WO2011056860A1 - Echangeur de chaleur à ailettes microcanal - Google Patents

Echangeur de chaleur à ailettes microcanal Download PDF

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Publication number
WO2011056860A1
WO2011056860A1 PCT/US2010/055285 US2010055285W WO2011056860A1 WO 2011056860 A1 WO2011056860 A1 WO 2011056860A1 US 2010055285 W US2010055285 W US 2010055285W WO 2011056860 A1 WO2011056860 A1 WO 2011056860A1
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WIPO (PCT)
Prior art keywords
fin
micro
fluid
fins
channels
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PCT/US2010/055285
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English (en)
Inventor
Israel Urieli
Khairul Alam
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Ohio University
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Publication of WO2011056860A1 publication Critical patent/WO2011056860A1/fr

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/0266—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00—Tubular elements; Assemblies of tubular elements
    • F28F1/02—Tubular elements of cross-section which is non-circular
    • F28F1/022—Tubular elements of cross-section which is non-circular with multiple channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D2015/0225—Microheat pipes

Definitions

  • the invention relates to a heat exchanger using microchannel fins as a thermosyphon system.
  • Heat exchangers are thermal devices that are used to transport heat between moving fluids at different temperatures. Heat exchangers are widely used in many different applications and industries worldwide, such as aerospace, energy, heating and air conditioning, and transportation. A solid fin on a computer processor, a radiator for cooling a car or truck engine, and a condenser for an air conditioner are typical heat exchangers.
  • the ideal system should have fins of very high thermal conductivity (ideally infinite conductivity), resulting in isothermal fins and 100% fin efficiency.
  • Conduction resistance reduces the temperature of a fin so that much of the extended surface of the traditional solid fin always has a lower temperature than the heat source at the base of the fin.
  • the typical efficiency for a solid aluminum fin is about 60%. This means that, for every 100 Btu of heat transferred from a classical fin, there is the potential for an additional 67 Btu to be transferred from the same fin.
  • Many heat exchangers use solid fins to enhance heat transfer, and they are all limited by the fin efficiency factor.
  • the fin efficiency can be increased by making the temperature of the whole surface of the fin to be the highest possible value, i.e. the same temperature as the hot source (typically the base temperature of the fin) to which the fin is attached to conduct heat away.
  • the hot source typically the base temperature of the fin
  • an ideal, high efficiency fin should be isothermal all along its length with a large surface area; and the whole surface should be the highest possible temperature (the heat source temperature).
  • the fin should still be isothermal, but have the lowest possible temperature.
  • Finned heat exchangers are also used in the transport industry to enhance heat transfer; the automobile radiator is an example. As in the radiator, the cooling fluid is made to flow past the fin, either by natural or forced convection. Such fins can also be used in heat sinks for cooling of electronics and other heat sources that require efficient cooling methods.
  • the cooling requirement for automotive engines often requires a large frontal area for sufficient airflow to cool the radiator fluid. This increases the friction on the vehicle, especially at high speeds, and reduces fuel efficiency.
  • a disadvantage of conventional radiator designs is that heat transfer coefficient and heat transfer area are limited by the materials and configuration used.
  • the most commonly used number for measuring the performance of the automobile radiator is the ratio of heat transfer to the frontal area divided by the difference of the inlet temperatures of coolant and air (Q/(A f x ⁇ )). This number is typically 0.31 W/K-cm 2 for the state of the practice radiator. In the current design, it is not possible to increase this "performance" parameter cost-effectively.
  • MicroChannel tubes have been used in heat exchangers to pump a hot or cold fluid through the microchannel tubes.
  • the advantage of this approach is the simplicity of the design, and the increased heat transfer due to high surface to volume ratio in the microchannels.
  • the disadvantage is that the channels can be blocked due to scaling or due to particles in the fluid.
  • the pumping power necessary to pump sufficient fluid through small channels can be quite high due to the fact that smaller cross section passages have a greater pressure drop.
