The presently disclosed embodiments generally relate to appliances for heating and cooling air, and more particularly, to a heat exchanger for use in a condensing gas-fired heating, ventilation and air-conditioning (HVAC) appliance.
A typical condensing gas-fired HVAC appliance includes a flame or burner for heating flue gases, a primary heat exchanger for transferring heat from the heated gases to the circulated air, a secondary or condensing heat exchanger for transferring heat from the discharged gas of the primary heat exchanger to the circulated air, and a blower for circulating air through an interior space (or any surrounding area).
In some instances, the secondary or condensing heat exchangers are plate-type heat exchangers made from two opposing halves or half shells. Heat is transferred from the inside, between the half shells, to the exterior of the heat exchanger. In other instances, the secondary or condensing heat exchangers are tube and fin type heat exchangers made from a number of circular tubes penetrating a number of plate fins and having good thermal contact with the fins. Heat is transferred from inside each of the circular tubes to the plate fins, thereby releasing the latent heat of vaporization of the water in the flue gas and transferring this latent heat, along with sensible heat, to the air disposed outside the heat exchanger. However, such heat exchangers require a large number of tubes penetrating the plate fins to achieve an effective heat exchange process, and thus provide a given heat exchange efficiency. Therefore, there is a need for a secondary or condensing heat exchanger that improves the heat exchange efficiency with less number of tubes.
In one aspect, a secondary heat exchanger for use in a condensing gas-fired HVAC appliance is provided. In one embodiment, the heat exchanger includes at least one plate fin, each including a plate fin surface, and at least one plate fin aperture through the plate fin surface. The heat exchanger also includes at least one conduit, including an outer conduit surface, and a non-circular transverse geometry that penetrates the at least one plate fin aperture. In at least one embodiment, the outer conduit surface is in contact with the plate fin surface. In at least one embodiment, the heat exchanger includes at least two plate fins, each plate fin placed adjacent to one another to form a plate fin spacing. In one embodiment, the plate fin spacing is less than or equal to approximately 16 plate fins per inch.
In at least one embodiment, the non-circular transverse cross-sectional geometry includes an oval. In at least one embodiment, the oval includes a substantially elliptical geometry including a major axis length and a minor axis length. In at least one embodiment, the major axis length may be approximately 1.5 times the minor axis length.
In at least one embodiment, the non-circular transverse cross-sectional geometry includes a pair of opposing side walls, each having a proximal end, and a distal end. The at least one conduit further includes a first curved wall extending between each of the opposing side wall proximal ends, and a second curved wall extending between each of the opposing side wall distal ends.
In at least one embodiment, the secondary heat exchanger includes at least one conduit including a conduit outer surface, a longitudinal conduit length, a conduit width, and a non-circular transverse cross-sectional geometry. The secondary heat exchanger further includes at least one fin affixed to the conduit outer surface.
In at least one embodiment, the non-circular transverse cross-sectional geometry of the at least one conduit includes a pair of opposing side walls, each having a proximal end, a distal end, and an opposing side wall length. The at least one conduit further includes a first curved wall extending between each of the opposing side wall proximal ends, and a second curved wall extending between each of the opposing side wall distal ends. In at least one embodiment, a tube aspect ratio is defined by the opposing side wall length divided by the conduit width, and wherein the tube aspect ratio is less than or equal to 35. In at least one embodiment, at least two conduits are placed adjacent to one another to form a conduit spacing. In at least one embodiment, a tube spacing ratio is defined by the opposing side wall length divided by the conduit spacing, and wherein the tube spacing ratio is less than or equal to approximately 18. In at least one embodiment, the opposing side wall length may be less than or equal to approximately 7 inches. In at least one embodiment, conduit width may be less than or equal to approximately 1 inch. In at least one embodiment, the conduit spacing is less than or equal to approximately 3 inches.
In at least one embodiment, the at least one fin may be affixed to at least one of the opposing side walls along the longitudinal conduit length. In at least one embodiment, the at least one fin may be substantially rectangular in shape and arranged in a geometric pattern with the at least one opposing side walls. In at least one embodiment, the geometric patter is selected from a group consisting of: triangular, rectangular, and trapezoidal.
