This disclosure relates generally to heat exchangers and, more particularly, to a microchannel heat exchanger for use in heat pump applications.
One type of refrigerant system is a heat pump. A heat pump can be utilized to heat air being delivered into an environment to be conditioned, or to cool and typically dehumidify the air delivered into the indoor environment. In a basic heat pump, a compressor compresses a refrigerant and delivers it downstream through a refrigerant flow reversing device, typically a four-way reversing valve. The refrigerant flow reversing device initially routes the refrigerant to an outdoor heat exchanger, if the heat pump is operating in a cooling mode, or to an indoor heat exchanger, if the heat pump is operating in a heating mode. From the outdoor heat exchanger, the refrigerant passes through an expansion device, and then to the indoor heat exchanger, in the cooling mode of operation. In the heating mode of operation, the refrigerant passes from the indoor heat exchanger to the expansion device and then to the outdoor heat exchanger. In either case, the refrigerant is routed through the refrigerant flow reversing device back into the compressor. The heat pump may utilize a single bi-directional expansion device or two separate expansion devices.
In recent years, much interest and design effort has been focused on the efficient operation of the heat exchangers (indoor and outdoor) in heat pumps. High effectiveness of the refrigerant system heat exchangers directly translates into the augmented system efficiency and reduced life-time cost. One relatively recent advancement in heat exchanger technology is the development and application of parallel flow, microchannel or minichannel heat exchangers, as the indoor and outdoor heat exchangers.
These parallel flow heat exchangers are provided with a plurality of parallel heat transfer tubes, typically of a non-round shape, among which refrigerant is distributed and flown in a parallel manner The heat exchanger tubes typically incorporate multiple channels and are oriented substantially perpendicular to a refrigerant flow direction in the inlet and outlet manifolds that are in communication with the heat transfer tubes. Heat transfer enhancing fins are typically disposed between and rigidly attached to the heat exchanger tubes. The primary reasons for the employment of the parallel flow heat exchangers, which usually have aluminum furnace-brazed construction, are related to their superior performance, high degree of compactness, structural rigidity, and enhanced resistance to corrosion.
The growing use of low global warming potential refrigerants introduces another challenge related to refrigerant charge reduction. Current legislation limits the amount of charge of refrigerant systems, and heat exchangers in particular, containing most low global warming potential refrigerants (classified as A2L substances). Microchannel heat exchangers have a small internal volume and therefore store less refrigerant charge than conventional round tube plate fin heat exchangers. In addition, the refrigerant charge contained in the manifolds of the microchannel heat exchanger is a significant portion, about a half, of the total heat exchanger charge. As a result, the refrigerant charge reduction potential of the heat exchanger is limited.
According to an embodiment of the present disclosure, a heat exchanger is provided including a first manifold, a second manifold separated from the first manifold, and a plurality of heat exchanger tube arranged in spaced parallel relationship fluidly coupling the first and second manifolds. A first end of each heat exchange tube extends partially into an inner volume of the first manifold and has an inlet formed therein. A distributor is positioned within the inner volume of the first manifold. At least a portion of the distributor is arranged within the inlet formed in the first end of one or more of the plurality of heat exchange tubes.
In addition to one or more of the features described above, or as an alternative, in further embodiments the first manifold is configured to receive at least a partially liquid refrigerant
In addition to one or more of the features described above, or as an alternative, in further embodiments a height of the first manifold is less than a width of the first manifold
In addition to one or more of the features described above, or as an alternative, in further embodiments the first manifold is asymmetric about a horizontal plane extending there through.
In addition to one or more of the features described above, or as an alternative, in further embodiments the inlet formed in the first end is generally complementary to a contour of the distributor.
In addition to one or more of the features described above, or as an alternative, in further embodiments the inlet extends over only a portion of a width of the heat exchanger tube.
In addition to one or more of the features described above, or as an alternative, in further embodiments the distributor has an increased wall thickness to reduce the inner volume of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments wherein the distributor occupies between about 20% and about 60% of the inner volume of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments the distributor occupies between about 30% and about 50% of the inner volume of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments a porous structure is arranged within the inner volume of the manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments the distributor is arranged within the porous structure.
In addition to one or more of the features described above, or as an alternative, in further embodiments the porous structure has a porosity between about 30% and about 70%.