  • the pumping process itself can also introduce particulates into the microchannel flow.
  • Thermosyphons and heat pipes can carry high heat fluxes with a small temperature difference between the condenser and evaporator, and have been studied for thermal management of electronics.
  • the purpose of the invention is to produce efficient and compact heat exchangers by using highly efficient fins with microchannels formed therein that work as heat pipes or thermosyphons.
  • the overall configuration could also be used as a high efficiency heat exchanger that can replace radiators, evaporators, condensers, plate-fin heat exchangers, or heat sinks in a variety of applications.
  • the invention consists of a heat exchanger using fins that contain an array of microchannels operating as heat pipes or thermosyphons that make the fins isothermal and enhance the heat transfer between the fin and the surrounding fluid. Efficient heat exchangers using these fins can be used to either heat or cool a system. Applicants have completed the design, model and test of a more efficient, small heat exchanger working on the thermosyphon principle with microchannel tubes embedded into fins.
  • thermosyphon loop To take advantage of the very high apparent conductivity of thermosyphons, a loop, two-phase thermosyphon system was designed to keep a set of fins close to isothermal conditions.
  • the condenser of the thermosyphon loop was located within copper fins in a set of micro-channel tubes with propane as the working fluid. Experimental results showed that this integrated arrangement of thermosyphon and fins results in reasonably isothermal fins, producing high fin efficiency.
  • the specific volume of the working fluid was determined and used to characterize the system performance and stability.
  • the invention thus uses internal flow paths of a micro-channel tube as the condenser of a loop thermosyphon, while the external surface is used as a fin to be cooled by a flow of air.
  • Fins must be very thin structures, and therefore Applicants have noted that microchannels are most appropriate for flow inside the fins. Microchannels provide greater heat transfer due to greater heat transfer area per unit volume. Flows in microchannels have greater heat transfer coefficient. Therefore, the condensing fluid inside the microchannels is very effective in keeping the fin at the same temperature as the heat source.
  • the microchannel fin heat exchanger is very compact. Therefore, a radiator using such fins will reduce the frontal area of the radiator, thereby allowing more design latitude to reduce the drag coefficient of automobiles and trucks. This would increase their fuel efficiency.
  • thermosyphon design uses a passive, such as gravity, flow that eliminates the need to actively pump fluid through the microchannels, such as with a mechanical or other pump device.
  • Heat pipes likewise use capillary action, which is another mode of passive circulation.
  • the invention eliminates or reduces the pumping requirement for the fluid. Since the pressure drop in microchannels is quite high, the high pumping power for microchannel flow is eliminated.
  • the thermosyphon is a sealed unit, and therefore the possibility of flow obstruction in the microchannel due to scaling or particulates in the flow can be eliminated.
  • thermosyphon effect produces a uniform temperature in the microchannel fins. This increases the fin efficiency to almost 100%.
  • Microchannel heat pipes inside a fin can significantly increase the heat transfer of the fin, because heat pipes and thermosyphons transfer heat by phase change, unlike conventional radiators.
  • working fluid that is in vapor form condenses on the sidewalls of fluid flow passages, thereby changing to a liquid form.
  • Vaporized working fluid transports heat rapidly without the need for a pump. This process thereby maintains the microchannel sidewalls at high temperature, because the condensed liquid on the sidewalls is close to the temperature of the vaporized working fluid.
  • the micro-channels typically have a central portion that is vaporized fluid surrounding by condensed working fluid on the sidewalls of the micro-channels, but this is not necessarily so only in the micro-channels nor is it always present in the micro- channels. Therefore, with the invention the fin surface can be close to isothermal and higher heat fluxes are realized.
  • Another advantage of the invention is that pumping in the microchannels is eliminated.
  • the issue of flow blockage can also be eliminated due to the sealed working fluid - the fluid at the exterior of the sidewalls of the passages containing the working fluid does not communicate with the fluid inside the heat exchanger, and therefore no contaminants can block the flow.
