The present disclosure relates generally to a vapor compression system. More specifically, the present disclosure relates to a control system for a vapor compression system having a multichannel heat exchanger.
In a multichannel heat exchanger or multichannel heat exchanger coil, a series of tube sections are physically and thermally connected by fins. The fins are configured to permit airflow through the multichannel heat exchanger and promote heat transfer to a circulating fluid, such as water or refrigerant, that is being circulated through the multichannel heat exchanger. The tube sections of the multichannel heat exchanger extend within the multichannel heat exchanger. Each tube section has several tubes or channels that circulate the fluid. The outside of each tube section may be a continuous surface with a generally oval or generally rectangular shape.
Multichannel heat exchangers may be used in residential, industrial or commercial heating, ventilation, air conditioning and refrigeration environments or other suitable vapor compression systems. A vapor compression system may include a compressor, a condenser, an expansion valve, and an evaporator to facilitate heat transfer in a cooling mode or heating mode. In vapor compression systems involving heat transfer, the condenser may operate as a heat exchanger.
Under low-ambient conditions, multichannel heat exchangers may be unable to maintain sufficient pressure, which can prevent proper operation of the vapor compression system.
This disclosure is related to a vapor compression system that circulates a fluid through a closed loop interconnecting a compressor, a first heat exchanger, a flow-restricting expansion device, and a second heat exchanger. The system further includes a vessel in a first fluid communication and a selective second fluid communication with the loop between the compressor and the first heat exchanger with each of the first and second fluid communication configured to receive fluid from the loop. The vessel is in a third fluid communication with the first heat exchanger configured to provide fluid to the first heat exchanger. In response to a predetermined ambient temperature surrounding the system, the second fluid communication is selectively opened to provide an increased fluid flow from the vessel to the first heat exchanger.
A further embodiment relates to a control system for a vapor compression system that circulates a fluid through a closed loop interconnecting a compressor, a first heat exchanger, a flow-restricting expansion device, and a second heat exchanger. The control system further includes a vessel in a first fluid communication with the loop between the compressor and the first heat exchanger to receive fluid from the loop. The vessel is in a selective second fluid communication with the loop between an outlet of the first heat exchanger and an inlet of the second heat exchanger. The vessel is in a third fluid communication with the first heat exchanger to provide fluid to the first heat exchanger. In response to a predetermined ambient temperature surrounding the system, the second fluid communications is selectively opened to provide an increased fluid flow from the vessel to the first heat exchanger.
A yet further embodiment relates to a method of controlling a vapor compressor system that circulates a fluid through a closed loop interconnecting a compressor, a first heat exchanger, a flow-restricting expansion device, and a second heat exchanger. The method includes providing a vessel in a first fluid communication with the loop between the compressor and the first heat exchanger to receive fluid from the loop. The vessel is in a selective second fluid communication with at least one of: the loop between the compressor and the first heat exchanger; and the loop between the first and second heat exchanger; the second fluid communication to provide fluid to the vessel. The method further includes providing the vessel in a third fluid communication with the first heat exchanger to provide fluid to the first heat exchanger. The method further includes enabling each of the second and third fluid communication during operation of the compressor at less than a predetermined ambient temperature surrounding the system.
Referring to
Referring to
An embodiment of heat exchanger 110 is shown in
It should be noted that the present discussion makes use of the term “multichannel” tubes, coils or “multichannel heat exchanger” to refer to arrangements in which heat transfer tubes include a plurality of flow paths between manifolds that distribute flow to and collect flow from the tubes. A number of other terms may be used in the art for similar arrangements. Such alternative terms might include “microchannel” (sometimes intended to imply having fluid passages on the order of a micrometer and less), and “microport”. Other terms sometimes used in the art include “parallel flow” and “brazed aluminum”. However, all such arrangements and structures are intended to be included within the scope of the term “multichannel”. In general, such “multichannel” tubes will include flow paths disposed along the width or in a plane of a generally flat, planar tube, although, again, the invention is not intended to be limited to any particular geometry unless otherwise specified in the appended claims. For example, U.S. application Ser. No. 11/863,677, filed Sep. 28, 2007, which is assigned to Applicant, is hereby incorporated by reference in its entirety.
