US20090173479A1 - Louvered air center for compact heat exchanger - Google Patents

Louvered air center for compact heat exchanger Download PDF

Info

Publication number
US20090173479A1
US20090173479A1 US12/221,705 US22170508A US2009173479A1 US 20090173479 A1 US20090173479 A1 US 20090173479A1 US 22170508 A US22170508 A US 22170508A US 2009173479 A1 US2009173479 A1 US 2009173479A1
Authority
US
United States
Prior art keywords
louver
centerlines
louvers
width direction
angle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/221,705
Inventor
Lin-Jie Huang
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Delphi Technologies Inc
Original Assignee
Delphi Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Delphi Technologies Inc filed Critical Delphi Technologies Inc
Priority to US12/221,705 priority Critical patent/US20090173479A1/en
Assigned to DELPHI TECHNOLOGIES, INC. reassignment DELPHI TECHNOLOGIES, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HUANG, LIN-JIE
Publication of US20090173479A1 publication Critical patent/US20090173479A1/en
Priority to US13/834,355 priority patent/US20130199760A1/en
Priority to US14/486,130 priority patent/US20150000880A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/126Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
    • F28F1/128Fins with openings, e.g. louvered fins
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/04Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
    • F28D1/053Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
    • F28D1/0535Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section

Definitions

  • a heat exchanger assembly for dissipating heat and more specifically, a heat exchanger assembly having fins.
  • a heat exchanger assembly generally includes a plurality of tubes each extending parallel to and spaced from one another for transferring heat from a refrigerant flowing through the tubes.
  • a plurality of undulating fins zigzag back and forth between adjacent ones of the tubes to define air channels.
  • Each one of the fins typically define at least one louvered portion which has a plurality of louvers each extending parallel to one another and disposed along a single axis, referred to as the louvered air center.
  • the louvers of a second louvered portion are also disposed along the same single axis.
  • the louvers are angled relative to the fin surface such that the louvers divert some of the air flowing through each of the air channels through the fin and into adjacent air channels.
  • Louvered air center performance is critical to the heat transfer rate of compact heat exchangers, such as radiator, heaters, condensers, and evaporators.
  • a typical louvered air center includes a plurality of louvered portions on each fin, e.g., a leading margin, a turn-around margin, and a trailing margin.
  • the actual airflow path in the air center can be theoretically divided into two different flow paths, louver flow and channel flow.
  • Channel flow is defined as the flow along the air channels.
  • Louver flow is defined as the flow between the louvers into adjacent air channels. The greater the percentage of air flowing between the louvers as louver flow, the greater the heat transfer and airflow efficiency.
  • louver widths For a given distance between two groups of louvers, i.e., the width of each air channel formed by the zigzagging fin, smaller louver widths result in a thinner thermal boundary layer which increases heat transfer for the assembly. On the other hand, the smaller louver widths also result in a larger gap between two adjacent groups of louvers, i.e., a larger air channel width, which results in a higher percentage of channel flow and therefore lower heat transfer performance. Accordingly, in the current heat exchanger fin designs, there is an optimum louver width for a given air channel width wherein performance cannot be further improved.
  • the invention includes a louvered portion having a plurality of first louvers each extending in a height direction along a first louver centerline as well as a plurality of second louvers each extending in the height direction along a second louver centerline.
