MPa (150 psi). Finite element structural analysis was used to design the evaporators to allow for elevated-pressure operation. The condensers were purchased and had a 2 MPa pressure rating. Once the condensers and evaporators were assembled, hydrostatic pressure-tests were conducted to verify the system's pressure rating. The cooling system was instrumented with sensors to measure system pressure and temperatures. System vapor pressure was measured using a calibrated absolute pressure transducer. System temperatures were measured using calibrated K type thermocouples for the inlet-air, outlet-air, liquid, vapor, and heater temperatures.
Experimental Procedures: Six Watlow ceramic heaters were used in place of the Delphi power modules. The dimensions of the ceramic heaters (25 mm×15 mm×2.5 mm) were similar to those of the Delphi modules. Each heater generated up to about 580 W of heat (total power for six heaters: 3,500 W). The ceramic heaters were externally attached to the evaporators using thermally conductive grease as the thermal interface material. The temperatures of the heaters were measured via thermocouples embedded within the ceramic heaters.
After the heaters were attached to the evaporator, the system was charged using a transfer tube that contained a measured amount of saturated, oil-free refrigerant. Prior to charging the system with the refrigerant, the air in the system was removed using a vacuum pump. Pressure within the system was allowed to decrease to about 2 Pa to ensure that most of the air was evacuated. A valve between the transfer tube and the system was then opened, allowing the refrigerant to drain into the system. Once the refrigerant was transferred, the valve between the transfer tube and the system was closed, and the transfer tube was disconnected from the system. Measurements of the vapor temperature and pressure confirmed saturated conditions, verifying that no air was present within the system.
Experiments were initiated after saturated conditions were verified. First, the fan was powered to pull ambient air (Ta inlet=25° C.) through the condenser. The six heaters were then powered using two Agilent direct current power supplies. Heater loads ranged from 250 W to 3,500 W. The system was allowed to reach equilibrium conditions (about 15 minutes) at each power level before increasing the power. Measurements of the system and heater temperatures combined with heat load measurements were used to compute the evaporator and condenser thermal resistances at various power levels.
Uncertainty Analysis: Analysis was conducted to quantify the uncertainty in the measured experimental values according to the procedures known in the art. The procedure consisted of gathering systematic and random uncertainties in all measured variables. The propagation-of-error equation was then used to estimate the uncertainties in the calculated values. The uncertainty for the thermal resistance values is estimated to be approximately ±9%. After calibration, the uncertainty in a thermocouple was conservatively estimated at ±0.1° C., while the uncertainties in the heat measurements were estimated to be ±1%. All stated uncertainties were calculated at a 95% confidence level.
Results: Experiments were conducted to measure the thermal performance of a passive two-phase cooling system. This included measuring the thermal resistance of the condenser and evaporator. The thermal performance data combined with the volume, weight, and parasitic power requirements of the two-phase cooling system were then compared with equivalent metrics of a conventional, water-ethylene glycol-based (WEG) cooling system.
Experiments were conducted to measure the thermal resistance of two evaporator designs—a copper cold plate-based design and an advanced all-aluminum-based design. The evaporator's specific (area-weighted) thermal resistance was defined per Equation 1.
$\begin{matrix} R_{th, evaporator}^{″} = \frac{(\overline{T_{htr}} - T_{l})}{Total power} \times A_{htr} & (1) \end{matrix}$
where T_htr is the average temperature of the six ceramic heaters as measured by the thermocouples embedded within each heater, and T_lis the refrigerant liquid temperature. The total power is the total heat dissipated by the system and A_htris the total surface area of the six heaters (22.5 cm²).
Evaporator Thermal Performance (Concept 1): The initial copper cold plate design consisted of a steel cylinder and three copper cold plates and was charged with 250 cm³of refrigerant (see FIG. 13). This evaporator's flexible design also allows testing of different boiling/evaporation enhancement techniques (e.g., boiling enhancement coatings and finned surfaces). The copper cold plates were machined with 4-mm-tall fins, each of which has a wetted surface area of about 55 cm². Because two-phase cooling provides high heat transfer rates, the fins are not expected to have a significant effect on the evaporator thermal resistance. However, the fins were included as a means of increasing surface area in an attempt to delay dry-out.
The specific thermal resistance of the copper cold plate evaporator is plotted versus the total heat dissipated in FIG. 14. Results for refrigerants HFC-245fa (330 grams) and HFO-1234yf (280 grams) are provided. As shown in FIG. 14, the heater-to-liquid resistances for both refrigerants decrease with increasing heat dissipation. This effect is associated with an increased contribution from two-phase heat transfer (i.e., boiling/evaporation) at higher power levels, which improves thermal performance. Tests were performed with increasing and decreasing heat fluxes to evaluate for hysteresis effects. Results showed that using an increasing or decreasing heat rate had little effect on the thermal performance of the cooling system.
