HEAT RECOVERY VENTILATOR
20210254901 · 2021-08-19
Inventors
- Dhruv Chanakya Hoysall (West Hartford, CT, US)
- ABBAS A. ALAHYARI (Glastonbury, CT, US)
- Jack Leon Esformes (Jamesville, NY, US)
Cpc classification
F28F2245/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02P70/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F28F2245/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D19/041
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D19/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
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 arranged in a plurality of radial layers relative to a wheel central axis. Each layer is defined by a first shaped material having a first cross-sectional shape and a second shaped material assembled to the first shaped material, the second shaped material having a second cross-sectional shape. Radially adjacent layers of the plurality of layers are secured directly to one another, and 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.
Claims
1. A heat recovery wheel for a heat exchanger, comprising: 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 arranged in a plurality of radial layers relative to a wheel central axis, each layer defined by: a first shaped material having a first cross-sectional shape; and a second shaped material assembled to the first shaped material, the second shaped material having a second cross-sectional shape; wherein radially adjacent layers of the plurality of layers are secured directly to one another; and wherein 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.
2. The heat recovery wheel of claim 1, wherein the first cross-sectional shape is the same as the second cross-sectional shape.
3. The heat recovery wheel of claim 1, wherein the first cross-sectional shape is different from the second cross-sectional shape.
4. The heat recovery wheel of claim 1, wherein the first cross-sectional shape is a first chevron pattern.
5. The heat recovery wheel of claim 1, wherein the first cross-sectional shape is a first trapezoidal pattern.
6. The heat recovery wheel of claim 1, wherein the first cross-sectional shape has a first angular alignment relative to the wheel central axis and the second cross-sectional shape has a second angular alignment different from the first angular alignment.
7. The heat recovery wheel of claim 1, wherein the first cross-sectional shape is circumferentially angularly offset from the second cross-sectional shape.
8. The heat recovery wheel of claim 1, further comprising a plurality of axially stacked layers of wheel passages relative to the wheel central axis, wherein the wheel passages of axially adjacent layers are circumferentially offset.
9. A heat exchanger, comprising: 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; and a heat recovery wheel disposed in the housing and rotatable about a wheel axis, the heat recovery wheel including: 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 arranged in a plurality of radial layers relative to a wheel central axis, each layer defined by: a first shaped material having a first cross-sectional shape; and a second shaped material assembled to the first shaped material, the second shaped material having a second cross-sectional shape; wherein radially adjacent layers of the plurality of layers are secured directly to one another; and wherein 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.
10. The heat exchanger of claim 9, wherein the first cross-sectional shape is the same as the second cross-sectional shape.
11. The heat exchanger of claim 9, wherein the first cross-sectional shape is different from the second cross-sectional shape.
12. The heat exchanger of claim 9, wherein the first cross-sectional shape is a first chevron pattern.
13. The heat exchanger of claim 9, wherein the first cross-sectional shape is a first trapezoidal pattern.
14. The heat exchanger of claim 9, wherein the first cross-sectional shape has a first angular alignment relative to the wheel central axis and the second cross-sectional shape has a second angular alignment different from the first angular alignment.
15. The heat exchanger of claim 9, wherein the first cross-sectional shape is circumferentially angularly offset from the second cross-sectional shape.
16. The heat exchanger of claim 9, further comprising a plurality of axially stacked layers of wheel passages relative to the wheel central axis, wherein the wheel passages of axially adjacent layers are circumferentially offset.
17. A method of forming a heat recovery wheel, comprising: forming a first cross-sectional shape in a first material layer; forming a second cross-sectional shape in a second material layer; assembling the first material layer directly to the second material layer thereby defining a passage layer having a plurality of wheel passages; and winding the passage layer about a central wheel axis, with radially adjacent passage layers directly abutting.
18. The method of claim 17, further comprising angularly offsetting the first material layer from the second material layer.
19. The method of claim 17, further comprising circumferentially offsetting radially adjacent passage layers.
20. The method of claim 17, wherein the first cross-sectional shape is different from the second cross-sectional shape.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] The following descriptions should not be considered limiting in any way.
[0026] With reference to the accompanying drawings, like elements are numbered alike:
[0027]
[0028]
[0029]
[0030]
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DETAILED DESCRIPTION
[0035] 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.
[0036] Referring now to
[0037] Referring again to
[0038] Referring to the cross-sectional view of
[0039] Referring now to
[0040] The first shaped material 52 and the second shaped material 58 are assembled directly to each other at an assembly section 64 (shown in
[0041] In another embodiment, shown in
[0042] When assembled at the assembly section 64, the first shaped material 52 and the second shaped material 58 are offset such that when wound or rolled to for the heat recovery wheel 32, the first trapezoidal-shaped pattern 70 is angularly offset from the second trapezoidal-shaped pattern 72. Referring now to
[0043] In some embodiments, the first shaped material 52 and/or the second shaped material 58 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 first shaped material 52 and the second shaped material 58 may be coated with a hydrophobic and/or hydrophilic coatings to enhance moisture removal. The first shaped material 52 and the second shaped material 58 may be formed from a metallic material, or alternatively may be formed from a polymer or a composite material.
[0044] The first shaped material 52 and the second shaped material 58 and heat recovery wheel 32 of the present disclosure provides a solution to improve heat transfer of the heat recovery wheel 32 while maintaining a compact structure of the heat recovery wheel 32 by not including a parting sheet of a typical heat recovery wheel 32, and not increasing the length of the heat recovery wheel 32 to increase the performance.
[0045] 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.
[0046] 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.
[0047] 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.