  • the first louver centerlines are parallel to one another and disposed side by side along a first axis extending in a width direction transverse to the height direction and the second louver centerlines are parallel to one another and disposed side by side along a second axis extending in the transverse width direction.
  • the first louvers are disposed at a first angle and the second louvers are disposed at a second angle relative to the transverse width direction.
  • the second axis extends parallel to said first axis and spaced from said first axis in a length direction transverse to the height direction and the width direction.
  • the invention reduces the thermal boundary layer of each louver which improves performance while simultaneously reducing the amount of channel flow which also improves performance.
  • FIG. 1 is a perspective view of a heat exchanger assembly illustrating two fins each having a plurality of louvered portions;
  • FIG. 2 is an enlarged view of a fin of FIG. 1 illustrating the first and second louvers of one louvered portion;
  • FIG. 3 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating parallel first and second louvers;
  • FIG. 3A is an enlarged view of area 3 A in FIG. 3 ;
  • FIG. 4 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 ;
  • FIG. 5 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating parallel first, second, and third louvers;
  • FIG. 5A is an enlarged view of area 5 A in FIG. 5 ;
  • FIG. 6 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating non-parallel first and second louvers;
  • a heat exchanger assembly for dissipating heat is generally shown.
  • a plurality of tubes 20 each extend between ends in a length direction A L and between sides in a width direction A W transverse to the length direction A L for transferring heat from a refrigerant flowing through the tubes 20 .
  • the tubes 20 are parallel to one another and spaced from one another in a height direction A H transverse to the length direction A L and the width direction A W .
  • the length direction A L is perpendicular to the height direction A H and the width direction A W is perpendicular to the height direction A H and the length direction A L .
  • a plurality of fins 22 each are zigzagged back and forth in the height direction A H between adjacent ones of the tubes 20 for receiving heat from the tubes 20 .
  • the fins 22 are disposed along the length direction A L between the ends of the tubes 20 to define an air channel 24 .
  • the air channels 24 extend between the sides of the tubes 20 in the width direction A W .
  • Each one of the fins 22 define at least one louvered portion 26 to divert some of the air flowing through each of the air channels 24 , through the fin 22 and into an adjacent one of the air channels 24 .
  • the louvered portion 26 has a plurality of first louvers 28 each extending in the height direction A H along a first louver centerline CL 1 .
  • the first louver centerlines CL 1 are parallel to one another and are disposed side by side along a first axis A 1 .
  • the first axis A 1 extends in the transverse width direction A W .
  • the first louvers 28 are parallel to one another and are all disposed at a first angle ⁇ 1 relative to the transverse width direction A W .
  • the louvered portion 26 also has a plurality of second louvers 30 each extending in the height direction A H along a second louver centerline CL 2 .
  • the second louver centerlines CL 2 are parallel to one another and disposed side by side along a second axis A 2 extending in the transverse width direction A W .
  • the second louvers 30 are also parallel to one another and are all disposed at a second angle ⁇ 2 relative to the transverse width direction A W .
  • the second axis A 2 extends parallel to the first axis A 1 and is spaced from the first axis A 1 in the length direction A L , as best shown in FIGS. 3-6 .
  • each one of the second louver centerlines CL 2 is spaced from a corresponding one of the first louver centerlines CL 1 in the length direction A L by a first distance a.
