Exemplary embodiments pertain to the art of heating, ventilation, air conditioning and refrigeration (HVAC&R) systems. More particularly, the present disclosure relates to configurations of tube and fin heat exchangers for HVAC&R systems.
Currently, many HVAC&R systems utilize round-tube plate-fin (RTPF) heat exchangers in their evaporator sections. Due to frosting and other design considerations, these heat exchangers typically utilize rudimentary fin designs without enhancements to improve thermal energy exchange performance and efficiency, and thus need large fin surface areas to meet the performance requirements.
In general, such evaporators need large flow depths to manage exit air temperature and are overtly large, are excessively heavy and higher cost. Most common fin enhancement strategies requiring surface interruptions such as lances and louver geometries are rendered ineffective under frosting conditions due to blockage.
In one embodiment, a tube and fin heat exchanger includes a plurality of heat exchange tubes configured for flowing a refrigerant therethrough, a plurality of fins positioned such that the plurality of heat exchange tubes pass through a plurality of tube openings in the plurality of fins, and a plurality of vortex generators extending from a fin surface of the plurality of fins. The plurality of vortex generators are arranged to define nozzle like passages at the heat exchange tubes.
Additionally or alternatively, in this or other embodiments one or more vortex generators of the plurality of vortex generators are one of triangular or rectangular in shape.
Additionally or alternatively, in this or other embodiments the plurality of vortex generators are positioned at a nonzero angle of attack relative to a general direction of an airflow across the heat exchanger.
Additionally or alternatively, in this or other embodiments the angle of attack is between 5 degrees and 70 degrees.
Additionally or alternatively, in this or other embodiments a ratio of a vortex generator height from the fin surface to a span between adjacent fins of the plurality of fins is between 0.01 and 1.
Additionally or alternatively, in this or other embodiments the vortex generator has an aspect ratio of streamwise length to height from the fin surface greater than 1.
Additionally or alternatively, in this or other embodiments an upstream most end of the vortex generator is upstream from an associated tube of the plurality of heat exchange tubes.
Additionally or alternatively, in this or other embodiments the plurality of heat exchange tubes are arranged in a plurality of streamwise-extending rows.
Additionally or alternatively, in this or other embodiments the vortex generators are positioned at alternating heat exchange tubes of each streamwise-extending row.
Additionally or alternatively, in this or other embodiments the vortex generators are positioned at only an upstreammost heat exchange tube of a streamwise-extending row of the plurality of streamwise-extending rows.
Additionally or alternatively, in this or other embodiments the heat exchanger is an evaporator.
In another embodiment, a heating, ventilation, air conditioning and refrigeration (HVAC&R) system includes a compressor, a condenser fluidly connected to the compressor, and an evaporator fluidly connected to the compressor and the condenser. One or more of the evaporator or the condenser are configured as a tube and fin heat exchanger and include a plurality of heat exchange tubes configured for flowing a refrigerant therethrough, a plurality of fins located such that the plurality of heat exchange tubes pass through a plurality of tube openings in the plurality of fins, and a plurality of vortex generators extending from a fin surface of the plurality of fins. The plurality of vortex generators are arranged to define nozzle like passages at the heat exchange tubes.
Additionally or alternatively, in this or other embodiments one or more vortex generators of the plurality of vortex generators are one of triangular or rectangular in shape.
Additionally or alternatively, in this or other embodiments the plurality of vortex generators are positioned at a nonzero angle of attack relative to a general direction of an airflow across the tube and fin heat exchanger.
Additionally or alternatively, in this or other embodiments the angle of attack is between 5 degrees and 70 degrees.
Additionally or alternatively, in this or other embodiments a ratio of a vortex generator height from the fin surface to a span between adjacent fins of the plurality of fins is between 0.01 and 1.
Additionally or alternatively, in this or other embodiments the vortex generator has an aspect ratio of streamwise length to height from the fin surface greater than 1.
Additionally or alternatively, in this or other embodiments an upstream most end of the vortex generator is upstream from an associated tube of the plurality of heat exchange tubes.
Additionally or alternatively, in this or other embodiments the plurality of heat exchange tubes are arranged in a plurality of streamwise-extending rows.
Additionally or alternatively, in this or other embodiments vortex generators are located at alternating heat exchange tubes of each streamwise-extending row.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.
Referring now to
Within this vapor compression refrigerant cycle 20, the refrigerant flows in a counterclockwise direction as indicated by the arrow. The compressor 22 receives refrigerant vapor from the evaporator 24 and compresses it to a higher temperature and pressure, with the relatively hot vapor then passing to the condenser 26 where it is cooled and condensed to a liquid state by a heat exchange relationship with a cooling medium (not shown) such as air. The liquid refrigerant R then passes from the condenser 26 to an expansion device 28, wherein the refrigerant R is expanded to a low temperature two-phase liquid/vapor state as it passes to the evaporator 24. At the evaporator 24 a flow or relatively warm return air 30 is urged across the evaporator 24 by, for example, an evaporator fan 32. The return air 30 is cooled via thermal energy exchange with the refrigerant R flowing through the evaporator 24, and is flowed to a conditioned space 34, such as a room or refrigerated case, as supply air 36. The low pressure refrigerant vapor then returns to the compressor 22 where the cycle is repeated.
Referring now to
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Shown in
Referring now to the side view of
Referring again to
The embodiments of
The configurations of the present disclosure improve thermal energy performance of the evaporator 24, especially in frosting configurations. The performance improvement includes a low pressure drop penalty, in a configuration that is easily and cost-efficiently manufactured. Additionally, the overall size of the heat exchanger may be reduced for the same performance as a heat exchanger without vortex generators 48.
The term “about” is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms “a”, “an” and “the” are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms “comprises” and/or “comprising,” when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.
While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.
This application is a National Stage application of PCT/US2020/049350, filed Sep. 4, 2020, which claims the benefit of Provisional Application No. 62/896,131 filed Sep. 5, 2019, the disclosures of which are incorporated herein by reference in their entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/US2020/049350 | 9/4/2020 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2021/046314 | 3/11/2021 | WO | A |
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Number | Date | Country | |
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20210148657 A1 | May 2021 | US |
Number | Date | Country | |
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62896131 | Sep 2019 | US |