  • Additional metal fins (the traditional solid, heat exchanger type) can be brazed or bonded to the microchannel fins to increase the heat transfer area.
  • a disadvantage of heat pipes is that the fins, including the heat pipes and wick inside, involve a more complex design than thermosyphons.
  • the microchannel arrays can be thermosyphons, which have a simpler design than heat pipes. Microchannels can be operated as thermosyphons with no modification of the channels. The disadvantage is that thermosyphons need to be vertical, or have sufficient vertical orientation to use gravity for driving the fluid flow. In situations where the vertical orientation is possible, the thermosyphon can be a preferred configuration, because it allows the heat exchanger to operate at very high efficiency.
  • microchannel tubes which are metal ribbon or tape-like structures containing an array of microchannels running through them.
  • the channels are preferably in the range of about 50 to about 1,000 microns in hydraulic diameter for the particular working fluid used.
  • the microchannels are used to contain the thermosyphon or heat pipe fluid which is sealed under high pressure.
  • the ribbon shape makes it feasible to use the tubes as fins over which air or any other fluid is directed, while the microchannel tubes inside these fins are used as heat pipes or thermosyphons.
  • the microchannels can be operated as a condenser or an evaporator. The desired end result is that the "microchannel tubes" perform similarly to fins, but with very high efficiency.
  • thermosyphon produces a uniform temperature in the micro-channels due to the high apparent conductivity. Since each fin contains a thermosyphon condenser, it is essentially isothermal. Vapor can move through the channels at essentially one temperature, and condenses against the sidewalls at a precise condensation temperature. The condenser is cooled by the external flow of common coolants (such as air) over the outside surface of the fin, which is heated isothermally by the gaseous refrigerant and/or condensing liquid inside. Thermosyphons also eliminate the need to pump the working fluid through the micro-channels due to gravity flow resulting from the phase change. If there is need for flexibility with respect to orientation of the fins, the thermosyphon can be replaced by heat pipes within the fins.
  • common coolants such as air
  • the invention integrates thermosyphons and fins by embedding the condenser of a thermosyphon loop within the fin. This can be achieved by using a product similar to the commercial micro-channel tubes used in the HVAC industry.
  • These micro-channel tubes made of aluminum alloys, are typically flat, ribbon-like in shape, and usually contain about 5 to 10 micro-channels per tube. They are advantageous in HVAC applications since they require less storage space, and are highly efficient.
  • aluminum alloy is the typical material used for these tubes, copper presents some advantages over aluminum.
  • the main advantage of copper for heat transfer applications is its thermal conductivity (approximately 400 W/mK), which is almost double the thermal conductivity of aluminum (approximately 235 W/mK).
  • Other advantages of copper are that it has anti-microbial properties and it is easier to join and repair than aluminum.
  • micro-channel tubes An important characteristic of micro-channel tubes is that they increase both the heat exchange and efficiency of the heat exchanger designs. This characteristic allows the micro-channel heat exchanger to be smaller and yet have the same performance as a regular heat exchanger, or to get improved performance in the same volume as a conventional heat exchanger.
  • thermosyphon system was designed by using copper micro-channel tubes that are similar to aluminum micro-channel tubes. Copper micro-channels were selected because of ease of joining and potential for improvement in heat transfer.
  • Fig. 1 shows a cross section of a copper micro-channel tube.
  • Fins can be used for both heating and cooling the fluid that is flowing across their surfaces, depending on the condensation or boiling temperature of the working fluid inside the thermosyphon or heat pipe.
  • the heating of the external fluid flow takes place when the micro-channels inside the fin are used as condensers, and the cooling of the outside flow is achieved by using the micro-channels as evaporators.
  • Fig. 1A is a view in perspective illustrating an embodiment of the preferred microchannel fin heat exchanger.
  • Fig. IB is a side view illustrating the embodiment of Fig. 1A.
  • Fig. 2 is a table that includes properties of various common working fluids for heat pipes and thermosyphons.