  • Each one of the second louver centerlines CL 2 is also offset from the corresponding one of the first louver centerlines CL 1 in the width direction A W by a second distance b.
  • the first distance a, the second distance b, and the first angle ⁇ 1 are interrelated according to a first relationship defined as tan ⁇ 1 (a/b) ⁇ 1 .
  • FIGS. 3 and 5 illustrate an embodiment wherein the tan ⁇ (a/b)> ⁇ 1 .
  • FIGS. 4 and 6 illustrate an embodiment wherein the tan ⁇ 1 (a/b) ⁇ 1 .
  • the first distance a, the second distance b, and the first angle ⁇ 1 are interrelated according to a second relationship defined as tan ⁇ 1 (a/b) ⁇ 1 and the first angle ⁇ 1 and the second angle ⁇ 2 are interrelated according to a third relationship defined as ⁇ 1 ⁇ 2 .
  • the first angle ⁇ 1 may be equal to the second angle ⁇ 2 , as shown in FIGS. 2-5 .
  • the first angle ⁇ 1 may be different than the second angle ⁇ 2 , as shown in FIG. 6 . If the first angle ⁇ 1 is different than the second angle ⁇ 2 , as shown in FIG. 6 , the difference between the first angle ⁇ 1 and the second angle ⁇ 2 is preferably in the range of 0 to 50% of the first angle ⁇ 1 .
  • the first louver centerlines CL 1 of the first louvers 28 are each spaced equidistant from one another.
  • the second louvers 30 are each spaced equidistant from one another.
  • the louvered portion 26 has a plurality of third louvers 32 each extending in the height direction A H along a third louver centerline CL 3 .
  • the third louver centerlines CL 3 extend parallel to one another and are spaced equidistant from one another.
  • the third louvers 32 are parallel to one another and are all angled at a third angle ⁇ 3 relative to the transverse width direction A W .
  • Each of the third louvers 32 are disposed side by side along and perpendicular to a third axis A 3 .
  • the third axis A 3 extends parallel to and spaced from the second axis A 2 in the length direction A L .
  • Each one of the third louver centerlines CL 3 is spaced from a corresponding one of the second louver centerlines CL 2 in the length direction A L by the first distance a.
  • Each one of the third louver centerlines CL 3 is also offset from the corresponding one of the second louver centerlines CL 2 in the width direction A W by the second distance b.
  • Each of the third louver centerlines CL 3 are offset from corresponding ones of the second louver centerlines CL 2 in the width direction A W by the first distance a and are spaced from corresponding ones of the second louver centerlines CL 2 in the length direction A L by the second distance b.
  • the angles ( ⁇ 1 , ⁇ 2 , ⁇ 3 ) may all be equal to one another, as shown in FIG. 5 or alternatively may be different (not shown).
  • louvered portions 26 of the zigzagging fin 22 In operation, air flowing through the air channels 24 is diverted through the louvered portions 26 of the zigzagging fin 22 and into adjacent air channels 24 . Because the invention requires multiple rows of louvers 28 , 30 , 32 for each louvered portion 26 , the width of each louver may be reduced, reducing the thermal boundary layer and increasing heat transfer, without reducing the gap in the length direction A L between two parallel louvered portions 26 , i.e., without reducing the width of the air channels 24 . Accordingly, the invention surpasses the heat transfer of prior assemblies by decreasing louver width below that of the optimum width of the prior assemblies while maintaining the same air channel 24 width.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A louvered fin of a heat exchanger assembly includes a louvered portion having a plurality of first louvers each extending along a first louver centerline as well as a plurality of second louvers each extending along a second louver centerline. Each set of louver centerlines are parallel to one another and disposed side by side along a respective axis extending transversely to the centerlines. The first louvers are disposed at a first angle and the second louvers are disposed at a second angle relative to the respective axes. The two axes extend parallel to one another and are spaced from one another in a length direction transverse to the centerlines and the axes.