With 250 cm³of HFC-245fa, the system was capable of dissipating 3.5 kW of heat under steady-state conditions without reaching dry-out (i.e., critical heat flux). The refrigerant-volume-to-heat-dissipated ratio, at maximum heat load, was 71 cm³/kW. At 3.5 kW, the heaters were at their maximum allowable power rating, thus it was not possible to test at higher heat loads. The 3.5 kW of heat dissipation is noteworthy because it was a conservative estimate on the inverter heat dissipation requirement for a 55-kW electric traction-drive system. With HFO-1234yf, tests were limited to lower heat loads due to HFO-1234yf's higher operating pressures. At 1.25 kW of heat dissipation, HFO-1234yf's saturated temperature reached 42° C., which corresponded to a pressure of about 1.1 MPa—the maximum operating pressure of the system. Increasing the heat dissipation with HFO-1234yf required increasing the condensing and/or pressure capacity of the system. Compared at the same heat loads, HFO-1234yf produced thermal resistance values that were 22%-47% lower than those produced with HFC-245fa. HFO-1234yf's higher heat transfer coefficients allowed it to outperform HFC-245fa.
Evaporator Thermal Performance (Advanced Design): Features to improve the evaporator's performance and reduce its size were identified and incorporated into an advanced evaporator design. The features were intended to reduce the evaporator thermal resistance while utilizing low-cost fabrication techniques and materials (e.g., aluminum). The advanced evaporator concept used an indirect cooling approach to be compatible with conventional power electronic packages (i.e., silicon on ceramic substrate). A simple schematic of the advanced evaporator design is shown in FIG. 15. The evaporator was designed to cool six Delphi discrete power switches. The advanced design reduced the refrigerant volume to 180 cm³(HFC-245fa=240 grams, HFO-1234yf=200 grams). For comparison, the 2010 Toyota Camry requires 510 grams of refrigerant (HFC-134a) for the cabin's air-conditioning system. Also, typical automotive inverter coolant systems utilize several liters of WEG (i.e., antifreeze). Reducing the refrigerant quantity is an effort to reduce system cost, weight, and size. As shown in FIG. 15, the advanced design is more compact as compared with the previous copper-based design.
The specific thermal resistance of the advanced evaporator design is compared in FIG. 16 to the thermal performance of the previous copper cold-plate design. The performance curves shown in this figure were obtained using HFC-245fa. The results demonstrated that the advanced design can dissipate automotive-scale power electronic heat loads (3.5 kW) with only 180 cm³of refrigerant. Additionally, the unique features of the advanced evaporator design allowed the aluminum evaporator to provide equal or lower thermal resistance values as compared with the initial evaporator design that utilized copper cold plates. Further reductions to the thermal resistance can be obtained if the advanced design is fabricated entirely out of copper. However, in an effort to reduce cost and weight, the use of aluminum is seen as a more practical option.
At higher heat loads (≧3 kW), fluctuations in the pressure and temperature were observed for tests with the advanced evaporator design. These fluctuations resulted in an increase in thermal resistance. The fluctuations are believed to be associated with the compact size of the advanced evaporator design that restricts vapor from exiting the evaporator. Applying microporous coatings to the evaporator's boiling surface may reduce or eliminate the fluctuations. Microporous coating structures provide passive refrigerant transport via wicking and may reduce the amount of vapor generation and these effects are believed to potentially suppress pressure-temperature fluctuations in passive, two-phase systems.
It is important to note that the thermal performance results provided in FIGS. 14 and 16 were obtained using ceramic heaters attached via thermal interface material. These heaters were used as a substitute for actual power modules attached via bonded interface materials (e.g., thermoplastics, solder). Therefore, the thermal resistance values are not necessarily indicative of the thermal performance in actual applications. Also, the thermal performance results provided in FIGS. 14 and 16 were obtained using non-coated evaporator surfaces. The use of boiling enhancement coatings such as 3M's copper microporous coating within the evaporator may enable both increased heat dissipation and lower thermal resistance values.
The junction-to-liquid thermal resistance of the advanced evaporator design was simulated through finite element analysis (FEA). A computer-assisted design (CAD) model of the Delphi power modules bonded to the advanced evaporator design was first developed. The CAD model incorporated all the thermal resistance interfaces within the module stack, including the solder layers within the power electronics module and a thermoplastic-type bonded interface between the power electronics module and the evaporator. The model was then imported into ANSYS Workbench for thermal analysis. The FEA imposed heat transfer coefficient boundary conditions to simulate boiling heat transfer from enhanced surfaces within the evaporator. The boiling heat transfer coefficients for HFC-245fa and HFO-1234yf were experimentally measured with enhanced surfaces (3M microporous boiling enhancement coating) at various saturated temperatures. The measured heat transfer coefficient values exceeded 100,000 W/m²-K within a wide heat flux range. Moreover, the performance of the two refrigerants was found to be similar for boiling on microporous-coated surfaces. Because uniform boiling may not occur with the evaporator surfaces, a conservative estimate on the heat transfer coefficients was imposed (50,000 W/m²-K) for these simulations.
The specific thermal resistance results (junction-to-liquid) as predicted by FEA are provided in Table 1. The insulated gate bipolar transistor's area and maximum temperature (i.e., junction temperature) combined with the refrigerant temperature were used to calculate the thermal resistance values. Two evaporator designs were analyzed—aluminum-based and copper-based. The aluminum fabrication is a more practical design while the copper fabrication is more of a concept aimed at reducing the package stack resistance. For comparison, the thermal resistance (junction-to-liquid) of the 2008 Lexus Hybrid double-sided and liquid (WEG)-cooled power module are also shown in Table 1. The thermal resistance value of 0.33 cm²-K/W was calculated using performance data known in the field.