  • Fig. 3 is a pressure-enthalpy (P-h) diagram for propane.
  • Fig. 4 is a table illustrating the temperature of the top two positions on microchannel fins versus the bottom position temperature. The temperatures at the top, middle and bottom are almost perfectly correlated, thereby indicating an isothermal system.
  • Fig. 5 is a view in section illustrating a copper microchannel fin of the type used in the present invention.
  • Fig. 6 is a view in perspective illustrating an embodiment of the preferred copper microchannel fin heat exchanger on a loop thermosyphon prototype.
  • Fig. 7 is a view in perspective illustrating a prototype embodying the invention.
  • Fig. 8 is a side view illustrating the experimental set-up used in the experiments described herein.
  • Fig. 9 is a schematic illustration of a computer simulation showing the contours of velocity in the flow across the 3 copper micro-channel fins.
  • Fig. 10 is a schematic illustration of a computer simulation showing temperatures in the airflow across the 3 copper micro-channel fins.
  • Fig. 12 is a graphical illustration of the experimental fin temperature data obtained for three microchannel locations.
  • Fig. 13 is a graphical illustration of the data obtained for an experiment using a prototype with propane (0.007 m 3 /kg, evaporator at ⁇ 50°C, 0.5 m/s).
  • the fin temperatures are given by nine thermocouples showing temperatures in the back, middle and front fins, at top, middle and bottom locations. The reading number corresponds to time.
  • the graph shows the transient and steady state behavior of the apparatus.
  • Fig. 14 is a graphical illustration of the data obtained for an experiment using a prototype with propane (0.007 m 3 /kg, evaporator at ⁇ 50°C, 1.0 m/s).
  • the fin temperatures are given by nine thermocouples showing temperatures in the back, middle and front fins, at top, middle and bottom locations. The reading number corresponds to time.
  • the graph shows the transient and steady state behavior of the apparatus.
  • Fig. 15 is a table listing the data obtained for an experiment using a prototype with propane at 0.007 m 3 /kg.
  • Fig. 16 is a table listing the data obtained for an experiment using a prototype with propane at 0.009 m 3 /kg.
  • Fig. 17 is a table listing the data obtained for an experiment using a prototype with propane at 0.011 m 3 /kg.
  • Fig. 18 is a is a table listing energy balance results showing heat transfer to the air at two air flow velocities comparing the invention to the conventional (classical) solid fin.
  • Fig. 19 is a view in perspective illustrating an embodiment of the automotive radiator using heat pipes.
  • the heat pipes are shown approximately horizontal, whereas thermosyphons would be operated in a vertical or "close to vertical” configuration.
  • Fig. 20 is a view in perspective illustrating an end of an embodiment of a fin showing the array of micro-channels inside the copper fin.
  • Fig. 21 is a view in perspective illustrating the thermosyphon with thermocouples mounted thereon. The fins are shown exposed in the wind tunnel, while the rest of the thermosyphon loop is insulated.
  • Fig. 22 is a graphical illustration of the data obtained for an experiment, in particular the temperature history of the thermocouples during experimentation of the copper micro-channel thermosyphon system.
  • the top set of data includes all nine readings from the micro-channel tube fins. The two lines shown below represent the temperature readings of the air flow at the inlet and the outlet of the experimental wind tunnel.
  • Fig. 23 is a table listing the data obtained for an experiment using propane at 0.007 m 3 /kg for two different air flow velocities.
  • Fig. 24 is a table listing the data obtained for an experiment using propane at 0.007 m 3 /kg for air flow at 0.5 m/s, particularly listing the temperatures at the three locations (front, middle and back along the direction of air flow) of each of the three fins.
  • Fig. 25 is a table listing the data obtained for an experiment using propane at 0.011 m 3 /kg for air flow at 0.5 m/s, particularly listing the temperatures at three locations (front, middle and rear along the direction of air flow) for each of the three fins.