Description

    BACKGROUND OF THE INVENTION
  • 1. Field of the Invention
  • A heat exchanger assembly for dissipating heat and more specifically, a heat exchanger assembly having fins.
  • 2. Description of the Prior Art
  • A heat exchanger assembly generally includes a plurality of tubes each extending parallel to and spaced from one another for transferring heat from a refrigerant flowing through the tubes. A plurality of undulating fins zigzag back and forth between adjacent ones of the tubes to define air channels.
  • Each one of the fins typically define at least one louvered portion which has a plurality of louvers each extending parallel to one another and disposed along a single axis, referred to as the louvered air center. Generally, if included the louvers of a second louvered portion are also disposed along the same single axis. The louvers are angled relative to the fin surface such that the louvers divert some of the air flowing through each of the air channels through the fin and into adjacent air channels.
  • Louvered air center performance is critical to the heat transfer rate of compact heat exchangers, such as radiator, heaters, condensers, and evaporators. A typical louvered air center includes a plurality of louvered portions on each fin, e.g., a leading margin, a turn-around margin, and a trailing margin. The actual airflow path in the air center can be theoretically divided into two different flow paths, louver flow and channel flow. Channel flow is defined as the flow along the air channels. Louver flow is defined as the flow between the louvers into adjacent air channels. The greater the percentage of air flowing between the louvers as louver flow, the greater the heat transfer and airflow efficiency.
  • For a given distance between two groups of louvers, i.e., the width of each air channel formed by the zigzagging fin, smaller louver widths result in a thinner thermal boundary layer which increases heat transfer for the assembly. On the other hand, the smaller louver widths also result in a larger gap between two adjacent groups of louvers, i.e., a larger air channel width, which results in a higher percentage of channel flow and therefore lower heat transfer performance. Accordingly, in the current heat exchanger fin designs, there is an optimum louver width for a given air channel width wherein performance cannot be further improved.
  • Although the prior heat exchanger assemblies are sufficient for their intended purposes, there is a continuing need for more efficient and improved assemblies.
  • SUMMARY OF THE INVENTION
  • The invention includes a louvered portion having a plurality of first louvers each extending in a height direction along a first louver centerline as well as a plurality of second louvers each extending in the height direction along a second louver centerline. The first louver centerlines are parallel to one another and disposed side by side along a first axis extending in a width direction transverse to the height direction and the second louver centerlines are parallel to one another and disposed side by side along a second axis extending in the transverse width direction. The first louvers are disposed at a first angle and the second louvers are disposed at a second angle relative to the transverse width direction. The second axis extends parallel to said first axis and spaced from said first axis in a length direction transverse to the height direction and the width direction.
  • The invention reduces the thermal boundary layer of each louver which improves performance while simultaneously reducing the amount of channel flow which also improves performance.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Other advantages of the present invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
  • FIG. 1 is a perspective view of a heat exchanger assembly illustrating two fins each having a plurality of louvered portions;
  • FIG. 2 is an enlarged view of a fin of FIG. 1 illustrating the first and second louvers of one louvered portion;
  • FIG. 3 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating parallel first and second louvers;
  • FIG. 3A is an enlarged view of area 3A in FIG. 3;
  • FIG. 4 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1;
  • FIG. 5 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating parallel first, second, and third louvers;
  • FIG. 5A is an enlarged view of area 5A in FIG. 5;
  • FIG. 6 is a schematic view showing a cross-section of an alternative embodiment of the fins of FIG. 1 illustrating non-parallel first and second louvers;
  • DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS
  • Referring to the Figures, wherein like numerals indicate corresponding parts throughout the several views, a heat exchanger assembly for dissipating heat is generally shown. As shown in FIG. 1, a plurality of tubes 20 each extend between ends in a length direction AL and between sides in a width direction AW transverse to the length direction AL for transferring heat from a refrigerant flowing through the tubes 20. The tubes 20 are parallel to one another and spaced from one another in a height direction AH transverse to the length direction AL and the width direction AW. The length direction AL is perpendicular to the height direction AH and the width direction AW is perpendicular to the height direction AH and the length direction AL.