TABLE 1

The FEA-estimated evaporator (junction-to-liquid) thermal
resistances for aluminum and copper evaporators. Performance
data for an automotive cooling system are provided for comparison.

	R″_th
	(cm²-	(% R″_th
	K/W)	reduction

Lexus Hybrid (2008) double-side	0.33	—
cooled modules	[11, 12]
Two-phase: aluminum baseplate	0.14	58%
(finite element analysis results)
Two-phase: copper baseplate	0.12	65%
(finite element analysis results)

The FEA-predicted thermal resistance values of the aluminum (0.14 cm²-K/W) and copper (0.12 cm²-K/W) evaporator modules are about 58% and 65% lower, respectively, than that of the double-sided, WEG-cooled 2008 Lexus system. (The 2013 Toyota Camry Hybrid uses a similar power modules and cooling system.) These thermal resistance reductions translate to a 139% and 189% increased heat flux capacity. Experimentally measuring the thermal resistance of the advanced evaporator with a power module was not possible due to equipment power limitations. An immersion cooling (two-phase) strategy may allow for even greater thermal enhancements. However, an indirect cooling approach was used in this case to allow for its use with more traditional power modules and to alleviate some reliability concerns associated with immersing electronics in a refrigerant.
Condenser Thermal Performance and Analysis: The unit-thermal resistances for the condensers are provided in Table 2 for both refrigerants. The vapor-to-air resistance includes the condensation-side and the air-side resistances and was defined per Equation 2.
$\begin{matrix} R_{th, codenser}^{″} = \frac{(T_{v} - {\overline{T}}_{a})}{Total power} \times Condenserfrontal area & (2) \end{matrix}$
where T_vis the refrigerant vapor temperature and T _ais the average inlet air temperature as measured by two thermocouples just upstream of the condenser. The stated condenser performances are for a passive condenser design cooled via an automotive axial fan. The total fan parasitic power was measured to be 38 W. An estimate of the air flow rate was calculated by imposing an energy balance on the air-side (i.e., inlet and outlet to the condenser) and the total heat dissipated. Assuming steady-state conditions and incorporating the appropriate air thermal properties, the estimated air volumetric flow rate is 0.12 m³/s (250 ft³per minute).