  • Fig. 26 is a table listing the data obtained for an experiment using propane at 0.011 m 3 /kg at two air flow velocities.
  • Fig. 27 is a graphical illustration of the data obtained for an experiment, in particular the temperature history of the thermocouples during an experiment of the copper micro-channel system without the working fluid (propane). The temperatures reach a steady state, but the micro-channel tube fins are not isothermal.
  • Fig. 28 is a table listing the data obtained for the experiments and comparing respective heat transfer for the thermosyphon and the simple fin apparatus.
  • Fig. 29 is a schematic view illustrating an alternative embodiment of the present invention.
  • thermosyphon In order to verify that the working fluid within the loop thermosyphon would circulate and produce isothermal microchannel fins with high heat transfer, a simple initial prototype was designed with microchannel and built (Figs. 1A and IB). Two embodiments are discussed below. First, a heat sink based on microchannel fins was fabricated as a prototype heat exchanger. Test results are discussed below. Second, an automotive radiator using thermosyphons and/or heat pipes is illustrated and discussed. The microchannel fins can be used to enhance the design further.
  • the inventors designed, fabricated and measured the performance of a heat sink using a microchannel fin heat exchanger. For additional details of the validation of the microchannel fin concept, a discussion is given below about the experimental design and results from a heat exchanger made from a set of three microchannel fins made from copper microchannel tubes. It was tested as a heat sink by using an electrical heater as the heat source.
  • thermosyphon fluid must be sealed under pressure so that the thermodynamic cycle is in the two phase range.
  • the fluid viscosity should be low.
  • carbon dioxide can be a preferred thermosyphon fluid in some applications because of lower viscosity.
  • thermosyphon fluid for the operating range of -30 to 50°C was selected on the basis of the Fig. 2 data for many thermosyphon fluids. Based on Fig. 2, ammonia seemed to be a good candidate, but because of its corrosiveness and toxicity it was not used in the apparatus. This is not meant to be an exclusion of ammonia for all purposes, but for the apparatus described herein. Therefore, for other conditions, such as temperature range, channel size, environment and/or material type of the thermosyphon sidewalls, ammonia or other fluids could be selected as a working fluid.
  • propane is not a common working fluid for thermosyphons, it was chosen for this project because (i) it can be efficient in the operating temperature range of -30°C to +90°C, (ii) has a relatively low global warming potential, (iii) it is readily available, and (iv) it is not toxic.
  • the thermodynamic chart of propane is shown in Fig. 3. The charging point was chosen based on the specific volume so that the system operates on a large enthalpy (h) range for maximum heat transfer. The charging and operating ranges are included in Fig. 3.
  • Another possible working fluid with acceptable operating ranges is ammonia which can be used in the range of -60°C to 100°C. However, ammonia must be handled with care because of toxicity.
  • the fin has an array of small channels which are used as heat pipes or thermosyphons.
  • the channels can be as small as 50 to 100 microns, or as large as 1,000 microns approximate hydraulic diameter.
  • Hydraulic diameter is a conventional term for a passage that is non-circular that is defined as the equivalent circular diameter of the passage after taking into consideration the effect of the non- circular passage on a fluid flowing through it.
  • the result is a fin structure that operates at isothermal conditions throughout its length (from top to bottom). This produces almost 100% fin efficiency over a range of heat transfer rates, and it improves the efficiency of the heat exchanger.
  • a "fin” is defined herein as a structure that is substantially thinner than it is wide. Typical fins are an order of magnitude (or more) wider than their thickness. For example, the fins of the prototype are about 1-3 mm thick and about 10-15 mm wide.