  • A plurality of fins 22 each are zigzagged back and forth in the height direction AH between adjacent ones of the tubes 20 for receiving heat from the tubes 20. The fins 22 are disposed along the length direction AL between the ends of the tubes 20 to define an air channel 24. The air channels 24 extend between the sides of the tubes 20 in the width direction AW.
  • Each one of the fins 22 define at least one louvered portion 26 to divert some of the air flowing through each of the air channels 24, through the fin 22 and into an adjacent one of the air channels 24.
  • As shown in FIG. 2, the louvered portion 26 has a plurality of first louvers 28 each extending in the height direction AH along a first louver centerline CL1. The first louver centerlines CL1 are parallel to one another and are disposed side by side along a first axis A1. The first axis A1 extends in the transverse width direction AW. The first louvers 28 are parallel to one another and are all disposed at a first angle θ1 relative to the transverse width direction AW.
  • The louvered portion 26 also has a plurality of second louvers 30 each extending in the height direction AH along a second louver centerline CL2. Similarly, the second louver centerlines CL2 are parallel to one another and disposed side by side along a second axis A2 extending in the transverse width direction AW. The second louvers 30 are also parallel to one another and are all disposed at a second angle θ2 relative to the transverse width direction AW.
  • The second axis A2 extends parallel to the first axis A1 and is spaced from the first axis A1 in the length direction AL, as best shown in FIGS. 3-6.
  • As best shown in FIGS. 3 and 4, each one of the second louver centerlines CL2 is spaced from a corresponding one of the first louver centerlines CL1 in the length direction AL by a first distance a. Each one of the second louver centerlines CL2 is also offset from the corresponding one of the first louver centerlines CL1 in the width direction AW by a second distance b.
  • The first distance a, the second distance b, and the first angle θ1 are interrelated according to a first relationship defined as tan−1(a/b)≠1. FIGS. 3 and 5 illustrate an embodiment wherein the tan(a/b)>θ1. FIGS. 4 and 6 illustrate an embodiment wherein the tan−1(a/b)<θ1.
  • In one embodiment shown in FIG. 4, the first distance a, the second distance b, and the first angle θ1 are interrelated according to a second relationship defined as tan−1(a/b)<θ1 and the first angle θ1 and the second angle θ2 are interrelated according to a third relationship defined as θ12.
  • The first angle θ1 may be equal to the second angle θ2, as shown in FIGS. 2-5. Alternatively, the first angle θ1 may be different than the second angle θ2, as shown in FIG. 6. If the first angle θ1 is different than the second angle θ2, as shown in FIG. 6, the difference between the first angle θ1 and the second angle θ2 is preferably in the range of 0 to 50% of the first angle θ1.
  • The first louver centerlines CL1 of the first louvers 28 are each spaced equidistant from one another. Similarly, the second louvers 30 are each spaced equidistant from one another.
  • In one embodiment shown in FIG. 5, the louvered portion 26 has a plurality of third louvers 32 each extending in the height direction AH along a third louver centerline CL3. The third louver centerlines CL3 extend parallel to one another and are spaced equidistant from one another. The third louvers 32 are parallel to one another and are all angled at a third angle θ3 relative to the transverse width direction AW. Each of the third louvers 32 are disposed side by side along and perpendicular to a third axis A3. The third axis A3 extends parallel to and spaced from the second axis A2 in the length direction AL.
  • Each one of the third louver centerlines CL3 is spaced from a corresponding one of the second louver centerlines CL2 in the length direction AL by the first distance a. Each one of the third louver centerlines CL3 is also offset from the corresponding one of the second louver centerlines CL2 in the width direction AW by the second distance b.
  • Each of the third louver centerlines CL3 are offset from corresponding ones of the second louver centerlines CL2 in the width direction AW by the first distance a and are spaced from corresponding ones of the second louver centerlines CL2 in the length direction AL by the second distance b. The angles (θ1, θ2, θ3) may all be equal to one another, as shown in FIG. 5 or alternatively may be different (not shown).
  • In operation, air flowing through the air channels 24 is diverted through the louvered portions 26 of the zigzagging fin 22 and into adjacent air channels 24. Because the invention requires multiple rows of louvers 28, 30, 32 for each louvered portion 26, the width of each louver may be reduced, reducing the thermal boundary layer and increasing heat transfer, without reducing the gap in the length direction AL between two parallel louvered portions 26, i.e., without reducing the width of the air channels 24. Accordingly, the invention surpasses the heat transfer of prior assemblies by decreasing louver width below that of the optimum width of the prior assemblies while maintaining the same air channel 24 width.
  • While the invention has been described with reference to an exemplary embodiment, 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 form the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims (14)