TABLE 1

Condenser thermal resistance values calculated using Equation 2.

R″_{th (cm} ²-K/W)

Rifled

	Refrigerant	Plain	Rifled	enhancements

HFC-245fa	9.30	7.58	18%
HFO-1234yf	8.12	6.06	25%

Condensation-side enhancements from the rifled tubes were found to reduce the overall condenser thermal resistances by 18% and 25% for HFC-245fa and HFO-1234yf, respectively. The results show that the rifled structures are more effective at enhancing condensation heat transfer with HFO-1234yf. Moreover, better performance is achieved with HFO-1234yf. For the plain tube condenser, HFO-1234yf yielded thermal resistance values that were about 13% lower than those with HFC-245fa. For the rifled tube condenser, HFO-1234yf yielded thermal resistance values that were about 20% lower than those with HFC-245fa.
An analysis was conducted to estimate condenser size based on operating conditions, a maximum allowable cooling system temperature (i.e., vapor and liquid), and the experimentally measured condenser thermal resistance values provided in Table 1. The operating conditions used for this analysis were: 3.3 kW of steady-state heat dissipation (estimated requirements for a 55-kW traction drive inverter) and 43° C. inlet air temperature. The estimated condenser frontal area (i.e., frontal footprint) requirements are plotted versus the system temperature in FIG. 17. In the figure, the lower system temperature of 65° C., used for this analysis, corresponds to the coolant (i.e., WEG) temperature typical of existing automotive power electronics systems. The solid line curves for both refrigerants are the sizing requirements for the finned-tube condenser per the performance data reported in Table 1. The T_jcurve in FIG. 17 represents the maximum junction temperature and was calculated using the thermal resistance data for an aluminum evaporator and a six power module/switch system configuration.
Because typical automotive condensers are constructed using a brazed, folded-fin design, a simplified analysis was conducted to estimate the sizing requirements for a folded-fin type condenser. For this analysis, the ratios of the air-side surface area to frontal surface area were measured for finned-tube and folded-fin condensers. The air-side-to-frontal-surface-area ratios were calculated to be 55.5 mm²/mm²for the finned-tube and 86.7 mm²/mm²for folded-fin condensers, assuming a condenser thickness of 4.5 cm for both cases. The folded-fin frontal area requirements were estimated by matching the air-side surface area for the folded-fin design to those of the finned-tube design at the various system temperatures. The folded-fin frontal area requirements were then calculated via the surface area ratio (86.7 mm²/mm²) and the results are shown FIG. 17. This simplified analysis assumes that the air-side is the dominant thermal resistance, and air velocities are similar to those provided by the fan used in this study. For reference, the performance of a folded-fin condenser operating in a thermosyphon configuration, as reported by Barnes and Tuma (“Practical Considerations Relating to Immersion Cooling of Power Electronics in Traction Systems,” IEEE Transactions on Power Electronics, (25:9), 2010; pp. 2478-2485.), is provided in FIG. 17. In that study, a condenser thermal resistance of 4.6 cm²-K/W was reported using a hydrofluoroether fluid and an air velocity and pressure drop of 2.2 m/s and 44 Pa, respectively. The estimated condenser sizing requirements, per the performance reported by Barnes and Tuma, are similar to the results predicted for HFC-245fa.
The size requirements of the condenser can then be estimated using FIG. 17 and a maximum allowable system temperature. For low-temperature applications typical of existing automotive power electronics coolant temperatures and conventional silicon devices, the use of HFO-1234yf is recommended because it provides better performance. At a system temperature of 80° C. and with HFO-1234yf, the condenser frontal size requirements are estimated to be about 325 cm²with a maximum T_jof about 125° C. HFC-134a may also be considered in this case because it is a refrigerant currently used in automotive systems and because prior studies have shown that its heat transfer performance (boiling and condensation) is similar, if not slightly better than, that of HFO-1234yf.
Operating at higher system temperatures has advantages because it allows for a more compact condenser. However, higher temperature operation may be dependent on the development of higher temperature auxiliary electronic devices (e.g., capacitors) that are packaged within the inverter. With this in mind, if higher system temperatures are practical, HFC-245fa is recommended due to its higher critical temperature (T_C=154° C.) and lower operating pressures. At a system temperature of 95° C. and a T_j=148° C., the condenser size requirements would decrease to about 310 cm².
Two-Phase and Baseline Cooling Metric Comparisons: Analysis was conducted to compare the coefficient of performance (COP), volume, and weight of a passive two-phase cooling system with that of a conventional automotive WEG-based (single-phase) power electronics cooling system.