  • Figs. 1A, IB and 6 Tests were carried out on the prototype shown in Figs. 1A, IB and 6, and the results are shown in Fig. 4, in which the temperature variation of the fin top section (measured at the top and the middle) is plotted as a function of the temperature at the bottom location. It can be observed that the temperatures at the top and middle locations are very close to each other, and the three temperatures (top, middle and bottom) were very closely correlated by a linear relationship with a slope of 1.005, which is a variation of only 0.5% from perfect match. This is a validation of the thermosyphon principle. The temperatures remained steady at the desired power input, showing that there was no flooding or dry out in the system. This shows that the microchannel fin structure is operating as a thermosyphon loop, thus producing nearly isothermal fins. Additional checks were carried out to verify that the microchannel fins are operating as highly efficient heat transfer surfaces.
  • the copper micro-channel tubes are shown in section in Fig. 5.
  • the prototype heat exchanger was designed by using three copper micro-channel tubes as the fins and additional copper connecting tubes as shown in Figs. 1 and 6.
  • the prototype heat exchanger was then fabricated with a charging tube connected as shown in Fig. 7.
  • the fins in the prototype are aligned parallel to the direction of the flow of air, and coplanar to one another.
  • the fins could be arranged in arrays to intersect the flow of air or to be parallel to the flow of air, but not coplanar.
  • Fig. 8 shows the experimental set-up for the project.
  • the wind tunnel has a flow meter in series to measure the air flow entering the experiment.
  • Computer simulations were performed to determine the heat transfer characteristics and Figs. 9 and 10 show the top view of the velocity and the temperature as the air flows across the three copper micro-channel fins.
  • thermocouples were calibrated and used to collect data during the experiment. Experiments were run with the prototype charged at three different specific volumes (0.007, 0.009 and 0.011 m 3 /kg), two different air flow speeds (0.5 and 1.0 m/s), and a temperature of approximately 50°C at the evaporator, for a total of six experiments. The same experiments were repeated with the evaporator temperature at approximately 70°C. The main goals of these experiments were to test the design and check for dry out conditions in the prototype.
  • Figs. 15, 16 and 17 present summaries of the results for the experiments with the prototype charged with specific volumes of 0.007 m 3 /kg, 0.009 m 3 /kg, and 0.011 m 3 /kg, respectively.
  • thermosyphon configuration is especially applicable to the heat sink system where the evaporator of the loop thermosyphon can be placed on the heat source and the fins can used to dissipate the heat in the air.
  • thermosyphon loop with the fins is shown in Figs. 1 and 6.
  • the complete loop is 292 mm high, and the three copper fins (with micro-channels inside) are required to be vertically oriented for proper functioning of the thermosyphon.
  • the Fig. 1 drawing forms the basis of the fabricated thermosyphon loop shown in Fig. 7.
  • the three fins comprise the condenser section of the loop thermosyphon.
  • Each fin is 190 mm high and 13 mm wide with nine flow channels inside.
  • the fins are expected to be approximately isothermal, and the heat transfer will be enhanced.
  • the rest of the loop (shown in Figs. 1, 6 and 7) is made of copper tubing, including the evaporator section at the bottom.
  • the evaporator is heated by a heating coil.
  • the evaporator geometry should be modified so that it can be an integral part of the heat spreader, such as a computer processor.
  • the evaporator can be thermally linked to a computer process, such as by adhesive, soldering, or by forming channels through the computer processor.
  • thermalally linking means a connection that permits thermal energy to pass from a warmer object to a cooler object.
  • the highest pressure used for charging was 4.2 MPa, which gave a specific volume of 0.007 m 3 /kg.
  • the pressure is about 1.7 MPa, and the system has an overall quality of 20%, i.e., 80% of the mass is liquid.
  • the liquid density is 14.5 times the vapor density under these conditions, so the volume of the liquid is 22% of the total loop volume. This is a rather large liquid volume fraction, so dry out of the evaporator is not expected to take place.
  • partial flooding of the condenser (accompanied by single phase convection) is possible, which would reduce the heat transfer.
  • the wind tunnel shown in Fig. 8 was used.
  • the cross section for the wind tunnel is 25.4 mm x 222 mm. This cross sectional area provides approximately 12 mm on each side of the three micro-channel tubes.