A first hot-gas line 104 provides a flow path between discharge line 102 and with a vessel 106, sometimes referred to as a receiver, to receive refrigerant. In one embodiment, the connection for first hot-gas line 104 to vessel 106 is proximate to an upper portion of vessel 106. Line 104 provides supplemental hot refrigerant vapor to vessel 106 during operation at low ambient temperatures, for example, about 30 degrees F. to about 40 degrees F. It is to be understood that upper and lower ranges can exceed these bounds in some embodiments. A solenoid valve 105 controls refrigerant flow through first hot-gas line 104. A second hot-gas line 108 also connects discharge line 102 and vessel 106. In one embodiment, the connection for second hot-gas line 108 is proximate to a lower portion of vessel 106. Line 108 provides a continuous flow of refrigerant vapor to vessel 106 whenever compressor 100 is operating. A refrigerant line 112 connects a lower portion of vessel 106 to the return end of heat exchanger 110. Under normal operating conditions, line 112 will deliver a flow of refrigerant from vessel 106 to heat exchanger 110 upstream of the subcooling section of heat exchanger 110. That is, for a two-pass heat exchanger 110, the end of line 122 opposite vessel 106 connects with heat exchanger 110 prior to the second pass (subcooling section) of the heat exchanger. In one embodiment, the location of the connection of line 122 and heat exchanger 110 is between the inlet and the outlet of heat exchanger 110, at which connection the refrigerant typically exists in a two-phase state in the heat exchanger.
As further shown, a layer of insulating material 126 substantially surrounds vessel 106. In one embodiment, insulating material 126 is closed-cell foam that is both water-resistant and weather-resistant and is capable of withstanding a wide range of temperatures. Closed-cell foam insulation works particularly well for cooler temperatures, and in one embodiment, is available in flexible sheets with different thickness, such as ¾ inch. A heater 128 is used to warm vessel 106. In one embodiment, heater 128 is a flexible electric heater that is encapsulated in silicone rubber and secured to the outside surface of the bottom of vessel 106, such as by adhesive, and then covered by insulating material 126.
In one embodiment, it has been found that a heater 128 having a heating capacity of about 100 watts is sufficient for a vessel 106 construction with outside dimensions of about 6 inches in diameter and a length of about 72 inches with about ¾ inch layer of insulating material 126 surrounding the vessel. For the exemplary vessel 106 embodiment, a nominal diameter of first hot-gas line 104 with the solenoid valve may be about ⅜ inch. A diameter of second hot-gas line 108 may be about ¼ inch. A length of lines 104, 108 may be from about 4 feet to about 12 feet. In the exemplary construction, the coil dimensions of heat exchanger 110 (see coils 34,
As shown in
Inverter 142 is optional, but may be preferred for systems with one or two condenser fans 127. In systems with four or more condenser fans 127, it is usually possible to control condenser pressure by simply staging the number of operating fans 127, and use of an inverter 142 would typically result only in increased system cost and complexity.
During automatic pump-down, liquid-line solenoid valve 154 closes while compressor 100 continues to operate. The refrigerant condenses in heat exchanger 110 and backs up from the heat exchanger through refrigerant line 112 for storage in vessel 106. Likewise, for manual servicing or preparation for shipping, a technician can operate compressor 100 with manual service valve 152 closed to pump the refrigerant charge in the vessel for storage. Liquid-line solenoid valve 154 is normally open during a manual pump-down.
In one embodiment, vessel 106 is cylindrical with an inside diameter of less than 6 inches, which is not subject to the ASME pressure vessel code. In one embodiment, vessel 106 is preferably constructed of steel pipe with steel end pieces welded together to form a strong container for refrigerant.
In an alternate embodiment, as shown in
In response to low-ambient conditions surrounding vapor compression system 800, valves 802 and 806 are opened, opening lines 112 and 804 to permit the flow of refrigerant from vessel 106, ensuring that the adequate heat exchanger 110 (condenser) pressure is maintained for proper operation of the vapor compression system at low ambient temperatures. In one embodiment, with an ambient temperature of 0 degrees F., vessel 106 operated properly without inclusion of either a heater 128 or a layer of insulating material 126 surrounding vessel 106. It is to be understood that in other embodiments, the vapor compression system may continue to operate properly in ambient temperatures less than 0 degrees F., with further reduction in ambient temperature possible with the addition of heater 128 and/or a layer of insulating material 126 surrounding vessel 106.