Passive Two-Phase Inverter Cooling System Metrics: The condenser, evaporator, and refrigerant were included in the volume and weight metrics for two-phase cooling system. The metrics for an aluminum evaporator were directly measured from the prototype that was fabricated and tested. The condenser metrics were estimated based on the condenser finned-frontal-area requirements from FIG. 17 assuming 80° C. (HFC-245 assumed) maximum system (liquid and vapor) temperatures. The additional volume of the headers/manifolds and specific weight (weight/volume) of an automotive condenser was measured and used to compute the total volume (finned and headers) and the weight of the condenser for the passive two-phase cooling system. The 240 grams (HFC-245 assumed) of refrigerant was included in the total system weight. The refrigerant volume was not included in the total volume measurement because the refrigerant is contained within the evaporator and thus its volume is accounted for in the evaporator volume. The thermal resistance of an aluminum evaporator (from Table 1) combined with the total parasitic power of the system (38-W fan parasitic power) was used to compute a COP value per Equation 3.
$\begin{matrix} COP = \frac{1}{R_{th}^{″} \times Parasitic power} & (3) \end{matrix}$
The volume and weight of the fan and associated piping (connecting the evaporator to the condenser) were not included in the total volume and weight calculations.
Baseline, WEG-Based Inverter Cooling System Metrics: Conventional automotive WEG-based inverter cooling systems consists of a cold plate to directly cool the inverter, radiator, pump, fan, WEG, and associated piping. Estimating the metrics for a baseline, the WEG-based automotive inverter cooling system is not a straightforward procedure because these systems are also designed to cool the electric motor. Therefore, the radiators in these inverter cooling systems are sized to dissipate the combined heat loads of the inverter and the electric motor. Because the proposed two-phase cooling system only considers cooling the inverter, analysis was conducted to size a radiator to dissipate heat loads for the inverter only, per procedures known in the art. The radiator was sized to dissipate 3.3 kW of heat with a maximum inlet air temperature of 43° C.—the same conditions used to size the two-phase condenser. Additionally, a 10 L/min WEG flow rate was assumed within the radiator. From this analysis, the finned radiator volume, fan pressure drop and flow rate, and pump pressure drop were estimated. The additional volume of the headers/manifolds and specific weight (weight/volume) of an automotive radiator was measured and used to compute the total volume (finned and headers) and the weight of the inverter-only radiator. The air-side pressure drop and flow rate were used to compute the fan parasitic power assuming 20% fan efficiency.
The 2012 Nissan Leaf inverter (80-kW motor) cold plate/heat exchanger was used to compute the volume, weight, and WEG pump parasitic power metrics for the inverter cold plate. The volume of the cold plate was directly measured and then scaled down by the ratio 55 kW/80 kW (80 kW for the Nissan Leaf and 55 kW for the two-phase cooling system). The weight was computed assuming the density of aluminum (6061) and a 60% cold plate void space (i.e., WEG channels).
Experiments were conducted to measure the parasitic power required to circulate WEG (10 L/min flow rate and 60° C.) through the 2012 Nissan Leaf inverter cold plate. The power required to circulate WEG through the inverter cold plate and radiator was used to compute the total pump parasitic power requirements assuming a 60% pump efficiency. The COP of the baseline system was calculated per Equation 3 using the total parasitic power (fan and pump) and the specific thermal resistance (junction-to-liquid) of the 2012 Nissan Leaf.
The volume of the WEG, contained within the Nissan Leaf cold plate was measured and doubled in an attempt to account for the total WEG volume in both the cold plate and radiator. The total WEG volume was computed to be approximately 1.6 L. The WEG's volume was not used when computing the overall volume of the system because the WEG is contained within the system components and thus its volume is accounted for in the cold plate and radiator volume. However, the WEG volume was used to compute the WEG weight via the specific weight properties of WEG. The weight of the WEG was then utilized to compute the overall baseline system weight. The volume and weight of the fan, pump, tubing, and WEG within the tubing were not included in the total volume and weight calculations for the baseline cooling system.
As shown in Table 3, utilizing a passive two-phase cooling system reduced the weight by an estimated 41% and increase the COP by an estimated 127%. The volumes of the two cooling systems were nearly identical; however, more components were excluded from the baseline system (i.e., fan, pump, piping, and additional WEG volume and weight) as compared with the two-phase system (i.e., fan and piping) and thus reductions to the volume are also likely. The majority of the reductions to the system are associated with reducing the amount of coolant/refrigerant and reducing the size of the inverter/power module heat exchanger. The advanced aluminum evaporator 33% the volume of the scaled-down (by 55 kW/80 kW) 2012 Nissan Leaf cold plate. Moreover, the two-phase cooling system contains about 17% less aluminum (by weight) as compared to the WEG-based cooling system.