  • a flow meter was attached to the wind tunnel and the air flow to the wind tunnel is provided from a pressurized air line through the flow meter.
  • a flow mixer was placed after the thermosyphon so that an average temperature of the air flow can be measured at the outlet of the wind tunnel.
  • the heat loss from the flow to the walls of the wind tunnel was estimated and found to be negligible, particularly because of the small increase in the temperature of the air flow.
  • thermocouples were used to measure the temperature along the length of the copper micro-channel fins; three thermocouples were placed at the bottom, middle and top of each tube. The thermocouple locations are shown in Fig. 21. These thermocouples were used to monitor and record the temperatures as a function of time until a steady state was reached.
  • the temperature at the bottom of the three micro-channel tube fins can be taken to be the evaporator temperature since they were placed next to the junction of the micro-channel tube and the top of the evaporator section.
  • the bottom thermocouples on the downstream side were slightly cooler, probably due the interaction of the airflow and the system geometry.
  • all three fins were close to isothermal when the thermosyphon reached steady state; so the full lengths of three micro-channel tubes were approximately at the temperature of the evaporator.
  • thermocouples A set of matched thermocouples was carefully selected and a comparative calibration check was performed over the temperature range of 25 °C to 75 °C. Special emphasis was given to the nine thermocouples that measure the temperature of the micro- channel tubes, and the thermocouples that measure the inlet and outlet air temperatures. It was determined that over the calibration range of 25 °C to 75 °C, the thermocouples that were to be used at the air inlet and outlet differed in their readings by no more than 0.06°C; and in the expected range of operation (-25 °C), they differed by approximately o.orc.
  • thermocouples selected for the micro-channel tubes compared well in the calibration, with their differences having a standard deviation of 0.2°C in the range of 25 °C to 75 °C; and only 0.1 °C when the upper limit was 50°C. Therefore these thermocouples were almost identical in their output values, and they provided a good evaluation of the temperature variations along the length of the micro-channels. Because the micro-channels were nearly isothermal, the matched sets of thermocouples showed almost identical values.
  • thermocouples that measured the copper micro-channel temperatures (marked "prototype") showed an average temperature of 53.7°C.
  • the air inlet temperature was 22°C, and the outlet temperature was 24.8°C.
  • thermosyphon behavior is clearly observed.
  • the thermocouples attached to the micro-channel tube fins indicated a nearly uniform temperature throughout the heat up period and steady state, with a standard deviation of 0.2°C at the steady state (-53.7 °C).
  • the evaporator temperature is not well defined because of the heater attached to this section.
  • the average temperature of the nine thermocouples can be considered to be representative of the evaporator temperature, which is at the bottom of the fin, since the fins were almost isothermal.
  • the steady state values are shown in Fig. 23.
  • the micro- channels seem to behave more isothermally at the lower flow rate, but the standard deviations are less than 1% of the evaporator temperature for both flow rates. With the evaporator above 70°C, the standard deviations are higher, but dry out was not detected even at this higher temperature.
  • Fig. 23 shows the results for an evaporator temperature of approx. 54°C, and an airflow of 0.5 m/s.
  • the thermocouples on the micro-channel tube fin in the front shows the most deviation. This is probably due to the fact that this fin experiences the full cooling effect of the incoming air.
  • the second and third micro-channel tube fins have a temperature variation of 0.1 °C, which is the standard deviation observed in the calibration process.
  • Fig. 26 summarizes results for this lower liquid volume fraction (11 ) of propane in the thermosyphon loop.
  • Fig. 27 shows the resulting temperature history, and even though a reasonably steady state is attained, the temperature of the fins varies along the length as well as the location of the fin in the air flow path.
  • thermosyphon loop had better performance when the propane density (or liquid volume fraction) was lower. But the difference was less at higher air flow rates.
  • the heat transfer increased by 45% to 63%, depending upon the amount of propane used in the loop, and the air flow rates. This should not be taken as an accurate measure of the enhancement over classical fin, since these fins are partly hollow.
