The disclosed embodiments relate to heat exchangers and more specifically to fin plates connected to tubes in heat exchangers.
In most evaporator and condenser applications with refrigerant-to-air heat transfer equipment, the airside convective resistance to heat transfer is dominant, at 75% or more of the total thermal resistance. To minimize this resistance finned surfaces are used. Wavy fin surface is one of such surfaces which have relatively higher frost tolerance. Air flow behind a tube may separate and result in a wake. The flow separation and wake contributes to a pressure drop and less efficient heat transfer.
Disclosed is a double wave fin plate for a fin-tube heat exchanger, comprising of: one half-plate having one perimeter edge with one cut-out forming one portion of a tube connector; another half-plate having another perimeter edge with another cut-out forming another portion of the tube connector; the one perimeter edge and the other perimeter edge are connected to one another about each cut-out to form the fin plate and the tube connector; one surface waveform is formed on the one half-plate; another surface waveform is formed on the other half-plate, and the one surface waveform is disposed at an angle to the other surface waveform in the fin plate.
In addition to one or more of the above disclosed aspects or as an alternate each half-plate is rectangular.
In addition to one or more of the above disclosed aspects or as an alternate each tube connector is circular.
In addition to one or more of the above disclosed aspects or as an alternate the one surface waveform is perpendicular to the other surface waveform in the fin plate.
In addition to one or more of the above disclosed aspects or as an alternate each surface waveform is sinusoidal, triangular, trapezoidal or corrugated.
In addition to one or more of the above disclosed aspects or as an alternate one peak or one trough from each surface waveform on each half-plate converges at a center of the tube connector.
In addition to one or more of the above disclosed aspects or as an alternate each of the surface waveforms is pitched so that each half-plate includes at least two peaks and two troughs.
In addition to one or more of the above disclosed aspects or as an alternate: a height of each of the peaks and each of the troughs of each of the surface waveforms is the same: and a distance between each of the peaks and each of the trough in each of the surface waveforms is the same.
In addition to one or more of the above disclosed aspects or as an alternate a fin plate seam is formed where the one perimeter edge and the other perimeter edge abut, and one end of the fin plate seam forms one of the peaks.
In addition to one or more of the above disclosed aspects or as an alternate another end of the fin plate seam forms one of the troughs.
In addition to one or more of the above disclosed aspects or as an alternate a peak-side edge of the fin plate is defined between one pair of corners of the fin plate that are adjacent the one end of the fin plate seam; and the one pair of corners are on ones of the peaks.
In addition to one or more of the above disclosed aspects or as an alternate a trough-side of the fin plate is defined between another pair of corners of the fin plate that are adjacent the other end of the fin plate seam: and the other pair of corners are on respective ones of the troughs.
A system is disclosed comprising a plurality of the fin plates having one or more of the above disclosed aspects arranged in a grid.
In addition to one or more of the above disclosed aspects or as an alternate the plurality of fin plates are arranged so that the trough-side edges of each of the fin plates is closer to one side of the system and the peak-side edge of each of the fin plates is closer to another side of the system.
In addition to one or more of the above disclosed aspects or as an alternate the plurality of the fin plates are arranged in an in-line grid, with ones of the fin plates distributed among a plurality of rows that are mutually parallel, and a plurality of columns that are mutually parallel, wherein the plurality of rows and the plurality of columns are mutually perpendicular.
In addition to one or more of the above disclosed aspects or as an alternate the plurality of the fin plates are arranged on a diagonal grid with ones of the fin plates distributed among a plurality of rows that are mutually parallel, and a plurality of columns that are mutually parallel, wherein the plurality of columns are angled relative to the plurality of rows.
In addition to one or more of the above disclosed aspects or as an alternate a fin plate seam of one fin plate is aligned with an outside edge of another fin plate.
In addition to one or more of the above disclosed aspects or as an alternate the system includes a plurality of tubes distributed among the plurality of fin plates.
Further disclosed is a method of directing gas flow over a fin plate that surrounds a tube, comprising directing gas flow over a plurality of surface waveforms formed on the fin plate, wherein the plurality of surface waveforms are disposed at an angle one another.
In addition to one or more of the above disclosed aspects or as an alternate the method includes directing the gas flow from a trough-side edge of the fin plate to a peak-side edge of the fin plate, wherein the peak-side edge comprises three mutually spaced peaks and the trough-side edge includes three mutually spaced troughs.
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.
The condenser assembly 20 and evaporator assembly 30 may each include a heat exchanger 82, more clearly illustrated in
At least one fin sheet 90 may be connected to the tube pack 84 for dissipating heat. Turning to
With the above typical type of fin sheet 90, airflow about the tube risers 85 may create airflow wakes behind the tube risers 85. This may result in a pressure drop and reduced heat transfer with the tube risers 85.