TABLE 2

Percent reductions to the volume and weight and
percent increases to the COP and heat dissipation
using a passive two-phase cooling system.

Volume	Weight		Heat dissipation
reduction	reduction	COP	increase

−2%	41%	127%	139%

It should be noted that the size of the condenser can be reduced and the volume and weight reductions listed in Table 3 would increase, if the two-phase coolant system is allowed to operate at higher temperatures (FIG. 7). In this analysis, the maximum two-phase temperatures (vapor and liquid) were kept below 85° C. to enable the use of low-temperature capacitors.
Conclusions: Experiments and analysis have been conducted to evaluate the use of two-phase cooling (passive) for automotive power electronics. The following summarizes some of the results from this work:
It was demonstrated that a passive two-phase cooling system can cool six Delphi discrete power modules, dissipating about 55 kW inverter-scale heat loads (˜3.5 kW) with only 180 mL of refrigerant.
The proposed passive and indirect two-phase cooling approach may reduce the junction-to-liquid thermal resistance by 58% to 65%. These reductions to the thermal resistance translate to a 139% to 189% increase in the device heat dissipation capabilities.
Analysis indicates that using a passive two-phase cooling approach may reduce the weight (by 41%) and significantly improve the COP (by 127%) of the inverter thermal management system. Additional improvements may be obtained if the two-phase cooling system is allowed to operate at higher vapor-liquid temperatures.
The foregoing discussion and examples have been presented for purposes of illustration and description. The foregoing is not intended to limit the aspects, embodiments, or configurations to the form or forms disclosed herein. In the foregoing Detailed Description of Some Embodiments for example, various features of the aspects, embodiments, or configurations are grouped together in one or more embodiments, configurations, or aspects for the purpose of streamlining the disclosure. The features of the aspects, embodiments, or configurations, may be combined in alternate aspects, embodiments, or configurations other than those discussed above. This method of disclosure is not to be interpreted as reflecting an intention that the aspects, embodiments, or configurations require more features than are expressly recited in each claim. Rather, as the following claims reflect, inventive aspects lie in less than all features of a single foregoing disclosed embodiment, configuration, or aspect. While certain aspects of conventional technology have been discussed to facilitate disclosure of some embodiments of the present invention, the Applicants in no way disclaim these technical aspects, and it is contemplated that the claimed invention may encompass one or more of the conventional technical aspects discussed herein. Thus, the following claims are hereby incorporated into this Detailed Description of Some Embodiments, with each claim standing on its own as a separate aspect, embodiment, or configuration.

Claims

What is claimed is:

1. An evaporator comprising:

a first wall comprising:

an external surface;

a first edge; and

a second edge, wherein:

the first wall, the first edge, and the second edge are substantially parallel to a plane, and

the first edge and the second edge are substantially parallel to each other;

a second wall extending from the first edge and the external surface, substantially perpendicular to the plane, and substantially parallel to the first edge; and

a third wall extending from the second edge and the external surface, substantially perpendicular to the plane, and substantially parallel to the second edge, wherein:

the external surface of the first wall, the second wall, and the third wall form a passage substantially parallel to the first edge,

the passage is configured to contain at least one heat source, and

at least the first wall is configured to be in thermal communication with the at least one heat source.