  • the improvement with higher specific volume of 0.011m 3 /kg (lower liquid fraction in the thermosyphon loop) is an indication that the condenser section was probably partially flooded due to higher volume fraction of liquid at the lower specific volume of 0.007 m 3 /kg. However, dry out phenomena was absent in all the experimental runs.
  • thermosyphon-fin system by embedding the condenser section of the thermosyphon within a set of copper micro- channel tubing used as fins.
  • Propane was used as the working fluid for the thermosyphon, with the liquid volume fraction quantified by determination of the specific volume.
  • the fins were shown to be nearly isothermal due to the thermosyphon effect, and significant improvement in fin performance was demonstrated.
  • the performance improved when the liquid volume fraction was reduced from 22% to 11% of the thermosyphon loop volume, with condenser flooding as a possible cause for the difference. Since specific volume (or liquid volume fraction) of a thermosyphon can be measured at the superheated state, this approach can be very useful in designing the thermosyphon to operate in an optimum range between the extremes of flooding and dry out.
  • thermosyphon/heat pipe is another embodiment of the thermosyphon/heat pipe.
  • the use of heat pipes or thermosyphons as fins can produce a new design of a radiator.
  • the design can be further improved by using the microchannel fins as discussed below.
  • thermosyphons or heat pipes such that the thermosyphons will be immersed in a radiator chamber where the coolant flows across the outside the thermosyphon tubes.
  • the top of the thermosyphon tubes will be exposed to airflow.
  • the thermosyphon tubes should be vertically oriented. If heat pipes are used, the tubes do not have to be vertically oriented.
  • the thermosyphons need not be straight, and can be substituted by heat pipes if required.
  • the microchannel fins described herein can be used to make the radiator, which conventionally uses a large number of traditional fins.
  • the new design (Fig. 29) is thermally linked, such as by physically mounting it, to a thermosyphon that has its own working fluid in the microchannel fins.
  • a thermosyphon that has its own working fluid in the microchannel fins.
  • Such a system can be used to extract heat efficiently from the car radiator or other part of the car cooling system, and can be used in series or parallel with other similar or identical thermosyphons to increase the thermal transfer.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Geometry (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

La présente invention se rapporte à un échangeur de chaleur efficace et compact, un thermosiphon par exemple, comprenant des ailettes dans lesquelles sont formés des microcanaux. La matrice de microcanaux améliore le transfert de chaleur entre les ailettes et le fluide qui circule au-dessus des ailettes. La phase gazeuse du fluide de travail, du propane par exemple, se condense sur les parois latérales du condenseur à mesure que la chaleur est éliminée, et la phase gazeuse s'étend centralement sur sensiblement la longueur totale des microcanaux. On obtient ainsi des ailettes isothermes qui améliorent le transfert de chaleur grâce à l'optimisation de la différence de température entre le fluide de travail et le fluide qui circule au-dessus des ailettes.
PCT/US2010/055285 2009-11-03 2010-11-03 Echangeur de chaleur à ailettes microcanal WO2011056860A1 (fr)

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US25751309P 2009-11-03 2009-11-03
US61/257,513 2009-11-03

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110505793A (zh) * 2019-08-23 2019-11-26 昆明理工大学 一种基于磁力的强化对流换热的微通道装置及方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020056908A1 (en) * 1999-11-12 2002-05-16 Michael Philip Brownell Heatpipesink having integrated heat pipe and heat sink
US20090056916A1 (en) * 2007-08-27 2009-03-05 Abb Research Ltd Heat exchanger

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020056908A1 (en) * 1999-11-12 2002-05-16 Michael Philip Brownell Heatpipesink having integrated heat pipe and heat sink
US20090056916A1 (en) * 2007-08-27 2009-03-05 Abb Research Ltd Heat exchanger

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110505793A (zh) * 2019-08-23 2019-11-26 昆明理工大学 一种基于磁力的强化对流换热的微通道装置及方法

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