Turning now to
The perimeter edges 140 are connected to one another about a tube connector 160 to form the fin plate 100. The tube connector 160 may also be provided as half sections that are formed each the respective half plate.
One surface waveform 170a is formed on the one half-plate 130a. Another surface waveform 170b is formed on the other half-plate 130b. The surface waveforms may be generally referred to as 170. The surface waveforms 170 may be sinusoidal, triangular, trapezoidal, etc. The surface waveforms 170 are disposed at an angle to one another on the fin plate 100. For example, one trough 175a1 of the one surface waveform 170a may be at an angle 176 to another trough 175b1 of the other surface waveform 170b. In one embodiment the angle 176 is approximately ninety degrees so that the surface waveforms 170 are mutually perpendicular. A trough from each of the surface waveforms 170 may intersect in the center of the tube connector 160.
Each of the surface waveforms 170 is pitched so that the half-plates 130 each include at least two of the troughs and two peaks. The toughs in the one half-plate 130a are generally referenced as 175a and the troughs in the other half-plate are generally referenced as 175b. The peaks in the one half-plate 130a are generally referenced as 180a and the peaks in the other half-plate are generally referenced as 180b. A height of each of the peaks 180a and 180b and troughs 175a and 175b of each of the surface waveforms 170 may be the same. A distance 200 between each of the peaks 180a and 180b and troughs 175a and 175b in each of the surface waveforms 170 may be the same.
A fin plate seam 210 is formed where the one perimeter edges 140 abut. The surface waveforms 170 are configured so that except for the cutouts 150, the fin plate seam 210 is a continuous seam. One end 215a of the fin plate seam 210 may be along one of the peaks and another end 215b of the fin plate seam 210 may be along one of the troughs. That is, the one end 215a of the fin plate seam 210 is higher than the other end 215b of the fin plate seam 210.
A peak-side edge 230a of the fin plate 100 is defined between one pair of corners 235a of the fin plate 100 that are adjacent the one end 215a of the fin plate seam 210. The one pair of corners 235b are also on respective ones of the peaks. Thus, the peak-side edge 230a has three mutually spaced peaks or portions of peaks. A trough-side edge 230b of the fin plate 100 is defined between another pair of corners 235b of the fin plate 100 that are adjacent the other end 215b of the fin plate seam 210. The other pair of corners 235n are on respective ones of the troughs. Thus, the trough-side edge 230b has three mutually spaced troughs or portions of troughs. As can be appreciated, when assembled in a grid of tubes, the corners 235a on the peak-side edge 230a of the fin plate seam 210 are higher than the corners 235b on the trough-side edge 230b of the fin plate seam 210.
The above fin plate 100 induces minimized airflow wakes, if any, behind the tube risers 85, in a direction that is downstream with respect to airflow. This results in a minimized, if any, pressure drop and more efficient heat transfer with the tube risers 85.
Turning to
Turning to
As seen in
Turning to
In sum the above disclosure provides a plurality of waves on the either side of a tube, and these waves are at an angle, such as 45 degrees, to the gas (air) flow. This configuration of the wave facilitates the air to flow radially towards the tube, which is the prime heat transfer area. This directed flow reduces a potential wake area of the tube. Thus, pressure drop is reduced and heat transfer capabilities may be enhanced. The configuration of the embodiments is applicable to condenser and evaporator application. It is noted that evaporators tend to work under frosting conditions and the disclosed embodiments are relatively frost tolerant.
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/US2020/049370, filed Sep. 4, 2020, which claims the benefit of U.S. Provisional Application No. 62/896,139, filed Sep. 5, 2019, both of which are incorporated by reference in their entirety herein.
Filing Document | Filing Date | Country | Kind |
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PCT/US2020/049370 | 9/4/2020 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2021/046326 | 3/11/2021 | WO | A |
Number | Name | Date | Kind |
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20130087318 | Nakano | Apr 2013 | A1 |
20160123681 | Honma | May 2016 | A1 |
Number | Date | Country |
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496733 | Apr 1930 | DE |
3018439 | May 2016 | EP |
54140253 | Oct 1979 | JP |
57104185 | Jun 1982 | JP |
0626778 | Feb 1994 | JP |
Entry |
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International Search Report; International Application No. PCT/US2020/049370; dated Sep. 4, 2020; dated Nov. 12, 2020; 5 pages. |
Written Opinion; International Application No. PCT/US2020/049370; dated Sep. 4, 2020; dated Nov. 12, 2020; 9 pages. |
Number | Date | Country | |
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20220307774 A1 | Sep 2022 | US |
Number | Date | Country | |
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62896139 | Sep 2019 | US |