Exemplary embodiments pertain to the art of heat exchangers, and more particularly to rotary wheel heat recovery ventilators.
Heat exchangers are utilized in ventilation systems installed in, for example, residential, commercial and industrial spaces to extract and remove heat and/or moisture from one airstream and transfer that heat energy and/or moisture to a second airstream. In particular, rotary wheel heat exchangers, or heat recovery ventilators, are known wherein a wheel rotates in a housing through countervailing streams of exhaust and fresh air, in the winter extracting heat and moisture from the exhaust stream and transferring it to the fresh air stream. In the summer rotary wheel heat exchangers extract heat and moisture from the fresh air stream and transfer it to the exhaust stream, preserving building air conditioning while providing desired ventilation.
Heat transfer enhanced heat recovery wheels present an opportunity for the development of significantly more compact designs of ventilation systems, reducing material and fabrication cost. However, a number of challenges exist for the application of new designs: Wheel effectiveness, pressure drop, material cost and design complexity are some of the key challenges.
In one embodiment, a heat exchanger includes a housing, the housing defining a first airflow chamber through which a first airflow is directed and a second airflow chamber through which a second airflow is directed. A heat recovery wheel is located in the housing and is rotatable about a wheel axis. The heat recovery wheel includes a wheel rim defining an outer perimeter of the heat recovery wheel, and a plurality of wheel passages located between the wheel rim and the wheel axis. The plurality of wheel passages are at least partially defined by one or more passage fins. At least a portion of a passage fin of the plurality of passage fins extends non-parallel to the wheel axis between a first wheel end of the heat recovery wheel and a second wheel end of the heat recovery wheel. The plurality of wheel passages are configured for flow of the first airflow and the second airflow therethrough for thermal energy exchange between the first airflow and the second airflow.
Additionally or alternatively, in this or other embodiments the at least one passage fin extends linearly non-parallel to the wheel axis from the first wheel end to the second wheel end.
Additionally or alternatively, in this or other embodiments the at least one passage fin extends in a chevron shape from the first wheel end to the second wheel end.
Additionally or alternatively, in this or other embodiments the at least one passage fin includes a first fin portion extending from the first wheel end parallel to the wheel axis, a second fin portion extending from the second wheel end parallel to the wheel axis, circumferentially offset from the first fin portion, and a third fin portion connecting the first fin portion to the second fin portion. The third fin portion is non-parallel to the wheel axis.
Additionally or alternatively, in this or other embodiments circumferentially adjacent passage fins are non-parallel.
Additionally or alternatively, in this or other embodiments the at least one passage fin is discontinuous between the first wheel end and the second wheel end.
Additionally or alternatively, in this or other embodiments the plurality of wheel passages are arranged in a plurality of layers from the wheel axis to the wheel rim.
Additionally or alternatively, in this or other embodiments a parting sheet separates radially adjacent layers of the plurality of layers.
In another embodiment, a heat recovery wheel for a heat exchanger includes a wheel rim defining an outer perimeter of the heat recovery wheel, and a plurality of wheel passages located between the wheel rim and the wheel axis. The plurality of wheel passages are at least partially defined by one or more passage fins. At least a portion of a passage fin of the plurality of passage fins extends non-parallel to the wheel axis between a first wheel end and a second wheel end. The plurality of wheel passages are configured for flow of a first airflow and a second airflow therethrough for thermal energy exchange between the first airflow and the second airflow.
Additionally or alternatively, in this or other embodiments the at least one passage fin extends linearly non-parallel to the wheel axis from the first wheel end to the second wheel end.
Additionally or alternatively, in this or other embodiments the at least one passage fin extends in a chevron shape from the first wheel end to the second wheel end.
Additionally or alternatively, in this or other embodiments the at least one passage fin includes a first fin portion extending from the first wheel end parallel to the wheel axis, a second fin portion extending from the second wheel end parallel to the wheel axis, circumferentially offset from the first fin portion, and a third fin portion connecting the first fin portion to the second fin portion, the third fin portion non-parallel to the wheel axis.
Additionally or alternatively, in this or other embodiments circumferentially adjacent passage fins are non-parallel.
Additionally or alternatively, in this or other embodiments the at least one passage fin is discontinuous between the first wheel end and the second wheel end.
Additionally or alternatively, in this or other embodiments the plurality of wheel passages are arranged in a plurality of layers from the wheel axis to the wheel rim.
Additionally or alternatively, in this or other embodiments a parting sheet separates radially adjacent layers of the plurality of layers.
Additionally or alternatively, in this or other embodiments passage fins of radially adjacent layers of the plurality of layers are non-parallel.
Additionally or alternatively, in this or other embodiments the plurality of passage fins are textured to enhance thermal energy transfer.
Additionally or alternatively, in this or other embodiments the plurality of passage fins are coated with one or more of an adsorbant, a hydrophobic coating or a hydrophilic coating.
Additionally or alternatively, in this or other embodiments the plurality of passage fins are formed from a metal, a polymer or a composite material.
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
Referring again to
Referring to the cross-sectional view of
Referring now to
Another embodiment of passage fin 46 configuration is illustrated in
Another embodiment of passage fin 46 configuration is illustrated in
In some embodiments, the passage fins 46 may be textured to further enhance heat transfer, and/or may be coated with an adsorbent material for moisture control in the heat recovery ventilator 10. Additionally, the passage fins 46 may be coated with a hydrophobic and/or hydrophilic coatings to enhance moisture removal. The passage fins 46 may be formed from a metallic material, or alternatively may be formed from a polymer or a composite material.
The passage fins 46 and heat recovery wheel 42 of the present disclosure provides a solution to improve heat transfer of the heat recovery wheel 42 while maintaining a compact structure of the heat recovery wheel 42, and not increasing the length of the heat recovery wheel 42 to increase the performance. Further, the configurations of heat recovery wheel 42 disclosed herein reduces cross-stream mixing of the first airflow 24 and the second airflow 30.
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/US2019/51440, filed Sep. 17, 2019, which claims the benefit of Provisional Application No. 62/733,249 filed Sep. 19, 2018, the disclosures of which are incorporated herein by reference in their entirety.
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PCT/US2019/051440 | 9/17/2019 | WO |
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WO2020/060995 | 3/26/2020 | WO | A |
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Number | Date | Country | |
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20210199387 A1 | Jul 2021 | US |
Number | Date | Country | |
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62733249 | Sep 2018 | US |