1. A heat exchanger assembly for dissipating heat comprising:
a plurality of tubes each extending between ends in a length direction and between sides in a width direction transverse to said length direction and parallel to and spaced from one another in a height direction transverse to said length direction and said width direction for transferring heat from a refrigerant flowing through said tubes;
a plurality of fins each being zigzagged back and forth between adjacent ones of said tubes in said height direction and disposed along said length direction between said ends of said tubes to define an air channel extending between said sides in said width direction for receiving heat from said tubes;
each of said fins defining at least one louvered portion to divert some of the air flowing through each of said air channels through said fin and into an adjacent one of said air channels;
said louvered portion having a plurality of first louvers each extending in said height direction along a first louver centerline;
said first louver centerlines being parallel to one another and disposed side by side along a first axis extending in said transverse width direction;
said first louvers disposed at a first angle relative to said transverse width direction;
said louvered portion having a plurality of second louvers each extending in said height direction along a second louver centerline;
said second louver centerlines being parallel to one another and disposed side by side along a second axis extending in said transverse width direction;
said second louvers disposed at a second angle relative to said transverse width direction; and
said second axis extending parallel to said first axis and spaced from said first axis in said length direction.
2. The assembly as set forth in claim 1 wherein each of said second louver centerlines are spaced from corresponding ones of said first louver centerlines in said length direction by a first distance and are offset from corresponding ones of said first louver centerlines in said width direction by a second distance.
3. The assembly as set forth in claim 2 wherein said length direction is perpendicular to said height direction and said width direction is perpendicular to said height direction and said length direction.
4. The assembly as set forth in claim 3 wherein said first distance and said second distance and said first angle are interrelated according to a first relationship defined as
tan - 1 ( a b ) θ 1 .
5. The assembly as set forth in claim 4 wherein said first distance and said second distance and said first angle are interrelated according to a second relationship defined as
tan - 1 ( a b ) < θ 1
and said first angle and said second angle are interrelated according to a third relationship defined as θ12.
6. The assembly as set forth in claim 2 wherein said first angle is equal to said second angle.
7. The assembly as set forth in claim 2 wherein said first angle is different than said second angle.
8. The assembly as set forth in claim 2 wherein said first louver centerlines of said first louvers each are spaced equidistant from one another and second louvers are each spaced equidistant from one another.
9. The assembly as set forth in claim 7 wherein a difference between said first angle and said second angle is in a range of 0 to 50% of said first angle.
10. The assembly as set forth in claim 2 wherein said louvered portion has a plurality of third louvers each extending in said height direction along a third louver centerline.
11. The assembly as set forth in claim 10 wherein said third louver centerlines extend parallel to and spaced equidistant from one another and said third louvers are angled at a third angle relative to said transverse width direction;
each of said third louvers being disposed side by side along and perpendicular to a third axis extending parallel to and spaced from said second axis in said length direction.
12. The assembly as set forth in claim 11 wherein each of said third louver centerlines are spaced from corresponding ones of said second louver centerlines in said length direction by said first distance and are offset from corresponding ones of said second louver centerlines in said width direction by said second distance.
13. The assembly as set forth in claim 12 wherein said angles are equal to one another.
14. A heat exchanger assembly for dissipating heat comprising:
a plurality of tubes each extending between ends in a length direction and between sides in a width direction and parallel to and spaced from one another in a height direction for transferring heat from a refrigerant flowing through said tubes;
a plurality of fins each being zigzagged back and forth between adjacent ones of said tubes in a height direction transverse to said length direction and disposed along said length direction between said ends of said tubes to define air channels in said width direction transverse to said length direction and height direction for receiving heat from said tubes;
each of said fins defining at least one louvered portion to divert some of the air flowing through each of said channels through said fin and into an adjacent one of said air channels;
each louvered portion having a plurality of first louvers each extending in said height direction along a first louver centerline;
said first louver centerlines being parallel to and spaced equidistant from one another and disposed at a first angle relative to said transverse width direction;
said first louver centerlines being disposed side by side along and perpendicular to a first axis extending transversely to said tubes in said width direction;
said louvered portion having a plurality of second louvers each extending in said height direction along a second louver centerline;
said second louver centerlines being parallel to and spaced equidistant from one another and angled at a second angle relative to said transverse width direction;
said second louver centerlines being disposed side by side along and perpendicular to a second axis extending parallel to said first axis and spaced from said first axis in said length direction;
said louvered portion having a plurality of third louvers each extending in said height direction along a third louver centerline;
said third louver centerlines being parallel to and spaced equidistant from one another and angled at a third angle relative to said transverse width direction;
said third louvers each being disposed side by side along and perpendicular to a third axis extending parallel to and spaced from said second axis in said length direction;
each of said second louver centerlines being spaced from corresponding ones of said first louver centerlines in said length direction by a first distance and being offset from corresponding ones of said first louver centerlines in a width direction by a second distance;
each of said third louver centerlines being spaced from corresponding ones of said second louver centerlines in said length direction by said first distance and being offset from corresponding ones of said second louver centerlines in a width direction by said second distance;
said first distance and said second distance and said first angle being interrelated according to a first relationship defined as
tan - 1 ( b a ) θ 1 ;
and
said angles being equal to one another.
US12/221,705 2008-01-09 2008-08-06 Louvered air center for compact heat exchanger Abandoned US20090173479A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US12/221,705 US20090173479A1 (en) 2008-01-09 2008-08-06 Louvered air center for compact heat exchanger
US13/834,355 US20130199760A1 (en) 2008-08-06 2013-03-15 Heat exchanger assembly having split mini-louvered fins
US14/486,130 US20150000880A1 (en) 2008-08-06 2014-09-15 Heat exchanger with varied louver angles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US2004808P 2008-01-09 2008-01-09
US12/221,705 US20090173479A1 (en) 2008-01-09 2008-08-06 Louvered air center for compact heat exchanger

