The present disclosure relates to an evaporatively cooled refrigeration system for refrigerants with a low critical temperature. More particularly, the present disclosure relates to a refrigeration system with an evaporatively cooled condenser and/or gas cooler for refrigerants with a low critical temperature.
Heat rejection devices are widely used in many applications to exchange heat and/or provide cooling. Particular applications for heat rejection devices may include refrigeration for supermarkets, process cooling in industry, and climate control in buildings. While heat rejection is generally well understood, a number of different principles are briefly discussed for reference. A supercritical fluid (SCF) is any substance at a temperature and pressure above its critical point, where distinct liquid and gas phases do not exist. The SCF expands to fill its container like a gas but with a density similar to that of a liquid. Typically, refrigeration systems using a refrigerant with a low critical temperature utilize a transcritical cycle to reject heat to the ambient environment. The transcritical cycle is a closed thermodynamic cycle where the refrigerant goes through both subcritical and supercritical states. While many substances have a critical temperature, only substances that have a critical temperature within a useful range of temperatures and pressures are suitable for use as refrigerants.
Traditionally, chlorofluorocarbons (CFCs) have been utilized as refrigerants. However, due to the negative impact CFCs have on the environment, other refrigerant chemistry is needed.
Accordingly, it is desirable to provide an evaporative heat rejection device for refrigerants with a low critical temperature that can offer improved performance or efficiency and/or without undesirably impacting the environment, increasing the size of the unit, the manufacturing cost of the unit, and/or operating cost of the unit.
The foregoing needs are met, at least in part, by the present disclosure where, in one embodiment an evaporative heat rejection device is disclosed.
An embodiment provides an evaporatively cooled refrigeration system. The evaporatively cooled refrigeration system includes a refrigerant, a gas/liquid separator, an expansion valve in fluid connection to the gas/liquid separator, an evaporator to receive the refrigerant from the expansion valve, a compressor configured to compress the refrigerant in fluid connection to the evaporator, and a gas cooler in fluid connection to the compressor. The gas cooler includes an indirect heat exchanger to convey the refrigerant and facilitate heat from the refrigerant and a spray system to spray an evaporative coolant on the indirect heat exchanger. The gas cooler optionally includes a direct heat exchanger. Evaporative cooling provided by the evaporative coolant on the indirect heat exchanger is configured to cool the refrigerant below a dry bulb ambient air temperature.
Another embodiment relates to a device that includes a gas cooler. The gas cooler includes an indirect heat exchanger and a spray system. The indirect heat exchanger has a coil to convey a refrigerant and facilitate heat removal from the refrigerant. The spray system is designed to spray an evaporative coolant on the indirect heat exchanger. The evaporative cooling is provided by the evaporative coolant on the coil and is configured to cool the refrigerant below a dry bulb ambient air temperature.
In yet another embodiment, an evaporatively cooled refrigeration system comprises a distribution system for providing an evaporative coolant to an indirect heat exchanger. The indirect heat exchanger includes a coil configured to cool a refrigerant flowing through the coil below a dry bulb ambient air temperature by transferring heat from the refrigerant to the evaporative coolant that passes over the coil. The evaporatively cooled refrigeration system further includes a pressure relief valve configured to automatically open at a pressure of about 1600 pounds per square inch (PSI) or greater. The indirect heat exchanger is configured to withstand a pressure of at least about 1000 PSI.
In this respect, before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of construction and to the arrangements of the components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments and of being practiced and carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein, as well as the abstract, are for the purpose of description and should not be regarded as limiting.
As such, those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the designing of other structures, methods and systems for carrying out the several purposes of the present invention. It is important, therefore, that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
In general, embodiments of an evaporatively cooled refrigeration system described herein refer to various forms of evaporative condensers, gas coolers, and other such heat transfer/rejection devices for use with a refrigerant having a low critical temperature. For the purposes of this disclosure, the term, “low critical temperature” refers to a substance having a critical temperature between about 0° C. and about 100° C., or 0° C. and 100° C. More particularly, the term, “low critical temperature” refers to a substance having a critical temperature between about 10° C. and about 40° C., or 10° C. and 40° C.