In one aspect, a condensing gas-fired HVAC appliance is provided. The condensing gas-fired HVAC appliance includes at least one primary heat exchanger and at least one secondary heat (condensing) exchanger disposed in a casing. In at least one embodiment, the condensing gas-fired HVAC appliance further includes a fan, an inducer assembly, and a burner assembly operably coupled to one another, and disposed in the casing.
The embodiments and other features, advantages and disclosures contained herein, and the manner of attaining them, will become apparent and the present disclosure will be better understood by reference to the following description of various exemplary embodiments of the present disclosure taken in conjunction with the accompanying drawings, wherein:
For the purposes of promoting an understanding of the principles of the present disclosure, reference will now be made to the embodiments illustrated in the drawings, and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of this disclosure is thereby intended.
In at least one embodiment, as shown in
In at least one embodiment, as shown in
In at least one embodiment, as shown in
In at least one embodiment, a tube aspect ratio is defined by the opposing side wall length 115 divided by the conduit width 117, and wherein the tube aspect ratio is less than or equal to 35. In at least one embodiment, at least two conduits 112A and 112B are placed adjacent to one another to form a conduit spacing 119. In at least one embodiment, a tube spacing ratio is defined by the opposing side wall length 115 divided by the conduit spacing 119. The conduit spacing 119 governs the volume of space available for the at least one fins 118; thus, impacting both the heat transfer and the air-side pressure drop. In at least one embodiment, the opposing side wall length 115 may be less than or equal to approximately 7 inches. It will also be appreciated that the opposing side wall longitudinal length 115 may be greater than 7 inches. In at least one embodiment, conduit width 117 may be less than or equal to approximately 1 inch. It will also be appreciated that the conduit width 117 may be greater than approximately 1 inch. In at least one embodiment, the conduit spacing 119 is less than or equal to approximately 3 inches. It will also be appreciated that the conduit spacing is greater than approximately 3 inches.
While the example in
In at least one embodiment, the at least one fin 118 may be affixed to at least one of the opposing side walls 120 and 122 along the longitudinal conduit length 116. In at least one embodiment, the at least one fin 118 may be substantially rectangular in shape and arranged in a geometric pattern with the at least one opposing side walls 120 and 122. In at least one embodiment, the geometric pattern is selected from a group consisting of: triangular, rectangular, and trapezoidal. For example, a first fin 118A may have a side 136A affixed to the opposing side wall 122 (or 120) of a conduit 112A. The opposite, congruent side 138A of the first fin 118A may be affixed to a side 138B of a second fin 118B to form an apex 140 above the opposing side wall 122 (or 120). In some embodiments, the apex 140 may be affixed to an opposing side wall 120 (or 122) of another conduit 112B. The opposite, congruent side 136B of the second fin 118B may be affixed to the opposing side wall 122 (or 120) of the conduit 112A. It will be appreciated that the non-circular transverse cross-sectional geometry increases the internal surface area of the at least one conduit 112 as compared to a conduit having the same cross-sectional area and a circular geometry; thus, enhancing the heat transfer between the at least one conduit 112 and the at least one fin 118. It will be appreciated that the thickness of each of the at least fins 118 may vary due to the required heat transfer from each of the at least one fins 118 to an airflow stream passing through the at least one fins 118 and a pressure drop of the airflow stream through the at least one fins 118.
According to at least one embodiment,
It will be appreciated that the at least one conduit 18 and 112 include a non-circular transverse cross-sectional geometry to increase the internal surface area therein as compared to a conduit having the same cross-sectional area and a circular geometry; thus, providing an increased area for heat transfer and increasing the steady-state efficiency of the condensing gas-fired HVAC appliance 200.
While the invention has been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only certain embodiments have been shown and described and that all changes and modifications that come within the spirit of the invention are desired to be protected.
The present application is related to, and claims the priority benefit of, U.S. Provisional Patent Application Ser. No. 61/929,653 filed Jan. 21, 2014, the contents of which are hereby incorporated in their entirety into the present disclosure.
Number | Date | Country | |
---|---|---|---|
61929653 | Jan 2014 | US |