In addition to one or more of the features described above, or as an alternative, in further embodiments the porosity of the porous structure is non-uniform.
In addition to one or more of the features described above, or as an alternative, in further embodiments the porosity of the porous structure is increased to have localized flow resistance.
In addition to one or more of the features described above, or as an alternative, in further embodiments the porosity of the porous structure changes uniformly along the length of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments the porous structure includes a plurality of cavities. Each cavity is configured to receive the first end of one of the plurality of heat exchanger tubes.
In addition to one or more of the features described above, or as an alternative, in further embodiments the first manifold is one of an inlet manifold and an intermediate manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments a spacer is positioned adjacent the distributor. The spacer is configured to set a position of the distributor within the inner volume of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments the spacer is configured to contact at least one of the plurality of heat exchanger tubes.
In addition to one or more of the features described above, or as an alternative, in further embodiments the spacer is configured to contact a portion of the first manifold inner wall.
In addition to one or more of the features described above, or as an alternative, in further embodiments the spacer extends over a portion of a length of the distributor.
In addition to one or more of the features described above, or as an alternative, in further embodiments the spacer includes a plurality of protrusions extending over at least a portion of a length of the distributor.
In addition to one or more of the features described above, or as an alternative, in further embodiments the distributor further comprises a groove formed in an exterior surface thereof. The groove and an interior wall of the first manifold form a flow passage between a first manifold section and a second manifold section.
In addition to one or more of the features described above, or as an alternative, in further embodiments the groove comprises a plurality of separate grooves.
In addition to one or more of the features described above, or as an alternative, in further embodiments the groove comprises an interconnected groove.
In addition to one or more of the features described above, or as an alternative, in further embodiments the groove comprises a spiral pattern along a circumference of the distributor.
In addition to one or more of the features described above, or as an alternative, in further embodiments the groove is configured such that a fluid flowing through the groove is not directly injected into any of the plurality of heat exchanger tubes.
In addition to one or more of the features described above, or as an alternative, in further embodiments the flow direction imparted to a fluid flowing through the groove is not parallel with one or more of the plurality of heat exchanger tubes.
In addition to one or more of the features described above, or as an alternative, in further embodiments the groove comprises a plurality of grooves. A total cross-sectional flow area of the plurality of grooves is less than a cross-sectional flow area of the first manifold.
In addition to one or more of the features described above, or as an alternative, in further embodiments the total cross-sectional area is between 50% and 200% of a cross-sectional flow area of the first manifold section.
The subject matter, which is regarded as the present disclosure, is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the present disclosure are apparent from the following detailed description taken in conjunction with the accompanying drawings in which:
The detailed description explains embodiments of the present disclosure, together with advantages and features, by way of example with reference to the drawings.
An example of a vapor compression system 20 is illustrated in
Referring now to
The heat exchanger 30 may be configured in a single pass arrangement, such that refrigerant flows from the first header 32 to the second header 34 through the plurality of heat exchanger tubes 36 in the flow direction indicated by arrow B (
Referring now to
As known, a plurality of heat transfer fins 50 may be disposed between and rigidly attached, usually by a furnace braze process, to the heat exchange tubes 36, in order to enhance external heat transfer and provide structural rigidity to the heat exchanger 30. Each folded fin 50 is formed from a plurality of connected strips or a single continuous strip of fin material tightly folded in a ribbon-like serpentine fashion thereby providing a plurality of closely spaced fins 52 that extend generally orthogonal to the flattened heat exchange tubes 36. Heat exchange between the fluid within the heat exchanger tubes 36 and air flow A, occurs through the outside surfaces 44, 46 of the heat exchange tubes 36 collectively forming the primary heat exchange surface, and also through the heat exchange surface of the fins 52 of the folded fin 50, which form the secondary heat exchange surface.