One or more embodiments of the evaporatively cooled refrigeration system may be designed to operate as correlated to the ambient wet-bulb temperature of the air, as opposed to the ambient dry-bulb temperature. Throughout many locations, wet-bulb temperatures may be less than 27° C. throughout the majority of the year.
The evaporatively cooled refrigeration system may be configured to operate and stay below the critical point of carbon dioxide (CO2). CO2 has a low critical temperature (31° C.) and high critical pressure (73.8 Bar). Using ammonia as a reference, the critical temperature and critical pressure of ammonia is 132° C. and 113 Bar, respectively. In warm climates, the low critical temperature of CO2 means the system would operate beyond the critical point using a transcritical CO2 system. Transcritical operation results in a significant higher compressor energy consumption, higher compressor first cost, and less compressor life.
Furthermore, in comparison to embodiments utilizing evaporative cooling, air cooled and adiabatic cooled CO2 condensing/cooling technologies require significantly greater heat rejection energy and/or much larger heat transfer surface area. It is an advantage of some embodiments that the evaporatively cooled refrigeration system is configured to operate with either condensing refrigerant vapor below its critical temperature, or cool refrigerant supercritical fluid above its critical temperature.
Moreover, CO2 has a low toxicity and low environmental impact as compared with conventional refrigerants. For example, the carbon footprint of CO2 is 1 global-warming potential (GWP). Further CO2 has an Ozone depletion potential (ODP) of 0. However, common refrigerants such as R-12 and R-22 have a GWP of 10,800 and 1,760, and an OPD of 0.73 and 0.034, respectively. Thus, there is a movement in the refrigeration industry to phase out the use of high GWP and ODP refrigerants.
Embodiments of the evaporatively cooled refrigeration system may include evaporative condenser coils configured to operate at internal pressures of about 120 Bar. The materials of the evaporative condenser coils are designed to be sufficiently corrosion-resistant to operate in a wetted environment. For example, the coils may be comprised of stainless steel, copper, galvanized steel, aluminum, or other similar materials. If the system operates in the supercritical state, the evaporative cooling technology is designed to operate at a low energy consumption compared to air cooled and adiabatic cooled systems, from both the compression and heat-rejection processes.
In some warm climates, a refrigeration system using the CO2 may be configured to operate as a transcritical system. When the high side of the CO2 refrigeration system operates in the supercritical state, it consumes significantly more energy from both the compression and the supercritical fluid (gas) cooling processes. By being configured to provide an evaporative cooled high side heat rejection, embodiments of the disclosure facilitate operation in the subcritical state for as many hours during a year as possible. If the evaporatively cooled refrigeration system operates in the supercritical state due to an elevated environmental temperature, for example, the evaporative cooling technology facilitates a lower system energy consumption compared to air cooled and adiabatic cooled systems.
Referring now to
Referring specifically to
At step 2, liquid refrigerant may be drawn from the bottom of the separator 102. For example, located at the bottom of the separator 102, a port provides an exit for the refrigerant to be drawn from the separator 102 as a saturated liquid, typically around −1° C. and 33 Bar.
At step 3, the flow of refrigerant is provided to one or more medium temperature evaporators 106. For example, the liquid refrigerant is conveyed through an expansion valve 108 and enters the one or more medium temperature evaporators 106. Preferably, the refrigerant experiences a limited amount of expansion as it passes through the expansion valve 108 and enters the one or more medium temperature evaporators 106. For example, the refrigerant may be nearly saturated at about −6.7° C. and 28 Bar as it enters the one or more medium temperature evaporators 106. As is generally understood, once the refrigerant enters the one or more medium temperature evaporators 106, the refrigerant absorbs heat. For example, the one or more medium temperature evaporators 106 may be designed to have a rejection heat load of about 510,600 British thermal units per hour (BTU/hr).