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US13/834,355 Continuation-In-Part US20130199760A1 (en) 2008-08-06 2013-03-15 Heat exchanger assembly having split mini-louvered fins

Publications (1)

Publication Number Publication Date
US20090173479A1 true US20090173479A1 (en) 2009-07-09

Family

ID=40843649

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/221,705 Abandoned US20090173479A1 (en) 2008-01-09 2008-08-06 Louvered air center for compact heat exchanger

Country Status (1)

Country Link
US (1) US20090173479A1 (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110017440A1 (en) * 2009-07-24 2011-01-27 Denso Corporation Heat exchanger
US20110139428A1 (en) * 2008-06-20 2011-06-16 Daikin Industries, Ltd. Heat exchanger
EP2708841A1 (en) * 2011-05-13 2014-03-19 Daikin Industries, Ltd. Heat exchanger
EP2778592A1 (en) * 2013-03-15 2014-09-17 Delphi Technologies, Inc. Heat exchanger assembly having split mini-louvered fins
US20180112933A1 (en) * 2015-04-17 2018-04-26 Denso Corporation Heat exchanger
US10247481B2 (en) 2013-01-28 2019-04-02 Carrier Corporation Multiple tube bank heat exchange unit with manifold assembly
US10337799B2 (en) 2013-11-25 2019-07-02 Carrier Corporation Dual duty microchannel heat exchanger
DE102022212358A1 (en) 2022-11-18 2024-05-23 Mahle International Gmbh Corrugated fin for a heat exchanger

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265127A (en) * 1963-10-21 1966-08-09 Ford Motor Co Heat exchange element
US4615384A (en) * 1983-06-30 1986-10-07 Nihon Radiator Co., Ltd. Heat exchanger fin with louvers
US4621687A (en) * 1984-10-11 1986-11-11 Nihon Radiator Co., Ltd. Flat tube heat exchanger having corrugated fins with louvers
US4676304A (en) * 1985-01-15 1987-06-30 Sanden Corporation Serpentine-type heat exchanger having fin plates with louvers
US4756362A (en) * 1985-09-06 1988-07-12 Hitachi, Ltd. Heat exchanger
US5062475A (en) * 1989-10-02 1991-11-05 Sundstrand Heat Transfer, Inc. Chevron lanced fin design with unequal leg lengths for a heat exchanger
US5975199A (en) * 1996-12-30 1999-11-02 Samsung Electronics Co., Ltd. Cooling fin for heat exchanger
US6170566B1 (en) * 1999-12-22 2001-01-09 Visteon Global Technologies, Inc. High performance louvered fin for a heat exchanger
US6357518B1 (en) * 1999-02-01 2002-03-19 Denso Corporation Corrugated fin for heat exchanger
US6938684B2 (en) * 2002-10-24 2005-09-06 Calsonic Kansei Corporation Corrugated fin

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265127A (en) * 1963-10-21 1966-08-09 Ford Motor Co Heat exchange element
US4615384A (en) * 1983-06-30 1986-10-07 Nihon Radiator Co., Ltd. Heat exchanger fin with louvers
US4621687A (en) * 1984-10-11 1986-11-11 Nihon Radiator Co., Ltd. Flat tube heat exchanger having corrugated fins with louvers
US4676304A (en) * 1985-01-15 1987-06-30 Sanden Corporation Serpentine-type heat exchanger having fin plates with louvers
US4756362A (en) * 1985-09-06 1988-07-12 Hitachi, Ltd. Heat exchanger
US5062475A (en) * 1989-10-02 1991-11-05 Sundstrand Heat Transfer, Inc. Chevron lanced fin design with unequal leg lengths for a heat exchanger
US5975199A (en) * 1996-12-30 1999-11-02 Samsung Electronics Co., Ltd. Cooling fin for heat exchanger
US6357518B1 (en) * 1999-02-01 2002-03-19 Denso Corporation Corrugated fin for heat exchanger
US6170566B1 (en) * 1999-12-22 2001-01-09 Visteon Global Technologies, Inc. High performance louvered fin for a heat exchanger
US6938684B2 (en) * 2002-10-24 2005-09-06 Calsonic Kansei Corporation Corrugated fin