An example of a cross-section of a conventional manifold 60, such as manifold 32 or 34 for example, is illustrated in
Referring now to
As illustrated in
The width of the manifold 60 must be at least equal to or greater than a width of the heat exchanger tubes 36 received therein. By positioning a portion of the distributor 70 within the inlet 56 formed at the end 54 of the heat exchanger tubes 36, the overall height of the manifold 60 may be reduced. As a result, the cross-section of the manifold may be asymmetrical about a horizontal plane. For example, the contour curvature of an upper portion 64 and a lower portion 66 of the manifold 60 may be substantially different. As shown in the non-limiting embodiment illustrated in
Referring now to
Referring now to
In another embodiment, illustrated in
The porous structure 80 may be integrally formed with the manifold 60, or alternatively, may be a separate removable sub-assembly inserted into the inner volume 62 of the manifold 60. The porous structure 80 may be combined with any of the previously described systems having a reduced inner volume. For example, a distributor 70 having an increased wall thickness may be inserted into the porous structure 80, or the porous structure 80 may be added to a manifold 60 having a reduced height.
The vapor compression system 20 can be used in a heat pump application. In such applications, the vapor compression system may encompass auxiliary devices such as an accumulator, charge compensator, receiver, air management systems, or a combination including at least one of the foregoing. For example, one or more air management systems can be utilized to provide the airflow over an indoor and/or outdoor heat exchanger (e.g., condenser 24, evaporator 28, or an auxiliary heat exchanger configured to thermally communicate with the refrigerant circuit). The one or more air management systems can facilitate heat transfer interaction between the refrigerant circulating throughout the refrigerant circuit and the indoor and/or outdoor environment respectively.
Referring now to
The spacer 90 can have any shape. For example, a cross-sectional shape of the spacer 90 can include circular, elliptical, or any polygonal shape having straight or curved sides. In one embodiment, the shape of the distributor 70 may be complementary to, and configured to contact, a portion of the manifold 60 or a tube 36 (e.g., contacting a solid portion adjacent to a port of a multiport tube, such as a web material between ports of a multiport tube) based on the overall distance between the spacer 90 and the tubes 36.
With reference now to
The one or more grooves 92 formed in the distributor 70 are generally arranged at an angle to each of the plurality of heat exchanger tubes 36 such that one or more of the grooves do not directly face a corresponding tube 36. As a result, refrigerant from the grooves 92 is not directly injected into the plurality of tubes 36. The configuration of each groove, including the size and cross-sectional shape thereof, may be selected to control a flow of refrigerant from each groove 92 to a corresponding heat exchanger tube or tubes 36.
The distributor 70 can separate the inner volume of a manifold into a first manifold section 94 and a second manifold section 96. The volume of the first manifold section 94 may be less than or equal to the volume of the second manifold section 96. The one or more grooves 92 can define one of more flow passages between the first manifold section 94 and the second manifold section 96. A total cross-sectional flow area of the one or more grooves 92 of the distributor 70 is generally less than the cross-sectional area of the manifold 60. In one embodiment, the total cross-sectional flow area of the one or more grooves 92 is between about 50% and about 200% of the cross-sectional area of a first manifold section 94 (see
The various methods for reducing the inner volume 62 can provide significant benefits to the system at minimal additional cost. By reducing the inner volume 62 of a manifold 60 (e.g., an inlet, exit, or intermediate manifold) of a microchannel heat exchanger 20 the refrigerant charge of the heat exchanger 20 can be correspondingly reduced. Furthermore, the present methods can be employed while maintaining or improving the refrigerant distribution to the tubes 36 of the heat exchanger. In addition, such heat exchangers 20 are compatible for use with lower global warming potential refrigerants.
While the present disclosure has been particularly shown and described with reference to the exemplary embodiments as illustrated in the drawings, it will be recognized by those skilled in the art that various modifications may be made without departing from the spirit and scope of the present disclosure. Therefore, it is intended that the present disclosure not be limited to the particular embodiment(s) disclosed as, but that the disclosure will include all embodiments falling within the scope of the appended claims.
This application is a continuation application of U.S. application Ser. No. 15/504,994, filed Feb. 17, 2017, which is a National Stage Application of PCT/US2015/045866, filed Aug. 19, 2015, which claims the benefit of U.S. provisional patent application Ser. No. 62/161,056 filed May 13, 2015 and U.S. provisional patent application Ser. No. 62/039,154 filed Aug. 19, 2014, the entire contents of which are incorporated herein by reference.
Number | Date | Country | |
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62161056 | May 2015 | US | |
62039154 | Aug 2014 | US |
Number | Date | Country | |
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Parent | 15504994 | Feb 2017 | US |
Child | 16399770 | US |