In one embodiment, valves 802, 806 may be electronic expansion valves or thermal expansion valves. In one embodiment, one or more of the thermal expansion valves 802, 806 include a bulb (not shown) that is connected, such as via a capillary tube (not shown), to an upper portion of the valves. The bulb is disposed in fluid communication with the suction line to the compressor, the pressure difference between the refrigerant in the bulb and the refrigerant in the heat exchanger (evaporator) being used to open the valve. If a migrating charge is used for the bulb, then a heater may be fitted to the top of the head of the thermal expansion valve to improve operation at lower ambient temperatures. In alternate embodiments, a non-migrating charge may be used instead of the connection with the compressor suction line, or an electronic expansion valve may be used. In a further embodiment, the embodiments of
Table 1 summarizes the control logic for the vessel heater and the solenoid that controls hot gas to the vessel for the vapor compression system construction of
Regulation of the amount of refrigerant liquid in vessel 106 is desirable to maintaining control of condensing pressure, which control is necessary for operating refrigeration equipment at low ambient temperatures. As previously described in an earlier embodiment, a continuously open line connection 108 between compressor 100 and vessel 106 may be adequate for maintaining control of the amount of refrigerant liquid in vessel 106 during normal ambient temperatures. At lower ambient temperatures (for example, less than about 30 degrees F. to about 40 degrees F.), refrigerant liquid tends to remain in vessel 106 during start-up. Maintaining too much liquid refrigerant in vessel 106 also tends to reduce condensing pressure and results in little or no subcooling of the refrigerant, both of which prevent an adequate amount of refrigerant from reaching heat exchanger 116 through the expansion valve 120, reducing cooling capacity of the system.
One partial solution is warm vessel 106 before start-up at low ambient temperatures. In one embodiment, vessel 106 may be warmed using a heater 128 or a combination of a heater 128 and insulation layer 126. In one embodiment, the open refrigerant connections are disposed adjacent to the lower portion of vessel 106, minimizing convection of refrigerant inside of vessel 106. The exemplary arrangement of receiver lines 108, 112 may increase the temperature of vessel 106 and reduce the amount of refrigerant liquid contained within vessel 106 at start-up, both of which assist with start-up at low ambient temperature conditions. However, large heaters may require excessive power input, which increases energy use and adds cost for larger control transformers. In addition, heaters alone may not be able to provide adequate control over the vessel at lower ambient temperature conditions.
Another partial solution is to warm vessel 106 with additional hot refrigerant vapor. The additional hot refrigerant vapor warms vessel 106 and helps to move liquid away from vessel 106 during start-up of vapor compression system 10. However, additional hot refrigerant vapor alone may be inadequate to assure reliable operation under all start-up conditions.
The combination of hot refrigerant vapor and heaters 128 appears to provide superior performance. The exemplary combination provides reliable start up even at 0 degrees F. ambient temperature conditions without requiring excessive heater power. The solution appears to provide an optimum combination of cost and performance for vessel 106 constructions, such as shown in
Table 2 summarizes the control logic for vessel 106 and solenoids 802, 806 that control the discharge connections or lines 112 and 804 between vessel 106 and heat exchanger 110 (condenser), and between the vessel and heat exchanger 116 (evaporator), respectively (
A control point of about 40 degrees F. worked well with the exemplary embodiment. A deadband of several degrees F. may be included to prevent rapid cycling of the valve.
Start up conditions usually create the most challenging operating conditions associated with control of refrigerant at lower ambient temperatures. In some cases it may be necessary to open the solenoid during start-up to prevent excess accumulation of liquid refrigerant in the receiver. A timer may be used to energize the solenoid for about the first several minutes (for example, 5 minutes) of operation of the refrigerant circuit, regardless of ambient temperature. At lower ambient temperatures, the solenoid would continue to operate as described above.
In an alternate embodiment, a more sophisticated control may be used that optimizes the operation of the solenoid as a function of ambient conditions and start up conditions. In a further embodiment, the liquid level in the vessel may be measured directly and used to control the operation of the solenoid.
While only certain features and embodiments of the invention have been shown and described, many modifications and changes may occur to those skilled in the art (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters (e.g., temperatures, pressures, etc.), mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter recited in the claims. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. It is, therefore, to be understood that the appended claims are intended to cover all such modifications and changes as fall within the true spirit of the invention. Furthermore, in an effort to provide a concise description of the exemplary embodiments, all features of an actual implementation may not have been described (i.e., those unrelated to the presently contemplated best mode of carrying out the invention, or those unrelated to enabling the claimed invention). It should be appreciated that in the development of any such actual implementation, as in any engineering or design project, numerous implementation specific decisions may be made. Such a development effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure, without undue experimentation.
This application claims the benefit of U.S. Provisional Application No. 60/957,940, filed Aug. 24, 2007, which Application is hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US08/73962 | 8/22/2008 | WO | 00 | 2/5/2010 |
Number | Date | Country | |
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60957940 | Aug 2007 | US |