2. The evaporator of claim 1, further comprising a conducting element, wherein:

the conducting element is positioned within the passage,

the conducting element is configured to be in thermal communication with the at least one heat source, and

the conducting element is in thermal communication with at least one of the second wall or the third wall.

3. The evaporator of claim 2, wherein:

the conducting element comprises a block of material with a substantially triangular cross-section,

the block of material has a first side that is in thermal communication with either the second wall or the third wall, and

the block has a second side that is configured to be in thermal communication with the at least one heat source.

4. The evaporator of claim 2, wherein the conducting element comprises:

a first block of material with a substantially triangular cross-section; and

a second block of material with a substantially triangular cross-section, wherein:

the first block of material has a first side that is in thermal communication with the second wall, and a second side that is configured to be in thermal communication with the at least one heat source, and

the second block of material has a first side that is in thermal communication with the third wall, and a second side that is configured to be in thermal communication with the at least one heat source.

5. The evaporator of claim 1, wherein the first wall further comprises an internal surface and the evaporator further comprises:

a surface area extender that extends from the internal surface, wherein:

the internal surface is substantially parallel to the external surface, and

the surface area extender is substantially perpendicular to the plane.

6. The evaporator of claim 5, wherein the surface area extender comprises a fin, wherein the fin is substantially parallel to the first edge.

7. The evaporator of claim 6, wherein:

the internal surface and the external surface define a width of the first wall, and

the fin comprises a height that is approximately equal to the width.

8. The evaporator of claim 1, wherein:

the second wall terminates with an edge,

the third wall terminates with an edge,

the edge of the second wall and the edge of the third wall are positioned below the external surface, and

the evaporator further comprises:

a first tab extending from the edge of the second wall, substantially perpendicular to the second wall, and away from the passage; and

a second tab extending from the edge of the third wall, substantially perpendicular to the third wall, and away from the passage.

9. The evaporator of claim 8, further comprising a housing, wherein:

the housing comprises:

a first end connected to the first tab;

a second end connected to the second tab; and

at least one wall physically connecting the first end to the second end, wherein:

the housing forms a first interior channel between the interior surface of the first wall and the housing,

the housing forms a second interior channel between the second wall and the housing, and

the housing forms a third channel between the third wall and the housing.

10. The evaporator of claim 9, wherein the first wall, the second wall, the third wall, the first tab, the second tab, and the housing are all a single piece of material.

11. The evaporator of claim 10, wherein the single piece of material is aluminum.

12. The evaporator of claim 9, wherein the first wall, the second wall, the third wall, the first tab, and the second tab are all a first single piece of material.

13. The evaporator of claim 12, wherein the first single piece of material is aluminum.

14. The evaporator of claim 13, wherein the housing is a second single piece of material.

15. The evaporator of claim 14, wherein the second single piece of material is copper.

16. A cooling system comprising:

an evaporator configured to cool a first heat source;

a condenser in fluid communication with the evaporator;

a refrigerant contained within the condenser and the evaporator; and

a circulating liquid system comprising:

a liquid contained within the circulating liquid system;

a liquid reservoir;

a pump in liquid communication with the liquid reservoir;

a first heat exchanger in liquid communication with the pump, wherein the first heat exchanger is configured to deliver heat from the liquid to the refrigerant; and

a second heat exchanger in liquid communication with the first heat exchanger, wherein:

the second heat exchanger is configured to deliver heat from a second heat source to the liquid,

the second heat exchanger is in liquid communication with the liquid reservoir, and

the pump circulates the liquid through the first heat exchanger, the second heat exchanger, and the liquid reservoir.

17. The cooling system of claim 16, wherein the second heat exchanger comprises a spray nozzle, wherein the liquid is sprayed onto the second heat source.

18. The cooling system of claim 17, wherein the liquid reservoir comprises a liquid collection pan configured to collect oil heated by the second heat source.

19. The cooling system of claim 16, wherein the evaporator and the circulating liquid system are fluid-sealed within a container operating at a first average temperature.

20. The cooling system of claim 19, wherein the condenser operates at a second average temperature that is less than the first average temperature.