It is to be understood that although
At step 4, the refrigerant exits the one or more medium temperature evaporators 106. Having gained heat in the one or more medium temperature evaporators 106, the refrigerant is provided in the form of a vapor having a small amount of superheat of less than 10° F., and at a pressure of about 28 Bar.
At step 5, the refrigerant may be conveyed to one or more low temperature evaporators 110. For example, the liquid refrigerant may be conveyed from the separator 102 to a low temperature expansion value 112. The flow of refrigerant is supplied to the one or more low temperature evaporators 110 at about −28.9° C. and 13.8 Bar. As is generally understood, once the refrigerant enters the one or more low temperature evaporators 110, the refrigerant absorbs heat. For example, the one or more low temperature evaporators 110 may have a rejection heat load of about 138,800 BTU/hr.
It is to be understood that although
It is to be further understood that although
At step 6, the refrigerant exits the one or more low temperature evaporators 110. For example, having gained heat in the one or more low temperature evaporators 110, the refrigerant is provided in the form of a vapor with a small amount of superheat, typically less than 10° F., and at a pressure of about 13.8 Bar. This flow of refrigerant exiting the one or more low temperature evaporators 110 provides a suction for one or more low temperature compressors 114 provided downstream of the low temperature evaporators. The flow of refrigerant is designed to be compressed by the one or more low temperature compressors 114 as described in more detail hereinbelow.
Referring again to the liquid/vapor separator 102, at step 7, a flash gas (e.g., excess vapor that has boiled off the liquid refrigerant in the separator 102) is removed from the liquid/vapor separator 102. A flash gas bypass valve 116 may be provided and is configured to meter a flow of the flash gas from the separator 102. In a particular example, the metered flow of the flash gas may be a saturated vapor provided at a pressure of about 33 Bar. The metered flow of the flash gas is then combined with an amount of compressed flow of refrigerant that is exiting the one or more low temperature compressors 114, and the combined stream is conveyed to one or more high stage compressors 118. The combined stream is designed to control or modulate the pressure of the separator 102 and the superheat supplied to the suction of the one or more high stage compressor(s) 118.
At step 8, the compressed flow of refrigerant exits the one or more low temperature compressors 114. For example, the one or more low temperature compressors 114 may have compressed the refrigerant to slightly above the high stage suction pressure, about 28.3 Bar. The refrigerant also has superheat leaving the one or more low temperature compressors 114 at around 93° C. The number of the one or more low temperature compressors 114 may depend on the needs of the embodiment. Thus, the amount of superheat leaving the one or more low temperature compressors 114 can vary.
At step 9, the flow of refrigerant is provided to one or more high stage compressors 118. In this instance, a high stage compressor head serves to converge the flow of refrigerant from the outlet of the low temperature compressor(s) 114, the outlet of the medium temperature evaporator(s) 106, and the flash gas bypass valve 116. The converged flow of refrigerant is provided to the one or more high stage compressors 118 and compressed.
It is to be understood that the evaporatively cooled refrigeration system 100 depicted herein is designed to operate at a low pressure during steps 1-9. Thus, the piping and one or more components of the portion of the evaporatively cooled refrigeration system 100 on the “low side” may be rated for low pressure environments. One of the benefits of using CO2 as a refrigerant is that the piping on the low side may be smaller than conventional refrigeration systems. For example, at −22° F., R-22 has a vapor density of about 0.43 pounds per cubic foot (lbs/ft3). Whereas, at the same temperature, CO2 has a vapor density of about 2.2 lbs/ft3. Thus, the same mass flow rate of CO2 can be transported through a smaller pipe as compared to R-22.
Referring again to
At an inlet 180 of an indirect heat exchanger 140 of the gas cooler 120, as further explained below, the coupling between the inlet 180 and the pipe leading from the high stage compressor 118 must also be able to withstand the high pressure and temperature described above. Further, the high-pressure portion of the evaporatively cooled refrigeration system 100 may comprise one or more safety relief valves configured to automatically vent at about 1600 psi. Accordingly, a pipe coupling 128 between the inlet 180 of the indirect heat exchanger 140 and the pipe leading from the high stage compressor 118 must be capable of withstanding about 1600 psi without separating or leaking.
The discharge of the high stage compressor 118 may pass through an oil separator 124. The refrigerant that is discharged from the high stage compressor(s) 118 is also provided to the inlet 180 of the gas cooler 120. The gas cooler 120 may be provided in the form of a gas condenser. The gas cooler 120 is configured to provide evaporative cooling. In some forms, an adiabatic cooler is not provided in the evaporatively cooled refrigeration system 100. In this manner, efficient cooling/condensing of refrigerants with low critical temperatures may be achieved. Primarily the throttling valve 104, along with capacity modulation of the gas cooler 120, controls the pressure at this point while the refrigerant is passing through the cooler. During transcritical operation, when the ambient dry bulb temperature, or adiabatically pre-cooled air dry bulb temperature is greater than the CO2 critical temperature (31° C.), an air-cooled or adiabatically cooled refrigeration system (as compared to the evaporatively cooled refrigeration system 100 shown in
As best seen in
As shown in
In some embodiments, the cooled evaporative fluid may be collected in a second distribution system 160 comprising an intermediate basin 138 and a second plurality of nozzles 162 configured to spray the evaporative fluid onto the indirect heat exchanger 140. However, in some other embodiments, the evaporatively cooled refrigeration system 100 may not include the intermediate basin 138. Thus, the evaporative fluid may pass through the direct heat exchanger 136 and then be provided for use with the indirect heat exchanger 140 without flowing through a secondary distribution system. In some examples, the indirect heat exchanger 140 may include one or more cooling/condensing coils, a plate heat exchanger, or the like. The indirect heat exchanger 140 may further include a drift eliminator 220. The indirect heat exchanger 140 is configured to cool the refrigerant flowing through the tube side of the indirect heat exchanger 140 by transferring heat from the refrigerant to the evaporative fluid. Thus, the evaporative fluid increases in temperature after contacting the indirect heat exchanger 140. The refrigerant may be provided to and enter the indirect heat exchanger 140 at the inlet 180 and exit the indirect heat exchanger 140 at an outlet 182. To aid in the transfer of heat via the indirect heat exchanger 140, the air movement device 134 may draw air in from a lower air inlet 240 and through the indirect heat exchanger 140.
A collection basin 142 may be provided to collect the hot evaporative fluid that has passed over the indirect heat exchanger 140. A recirculation system may then convey the hot evaporative fluid from the collection basin 142 to the hot water basin 132 in a well understood manner. In one non-limiting example, the recirculation system includes a pump 170 and piping 172. In this way, the evaporative fluid may be cycled over the gas cooler 120. However, due to evaporation, a supply of fresh water may be supplied to the gas cooler 120 to maintain a desired evaporative fluid volume. For example, the evaporative fluid may be cycled through the evaporatively cooled refrigeration system 100 at least three times before the evaporative fluid may need to be removed from the evaporatively cooled refrigeration system 100 through blowdown.
In most climates, the ambient wet bulb is 27° C. or lower. The highest temperature and pressure point of the evaporatively cooled refrigeration system 100 hence would be able to stay below the CO2 critical point. Referring again to
As shown in
In contrast, at step 11′, the refrigerant exits the gas cooler 120 as a liquid. In subcritical mode, the refrigerant at this point is a liquid and heat has been removed from the refrigerant via the gas cooler 120.
At step 12, the refrigerant cycle is completed as the refrigerant exits the outlet of the throttling valve 104. When passing through the throttling valve 104, the flow of refrigerant from the gas cooler 120 has been reduced in pressure to the pressure substantially equivalent to, or equal to the pressure within the liquid/vapor separator 102. In transcritical mode, the refrigerant here is a mixture of liquid and gas. In subcritical mode, the refrigerant is 100% liquid. Thus, piping downstream of the throttling valve 104 may be rated for lower pressure operation.
In many climates, the annual operating cost of the evaporatively cooled refrigeration system 100 is lower than the annual operating cost of a conventional adiabatic cooled refrigeration system with respect to the cost of water usage and energy usage in the instance where each of the evaporatively cooled refrigeration system 100 and the conventional adiabatic cooled refrigeration system provide substantially the same cooling capacity. For example, for a climate C1 with a mean coincident wet bulb temperature of MCWB1, a dry bulb temperature of DB1, and a wet bulb temperature of WB1, having water cost WC1 USD/Gal and energy cost EC1 USD/kWh, the conventional adiabatic cooled refrigeration system has a total annual cost of TACA1 to provide X BTU output. In contrast, in the same climate C1 and providing the same X BTU output, the evaporatively cooled refrigeration system 100 has a total annual cost of TACE1 which is less than TACA1. In C1, the annual energy use AEU1 of the evaporatively cooled refrigeration system 100 is less than the annual energy use AEU2 of the conventional adiabatic cooled refrigeration system. In some climates, the annual water use AWU1 of the evaporatively cooled refrigeration system 100 is higher than the annual water use AWU2 of the conventional adiabatic cooled refrigeration system. However, AEU1×EC1+AWU1×WC1 is less than AEU2×EC1+AWU2×WC1, and, therefore, TACE1 is less than TACA1. Accordingly, the cost savings in annual energy use of the evaporatively cooled refrigeration system 100 outweighs the cost of any additional water use. This is found to be true for a wide range of energy costs EC1, water costs WC1, and climates C1.
In
Turning to
Each of the adiabatic and the evaporative cooler systems of
By comparing the values in Table 500 to Table 600, it can be seen that the evaporative cooler system has a lower Annual Operation Cost compared to the adiabatic system. As shown in Table 600, the evaporative cooler system may have a lower annual operation cost because the evaporative cooler may have a lower power requirement for a fan, such as the air movement device 134 of
A summary of the Overall Annual Cost of the Adiabatic System of
Referring back to
In one scenario, the controller 103 may adjust the fan speed of the air movement device 134 of
In yet another scenario, the controller 103 may adjust the speed of the low temperature compressor 114 and/or the high stage compressor 118. For example, the evaporatively cooled refrigeration system 100 may have a low heat load, which does not require one or more of the compressors 114, 118 to operate at full speed. Thus, the controller 103 may be configured to reduce the speed of the low temperature compressor 114 and/or the high stage compressor 118. Therefore, the energy needs of the evaporatively cooled refrigeration system 100 may be reduced.
It is to be understood that the above examples are merely for illustrative purposes and are not to be considered limiting. The controller 103 may be configured to adjust multiple components of the evaporatively cooled refrigeration system 100 simultaneously.
Additionally, it is to be understood that carbon dioxide is one example of a suitable refrigerant for use in the evaporatively cooled refrigeration system 100. Other refrigerants having similar properties to that of carbon dioxide may be used. For example, the evaporatively cooled refrigeration system 100 may use refrigerants having one or more of the following properties: a low ODP (near zero), a low GWP, a low critical temperature (less than 45° C.), and a high critical pressure (greater than 700 psig).
The many features and advantages of the invention are apparent from the detailed specification, and thus, it is intended by the appended claims to cover all such features and advantages of the invention which fall within the true spirits and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention. For example, the direct heat exchanger 136 could be placed below the indirect heat exchanger 140 and still maintain the advantages of the invention with the condensing and/or cooling of the refrigerant with reference to the wet bulb temperature by virtue of the evaporative cooling.
This application is a Non-Provisional application and claims priority under 35 U.S.C. § 119 to U.S. Provisional Application Ser. No. 63/224,600, filed on Jul. 22, 2021, titled, “EVAPORATIVELY COOLED REFRIGERATION SYSTEM”, the disclosure of which is incorporated herein by reference in its entirety.
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20170122624 | Zha et al. | May 2017 | A1 |
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Number | Date | Country | |
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63224600 | Jul 2021 | US |