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8910703B2 (en) * 2008-06-20 2014-12-16 Daikin Industries, Ltd. Heat exchanger
US20110139428A1 (en) * 2008-06-20 2011-06-16 Daikin Industries, Ltd. Heat exchanger
US20110017440A1 (en) * 2009-07-24 2011-01-27 Denso Corporation Heat exchanger
US9074820B2 (en) * 2009-07-24 2015-07-07 Denso Corporation Heat exchanger
US9803935B2 (en) 2011-05-13 2017-10-31 Daikin Industries, Ltd. Heat exchanger
EP2708841A4 (en) * 2011-05-13 2014-10-29 Daikin Ind Ltd Heat exchanger
AU2012256999B2 (en) * 2011-05-13 2015-06-11 Daikin Industries, Ltd. Heat exchanger
EP2708841A1 (en) * 2011-05-13 2014-03-19 Daikin Industries, Ltd. Heat exchanger
US10247481B2 (en) 2013-01-28 2019-04-02 Carrier Corporation Multiple tube bank heat exchange unit with manifold assembly
CN104048522A (en) * 2013-03-15 2014-09-17 德尔福技术有限公司 Heat Exchanger Assembly Having Split Mini-louvered Fins
EP2778592A1 (en) * 2013-03-15 2014-09-17 Delphi Technologies, Inc. Heat exchanger assembly having split mini-louvered fins
US10337799B2 (en) 2013-11-25 2019-07-02 Carrier Corporation Dual duty microchannel heat exchanger
US20180112933A1 (en) * 2015-04-17 2018-04-26 Denso Corporation Heat exchanger
US10107553B2 (en) * 2015-04-17 2018-10-23 Denso Corporation Heat exchanger
DE102022212358A1 (en) 2022-11-18 2024-05-23 Mahle International Gmbh Corrugated fin for a heat exchanger

Similar Documents

Publication Publication Date Title
EP2314972B1 (en) Heat exchanger
US7913750B2 (en) Louvered air center with vortex generating extensions for compact heat exchanger
US20090173479A1 (en) Louvered air center for compact heat exchanger
AU2004241397B2 (en) Plate fin tube-type heat exchanger
US6401809B1 (en) Continuous combination fin for a heat exchanger
US6431263B2 (en) Heat exchanger with small-diameter refrigerant tubes
US20130153174A1 (en) Microchannel heat exchanger fin
KR100740180B1 (en) Finned heat exchanger and method of manufacturing the same
WO2009144909A1 (en) Fin-tube heat exchanger
US20070051502A1 (en) Heat exchanger fin, heat exchanger, condensers, and evaporators
US5117902A (en) Fin tube heat exchanger
EP1519133A2 (en) Heat exchanging apparatus
US6942024B2 (en) Corrugated heat exchange element
US7413002B2 (en) Corrugated fin and heat exchanger using the same
US5975200A (en) Plate-fin type heat exchanger
EP1977180B1 (en) Fin and tube heat exchanger
KR20060012303A (en) Heat exchanger fin, heat exchanger, condensers, and evaporators
JP6706839B2 (en) Fin tube heat exchanger
JP2004263881A (en) Heat transfer fin, heat exchanger, evaporator and condenser for car air conditioner
EP0803695B1 (en) Plate-fin heat exchanger
JPH0545474U (en) Heat exchanger
CN114322105B (en) Heat exchanger and air conditioning system
US20210389057A1 (en) Heat exchanger
EP2224198A1 (en) Fin and tube type heat exchanger
JP3867113B2 (en) Heat exchanger

Legal Events

Date Code Title Description
AS Assignment

Owner name: DELPHI TECHNOLOGIES, INC., MICHIGAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HUANG, LIN-JIE;REEL/FRAME:021417/0614

Effective date: 20080721

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION