[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP3660434A1 - Weaved cross-flow heat exchanger and method of forming a heat exchanger - Google Patents

Weaved cross-flow heat exchanger and method of forming a heat exchanger Download PDF

Info

Publication number
EP3660434A1
EP3660434A1 EP19207464.9A EP19207464A EP3660434A1 EP 3660434 A1 EP3660434 A1 EP 3660434A1 EP 19207464 A EP19207464 A EP 19207464A EP 3660434 A1 EP3660434 A1 EP 3660434A1
Authority
EP
European Patent Office
Prior art keywords
wall
waves
flow paths
heat exchanger
flow
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.)
Pending
Application number
EP19207464.9A
Other languages
German (de)
French (fr)
Inventor
Joseph Turney
Robert H. Dold
Christopher Britton Greene
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.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand Corp
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 Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of EP3660434A1 publication Critical patent/EP3660434A1/en
Pending 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
    • F28F3/00Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/02Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
    • F28F3/025Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations the means being corrugated, plate-like elements
    • 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
    • F28D7/00Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/0008Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one medium being in heat conductive contact with the conduits for the other medium
    • F28D7/0025Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one medium being in heat conductive contact with the conduits for the other medium the conduits for one medium or the conduits for both media being flat tubes or arrays of tubes
    • F28D7/0033Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one medium being in heat conductive contact with the conduits for the other medium the conduits for one medium or the conduits for both media being flat tubes or arrays of tubes the conduits for one medium or the conduits for both media being bent
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0025Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by zig-zag bend plates
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0031Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
    • 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
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0031Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
    • F28D9/0037Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the conduits for the other heat-exchange medium also being formed by paired plates touching each other
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F7/00Elements not covered by group F28F1/00, F28F3/00 or F28F5/00
    • F28F7/02Blocks traversed by passages for heat-exchange media
    • 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
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0026Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for combustion engines, e.g. for gas turbines or for Stirling engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2250/00Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
    • F28F2250/10Particular pattern of flow of the heat exchange media
    • F28F2250/106Particular pattern of flow of the heat exchange media with cross flow

Definitions

  • the present invention relates to heat exchangers and, in particular, to a method for forming a heat exchanger and to a heat exchanger that utilizes a weaved cross-flow configuration to increase the thermal energy transfer primary surface area of the heat exchanger.
  • Heat exchangers aim to transfer heat between a hot fluid and a cool fluid.
  • walls primary surfaces
  • fins secondary surfaces
  • the heat transfer through primary surface is very good because the walls are thin and the distance the thermal energy needs to travel is relatively small.
  • the heat transfer through secondary surfaces is less efficient than primary surfaces because the thermal energy must travel a longer distance along the length of the fins.
  • the most compact heat exchangers i.e., high surface area per unit volume
  • a heat exchanger is disclosed herein that extends laterally in a first direction and a second direction.
  • the heat exchanger includes three walls.
  • a first wall is shaped in a wave pattern with waves that extend in both the first direction and the second direction. These waves can have a variety of configurations, including waves based on a sinusoidal curve in both the first direction and the second direction.
  • the second wall is adjacent to and in contact with the first wall.
  • the second wall is also shaped in a wave pattern with waves that extend in both the first direction and the second direction.
  • the waves of the second wall are offset in the first direction from the first wall by one-half wavelength.
  • the third wall is adjacent to and in contact with the second wall.
  • the third wall is also shaped in a wave pattern with waves that extend in both the first direction and the second direction.
  • the waves of the third wall are offset in the second direction from the second wall by one-half wavelength.
  • the first wall and second wall form a first plurality of flow paths extending in the second direction, and the second wall and third wall form a second plurality of flow paths extending in the first direction.
  • a method of forming a heat exchanger includes forming a first wall with waves that extend laterally in both a first direction and in a second direction.
  • the method also includes forming a second wall adjacent to and in contact with the first wall with waves that are based on a sinusoidal curve and extend laterally in both the first direction and in the second direction.
  • the waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength.
  • the method also includes forming a third wall adjacent to and in contact with the second wall with waves that extend laterally in both the first direction and in the second direction.
  • the waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.
  • the first wall and the second wall bound a first plurality of flow paths that extend in the second direction
  • the second wall and the third wall bound a second plurality of flow paths that extend in the first direction.
  • the waves of the first, second, and third walls can be based on a sinusoidal curve.
  • a method of transferring thermal energy through the use of a heat exchanger includes flowing a first fluid through a first plurality of flow paths bounded by a first wall and a second wall.
  • the first wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both a first direction and a second direction.
  • the second wall is adjacent to and in contact with the first wall and having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction.
  • the waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength.
  • the method also includes flowing a second fluid through a second plurality of flow paths bounded by the second wall and a third wall.
  • the third wall is adjacent to and in contact with the second wall.
  • the third wall has a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction.
  • the waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.
  • a heat exchanger is disclosed herein that utilizes a weaved cross-flow configuration to transfer thermal energy between a first fluid and a second fluid.
  • the weaved configuration is constructed primarily from stacked sheets/walls that include waves in a first lateral direction and a second lateral direction.
  • the waves can have a variety of configurations, including waves that are based on a sinusoidal (i.e., cosine or sine) curve.
  • the walls are primary surfaces that have improved thermal energy transfer capabilities.
  • the waves of one wall are offset from waves of adjacent walls by one-half wavelength to form a plurality of flow paths between adjacent walls through which the first or second fluid flows. Utilizing walls with waves provides an increase in primary surface area of the walls which in turn increases the thermal energy transfer between fluids flowing adjacent those walls.
  • the increase in surface area of the walls eliminates the need for fins (i.e., additional secondary surface), thereby improving efficiency of the heat exchanger by maximizing the energy transfer-to-volume ratio.
  • Additive manufacturing can be utilized to create the disclosed heat exchanger so that all components of the heat exchanger are formed during one manufacturing process to form a continuous and monolithic structure. Further, additive manufacturing can easily and reliably form the heat exchanger with complex walls/shapes and small tolerances.
  • continuous and monolithic means formed as a single unit without seams, weld lines, adhesive lines, or any other discontinuities.
  • the waves of the walls (which, for example, are based on sinusoidal curves) can have alternate amplitudes, wavelengths, and other characteristics as required for optimal thermal energy transfer and to accommodate a designed flow of the first fluid and/or second fluid. Further, the waves can have a variety of shapes, such as triangular waves with pointed peaks and troughs, rectangular waves with flat tops and bottoms, and/or other configurations.
  • FIG. 1A is a perspective cross-sectional view of a portion of a heat exchanger
  • FIG. 1B is a second perspective view of the heat exchanger in FIG. 1A
  • FIG. 1C is a perspective view of a plurality of flow paths through the heat exchanger in FIG. 1A
  • Heat exchanger 10 includes first wall 12, second wall 14, third wall 16, fourth wall 18, fifth wall 20, sixth wall 22, seventh wall 24, and eighth wall 26.
  • Walls 12-26 are primary surfaces, extend laterally in first lateral direction 28A and second lateral direction 28B, and are vertically adjacent one another in vertical direction 28C.
  • First wall 12 and second wall 14 contact one another at first contact lines 30A to form first plurality of flow paths 30B
  • second wall 14 and third wall 16 contact one another at second contact lines 32A to form second plurality of flow paths 32B
  • third wall 16 and fourth wall 18 contact one another at third contact lines 34A to form third plurality of flow paths 34B
  • fourth wall 18 and fifth wall 20 contact one another at fourth contact lines 36A to form fourth plurality of flow paths 36B
  • fifth wall 20 and sixth wall 22 contact one another at fifth contact lines 38A to form fifth plurality of flow paths 38B
  • sixth wall 22 and seventh wall 24 contact one another at sixth contact lines 40A to form sixth plurality of flow paths 40B
  • seventh wall 24 and eighth wall 26 contact one another at seventh contact line 42A to form seventh plurality of flow paths 42B.
  • First wall 12 includes waves having first wall crests 12A and first wall troughs 12B
  • second wall 14 includes waves having second wall crests 14A and second wall troughs 14B
  • third wall 16 includes waves having third wall crests 16A and third wall troughs 16B
  • fourth wall 18 includes waves having fourth wall crests 18A and fourth wall troughs 18B
  • fifth wall 20 includes waves having fifth wall crests 20A and fifth wall troughs 20B
  • sixth wall 22 includes waves having sixth wall crests 22A and sixth wall troughs 22B
  • seventh wall 24 includes waves having seventh wall crests 24A and seventh wall troughs 24B
  • eighth wall 26 includes waves having eighth wall crests 26A and eighth wall troughs 26B.
  • Heat exchanger 10 is formed by stacking walls 12-26 vertically to form a plurality of flow paths 30B-42B (seen most easily in FIG. 1C ) through which hot fluid and cold fluid can flow (in a cross-flow configuration) to transfer thermal energy to cool the hot fluid through primary surface walls 12-26. While shown as having eight walls 12-26, heat exchanger 10 can have any number of walls that form the plurality of flow paths 30B-42B, including only three walls 12-16 that form two pluralities of flow paths 30B and 32B or more than eighth walls forming more than seven pluralities of flow paths (as shown in FIG. 1B (unlabeled)).
  • heat exchanger 10 can extend in a lateral direction any distance, including in first lateral direction 28A a distance that is equal to a distance that heat exchanger 10 extends in second lateral direction 28B. Alternately, heat exchanger 10 can extend in first lateral direction 28A a different distance than that in second lateral direction 28B to form heat exchanger 10 that has a rectangular footprint or another shape. In such configurations, the waves of walls 12-26 would repeat so as to have multiple wavelengths in first lateral direction 28A and second lateral direction 28B to provide sufficient thermal energy transfer surface area to meet thermal energy transfer requirements.
  • walls 12-26 each include waves in both first lateral direction 28A and second lateral direction 28B that are based on a sinusoidal curve.
  • adjacent walls are offset from one another either in first lateral direction 28A or second lateral direction 28B by one-half wavelength, resulting in crests 12A-26A contacting troughs 12B-26B of adjacent walls 12-26 to form a plurality of discrete flow paths 30B-42B.
  • Adjacent walls 12-26 being offset by one-half wavelength in either first lateral direction 28A or second lateral direction 28B forms contact lines 30A-42A that, along with adjacent walls 12-26, bound the plurality of discrete flow paths 30B-42B.
  • Such a configuration provides a weaved, cross-flow heat exchanger 10 with increased primary surface area. Nearly the entire surface area of each flow path of the plurality of flow paths 30B-42B is primary heat transfer area resulting in increased heat transfer and reduced volume of heat exchanger 10.
  • Each wall 12-26 will be described below and its relation to adjacent walls. However, other configurations of heat exchanger 10 can have different orientations such that "lateral" and “vertical” are used herein only to describe component in relation to one another with regards to FIG.S 1A-1C and do not require heat exchanger 10 be oriented such that walls 12-26 extend in a horizontal direction or any particular special direction.
  • First wall 12 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B.
  • the waves of first wall 12 are based on a sinusoidal curve that repeat in both directions 28A and 28B. Additionally, a person of ordinary skill in the art will recognize that the waves can be based on either cosine or sine curves, which are essentially the same and are only different as to the starting point of each type of wave. For convenience, this application will describe the disclosed heat exchanger 10 using cosine terminology.
  • the waves of first wall 12 show two complete wavelengths in first lateral direction 28A and four complete wavelengths in second lateral direction 28B. In FIG.
  • walls 12-26 are shown to have at least five waves in both directions 28A and 28B.
  • Multiple first wall crests 12A (the peaks of the waves) and multiple first wall troughs 12B (the valleys of the waves) are in each direction 28A and 28B.
  • first wall crests 12A and first walls troughs 12B are lines that extend in either first lateral direction 28A or second lateral direction 28B.
  • thick line 30A first contact lines 30A
  • first wall 12 contacts second wall 14 along first wall troughs 12B that extend in second lateral direction 28B.
  • first contact lines 30A do include multiple first wall crests 12A extending along lines in first lateral direction 28A.
  • first wall crests 12A and first wall troughs 12B form a checkered pattern with a lowest point of first wall 12 being at a point where first wall troughs 12B in first lateral direction 28A intersect first wall troughs 12B in second lateral direction 28B.
  • First wall 12 can have any thickness, including a constant thickness in one or both directions 28A and 28B or a varying thickness depending on structural and/or thermal energy transfer needs.
  • the thickness of first wall 12 (and other walls 14-26) can be configured to alter the cross-sectional flow area of the plurality of flow paths 30B-42B.
  • the cross-sectional flow area can be substantially circular (as shown in FIG. 2 ) or another shape.
  • the amplitude and/or wavelength of first wall 12 can be anything suitable for thermal energy transfer, can be the same or different than the amplitude and/or wavelength of the other walls 14-26, and/or can be different in first lateral direction 28A as compared to second lateral direction 28B.
  • first wall 12 in first lateral direction 28A can be at least 1.5 times greater in amplitude than the waves of first wall 12 in second lateral direction 28B.
  • first wall 12, third wall 16, fifth wall 20, and seventh wall 24 may need to have the same amplitude and wavelength (and similarly, second wall 14, fourth wall 18, sixth wall 20, and eighth wall 26).
  • Second wall 14 is similar to first wall 12 in that second wall 14 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Second wall 14 is adjacent to and in contact with first wall 14 (on a top side) and third wall 18 (on a bottom side). The waves of second wall 14 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of second wall 14 are offset from first wall 12 in first lateral direction 28A by one-half wavelength.
  • first contact lines 30A are where first wall 12 and second wall 14 connect to one another to bound first plurality of flow paths 30B.
  • second wall 14 has multiple second wall crests 14A and troughs 14B in both first lateral direction 28A and second lateral direction 28B.
  • the waves of second wall 14 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12 in one or both directions 28A and 28B.
  • the thickness of second wall 12 can be constant or varying in any direction 28A and 28B.
  • First plurality of flow paths 30B are formed and bounded by first wall 12 and second wall 14 (and first contact lines 30A) and extend in second lateral direction 28B. As seen most easily in FIG. 1C , which shows plurality of flow paths 30B-42B without the presence of walls 12-26, first plurality of flow paths 30B have undulating cross-sectional flow areas due to the waves of first wall 12 and second wall 14, which enhances heat transfer by limiting boundary layer growth through first plurality of flow paths 30B. In FIGS. 1A-1C , each of the first plurality of flow paths 30B are fluidically isolated from adjacent flow paths of first plurality of flow paths 30B. However, as shown in FIG.
  • first plurality of flow paths 30B can be laterally or vertically interconnected such that flow through one flow path of first plurality of flow paths 30B can transition and flow through an adjacent flow path of first plurality of flow paths 30B or adjacent pluralities of flow paths 32B-42B.
  • first contact lines 30A are not continuous along an entire distance of first wall 12 and second wall 14 in second lateral direction 28B and rather there are transition openings between adjacent flow paths of first plurality of flow paths 30B.
  • the cross-sectional flow area of each of the first plurality of flow paths 30B can be similar to adjacent flow paths or can be differing, such as flow paths of the first plurality of flow paths 30B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape.
  • Fluid flowing through each of first plurality of flow paths 30B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Third wall 16 is similar to second wall 14 in that third wall 16 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Third wall 16 is adjacent to and in contact with second wall 14 (on a top side) and fourth wall 18 (on a bottom side). The waves of third wall 16 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of third wall 16 are offset from second wall 14 in second lateral direction 28B by one-half wavelength.
  • third wall 16 is offset from second wall 14 in second lateral direction 28B, third wall crests 16A (in second lateral direction 28B) contact second wall troughs 14B (in second lateral direction 28B) to form second contact lines 32A, which extend in first lateral direction 28A.
  • Second contact lines 32A are where second wall 14 and third wall 16 connect to one another to bound second plurality of flow paths 32B.
  • third wall 16 has multiple third wall crests 16A and third wall troughs 16B in both first lateral direction 28A and second lateral direction 28B.
  • the waves of third wall 16 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12 and/or second wall 14 in one or both directions 28A and 28B.
  • the waves in first lateral direction 28A of first wall 12, second wall 14, and third wall 16 have an amplitude and/or wavelength that is greater than an amplitude and/or wavelength of the waves in second lateral direction 28B of first wall 12, second wall 14, and third wall 16.
  • a thickness of third wall 16 can be constant or varying in any direction 28A and 28B.
  • Second plurality of flow paths 32B are formed and bounded by second wall 14 and third wall 16 (and second contact lines 32A) and extend in first lateral direction 28A.
  • Second plurality of flow paths 32B form a weaved, cross-flow pattern with first plurality of flow paths 30B and third plurality of flow paths 34B.
  • hot fluid can flow through second plurality of flow paths 32B while cold fluid flows through first plurality of flow paths 30B and third plurality of flow paths 34B such that thermal energy transfers across second wall 14 and third wall 16.
  • Second plurality of flow paths 32B can be similar in configuration and functionality to first plurality of flow paths 30B (except that second plurality of flow paths 32B extend in first lateral direction 28A). In FIGS.
  • each flow path of second plurality of flow paths 32B are fluidically isolated from adjacent flow paths of second plurality of flow paths 32B.
  • second plurality of flow paths 32B can be laterally or vertically interconnected such that flow through one flow path of second plurality of flow paths 32B can transition and flow through an adjacent flow path of second plurality of flow paths 32B.
  • second contact lines 32A are not continuous along an entire distance of second wall 14 and third wall 16 in first lateral direction 28A and rather there are transition openings between adj acent flow paths of second plurality of flow paths 32B.
  • each of the second plurality of flow paths 32B can be similar to adjacent flow paths or can be differing, such as flow paths of the second plurality of flow paths 32B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape.
  • Fluid flowing through each of second plurality of flow paths 32B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Fourth wall 18 is similar to third wall 16 in that fourth wall 18 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Fourth wall 18 is adjacent to and in contact with third wall 16 (on a top side) and fifth wall 20 (on a bottom side). The waves of fourth wall 18 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of fourth wall 18 are offset from third wall 16 in first lateral direction 28A by one-half wavelength.
  • fourth wall 18 is offset from third wall 16 in first lateral direction 28A, fourth wall crests 18A (in second lateral direction 28B) contact third wall troughs 16B (in second lateral direction 28B) to form third contact lines 34A, which extend in second lateral direction 28B.
  • Third contact lines 34A are where third wall 16 and fourth wall 18 connect to one another to bound third plurality of flow paths 34B.
  • fourth wall 18 has multiple fourth wall crests 18A and fourth wall troughs 18B in both first lateral direction 28A and second lateral direction 28B.
  • the waves of fourth wall 18 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12, second wall 14, and/or third wall 16 in one or both directions 28A and 28B.
  • the thickness of fourth wall 18 can be constant or varying in any direction 28A and 28B.
  • Third plurality of flow paths 34B are formed and bounded by third wall 16 and fourth wall 18 (and third contact lines 34A) and extend in second lateral direction 28B. Third plurality of flow paths 34B form a weaved, cross-flow pattern with second plurality of flow paths 32B and fourth plurality of flow paths 36B. For example, hot fluid can flow through first plurality of flow paths 30B and third plurality of flow paths 34B while cold fluid flows through second plurality of flow paths 32B and fourth plurality of flow paths 36B such that thermal energy transfers through second wall 14, third wall 16, and fourth wall 18.
  • Third plurality of flow paths 34B can be similar in configuration and functionality to first plurality of flow paths 30B and second plurality of flow paths 32B (except that third plurality of flow paths 34B extend in second lateral direction 28B and are offset from first plurality of flow paths 30B by one-half wavelength in first lateral direction 28A).
  • each flow path of third plurality of flow paths 34B are fluidically isolated from adjacent flow paths of third plurality of flow paths 34B.
  • third plurality of flow paths 34B can be laterally or vertically interconnected such that flow through one flow path of third plurality of flow paths 34B can transition and flow through an adjacent flow path of third plurality of flow paths 34B.
  • third contact lines 34A are not continuous along an entire distance of third wall 16 and fourth wall 18 in second lateral direction 28B and rather there are transition openings between adjacent flow paths of third plurality of flow paths 34B.
  • the cross-sectional flow area of each of the third plurality of flow paths 34B can be similar to adjacent flow paths or can be differing, such as flow paths of the third plurality of flow paths 34B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape.
  • Fluid flowing through each of third plurality of flow paths 34B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Fifth wall 20 is similar to fourth wall 18 in that fifth wall 20 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Fifth wall 20 is adjacent to and in contact with fourth wall 18 (on a top side) and sixth wall 22 (on a bottom side). Fifth wall 20 has the same orientation as first wall 12 with the waves of fifth wall 20 being offset from fourth wall 18 in second lateral direction 28B by one-half wavelength.
  • the configuration of heat exchanger 10 downward from fifth wall 20 repeats so as to have the same configuration of heat exchanger 10 between first wall 12 and fifth wall 20.
  • fifth wall 20 is offset from fourth wall 18 in second lateral direction 28B, fifth wall crests 20A (in first lateral direction 28A) contact fourth wall troughs 18B (in first lateral direction 28A) to form fourth contact lines 36A, which extend in first lateral direction 28A.
  • Fourth contact lines 36A are where fourth wall 18 and fifth wall 20 connect to one another to bound fourth plurality of flow paths 36B.
  • fifth wall 20 has multiple fifth wall crests 20A and fifth wall troughs 20B in both first lateral direction 28A and second lateral direction 28B.
  • the waves of fifth wall 20 can have the same or differing amplitudes and/or wavelengths as the waves of walls 12-18 in one or both directions 28A and 28B. Additionally, similar to walls 12-18, the thickness of fifth wall 20 can be constant or varying in any direction 28A and 28B.
  • Fourth plurality of flow paths 36B are formed and bounded by fourth wall 18 and fifth wall 20 (and fourth contact lines 36A) and extend in first lateral direction 28A. Fourth plurality of flow paths 36B form a weaved, cross-flow pattern with third plurality of flow paths 34B and fifth plurality of flow paths 38B. For example, hot fluid can flow through first plurality of flow paths 30B and third plurality of flow paths 34B while cold fluid flows through second plurality of flow paths 32B and fourth plurality of flow paths 36B such that thermal energy transfers through second wall 14, third wall 16, fourth wall 18, and fifth wall 20. Fourth plurality of flow paths 36B can be similar in configuration and functionality to other pluralities of flow paths 30B-42B. In FIGS.
  • each flow path of fourth plurality of flow paths 36B are fluidically isolated from adjacent flow paths of fourth plurality of flow paths 36B.
  • fourth plurality of flow paths 36B can be laterally or vertically interconnected such that flow through one flow path of fourth plurality of flow paths 36B can transition and flow through an adjacent flow path of fourth plurality of flow paths 36B.
  • fourth contact lines 36A are not continuous along an entire distance of fourth wall 18 and fifth wall 20 in first lateral direction 28A and rather there are transition openings between adjacent flow paths of fourth plurality of flow paths 36B.
  • each of the fourth plurality of flow paths 36B can be similar to adjacent flow paths or can be differing, such as flow paths of the fourth plurality of flow paths 36B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape.
  • Fluid flowing through each of fourth plurality of flow paths 36B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Sixth wall 22 has the same orientation, configuration, and functionality as second wall 14. Sixth wall 22 is adjacent to and in contact with fifth wall 20 (along fifth contact lines 38A) to form fifth plurality of flow paths 38B. Fifth plurality of flow paths 38B has the same orientation, configuration, and functionality as first plurality of flow paths 30B. Seventh wall 24 has the same orientation, configuration, and functionality as third wall 16. Seventh wall 24 is adjacent to and in contact with sixth wall 22 (along sixth contact lines 40A) to form sixth plurality of flow paths 40B. Sixth plurality of flow paths 40B has the same orientation, configuration, and functionality as second plurality of flow paths 32B. Eighth wall 26 has the same orientation, configuration, and functionality as fourth wall 18. Eighth wall 26 is adjacent to and in contact with seventh wall 24 (along seventh contact lines 42A) to form seventh plurality of flow paths 42B. Seventh plurality of flow paths 42B has the same orientation, configuration, and functionality as third plurality of flow paths 34B.
  • Heat exchanger 10 can extend in vertical direction 28C by including additional walls having the same orientation as walls 12-26 (as shown in FIG. 1B ) and/or by increasing the amplitude of the waves of walls 12-26.
  • Heat exchanger 10 can be constructed from a variety of materials, including conventional materials and materials that have lower thermal conductivity properties than materials conventionally used to construct heat exchangers. Because the primary thermal energy transfer surface area of each flow path of the plurality of flow paths 30B-42B is increased due to the wave pattern of walls 12-26 of heat exchanger 10, the amount of thermal energy transfer of heat exchanger 10 is increased as compared to prior art heat exchangers. With an increase in primary surface area, heat exchanger 10 can be constructed from materials that have low thermal conductivity properties, such as plastics or composites.
  • heat exchanger 10 may be constructed from reinforced nylon, acrylonitrile butadiene styrene, epoxy, or urethane methacrylate. If desired, heat exchanger 10 can be located within a machine that requires increased thermal energy transfer capabilities and a small volume, such as a gas turbine engine.
  • heat exchanger 10 can be constructed from multiple components such that each of walls 12-26 is constructed independently and then fastened together along contact lines 30A-42A
  • heat exchanger 10 can be formed as one continuous and monolithic piece through additive manufacturing or other methods such that heat exchanger 10 is formed as a single unit without seams, weld lines, adhesive lines, or any other discontinuities.
  • first wall 12 is formed with waves based on a cosine curve extending in both first lateral direction 28A and second lateral direction 28B.
  • second wall 14 is formed with waves based on a cosine curve extending in both directions 28A and 28B with the waves being offset in first lateral direction 28A from first wall 12 by one-half wavelength to form first plurality of flow paths 30B.
  • Second wall 14 is adjacent to first wall 12 and can be either fastened to first wall 12 along first contact lines 30A, or second wall 14 can be formed simultaneously with first wall 12 such that first wall 12 and second wall 14 are one continuous and monolithic piece.
  • third wall 16 is formed with waves based on a cosine curve extending in both directions 28A and 28B with the waves being offset in second lateral direction 28A from second wall 14 by one-half wavelength to form second plurality of flow paths 32B.
  • Third wall 16 is adjacent to second wall 14 and can be either fastened to second wall 14 along second contact liens 32A, or third wall 16 can be formed simultaneously with second wall 14 (and possibly first wall 12) such that second wall 14 and third wall 16 are one continuous and monolithic piece.
  • Subsequent walls 18-26 (or more) can be formed utilizing similar steps.
  • a method of forming heat exchanger 10 can start at a bottom wall (a wall that is on a bottom side of heat exchanger 10) and build up walls from there, or the method can form heat exchanger 10 building the walls in first lateral direction 28A or second lateral direction 28B.
  • the disclosed heat exchanger 10 will be described as transferring thermal energy between two fluids, a first fluid and a second fluid, a person skilled in the art will recognize that the disclosed heat exchanger 10 may be used with more than two fluids provided it is constructed with sufficient pluralities of flow paths to accommodate more than two heat exchange fluids.
  • the first fluid (which can be a hot fluid or cold fluid) is conveyed/flowed in second lateral direction 28B through first plurality of flow paths 30B and, if necessary, third plurality of flow paths 34B, fifth plurality of flow paths 38B, and seventh plurality of flow paths 42B.
  • the second fluid (which can be a hot fluid or a cold fluid but should be a fluid that has a different temperature than the first fluid) is conveyed/flowed in first lateral direction 28A through second plurality of flow paths 32B and, if necessary, fourth plurality of flow paths 36B and sixth plurality of flow paths 40B. Because of the weaved, cross-flow configuration of heat exchanger 10 having walls 12-26 with a wave pattern, thermal energy transfer between the first fluid and second fluid is rapid because the thermal energy transfer surface areas of each flow path of the pluralities of flow paths 30B-42B is large and direct from the hot fluid to the cold fluid (i.e., no conduction along a fin) and the undulating nature of each flow path creates enhances heat transfer.
  • FIG. 2 is a second embodiment of a heat exchanger.
  • Heat exchanger 110 is similar to heat exchanger 10 in FIGS. 1A-1C except that heat exchanger 110 includes sub flow paths as part of a plurality of flow paths that are vertically connected by transition openings.
  • a plurality of flow paths includes multiple subflow paths that are connected to adjacent subflow paths vertically to allow for a fluid flowing through the plurality of flow paths to transition and flow through an adjacent subflow path while still providing an increase in primary surface area for optimal heat transfer. While FIG.
  • heat exchanger 110 can be such that subflow paths can be connected to adjacent subflow paths horizontally (i.e., the pluralities of flow paths 30B-42B in heat exchanger 10 are connected to one another by transition openings between adjacent flow paths). While the pluralities of flow paths of heat exchanger 110 can be described with regards to walls in a similar fashion to that of heat exchanger 10, it may be easier to understand the configuration of heat exchanger 110 by describing the pluralities of flow paths through heat exchanger 110 rather than the walls that bound the pluralities of flow paths.
  • Heat exchanger 110 includes walls 112 bounding cold fluid flow path 150 (which encompasses all cold fluid flow paths, including the pluralities of cold flow paths as well as subflow paths) extending in first lateral direction 128A and hot fluid flow path 170 (which encompasses all hot fluid flow paths, including the pluralities of hot flow paths as well as subflow paths) extending in second lateral direction 128B. While this disclosure describes the flow paths as being for "hot” fluid and "cold" fluid, this is done for simplicity such that the temperature and/or type of fluid is exemplary and any type of fluid and even more than two fluids can be utilized in heat exchanger 110.
  • Cold fluid flow path 150 includes first plurality of cold flow paths 152, second plurality of cold flow paths 154, third plurality of cold flow paths 156, fourth plurality of cold flow paths 158, fifth plurality of cold flow paths 160, sixth plurality of cold flow paths 162, and seventh plurality of cold flow paths 164.
  • Each cold plurality of cold flow paths 152-164 includes six cold subflow paths, with first plurality of cold flow paths 152 having first cold subflow paths 152A-152F (while not labeled in FIG. 2 for simplicity, the other pluralities of flow paths 154-164 also include six cold subflow paths of similar configuration and functionality).
  • hot fluid flow path 170 includes first plurality of hot flow paths 172, second plurality of hot flow paths 174, third plurality of hot flow paths 176, fourth plurality of hot flow paths 178, fifth plurality of hot flow paths 180, sixth plurality of hot flow paths 182, and seventh plurality of hot flow paths 184.
  • Each plurality of hot flow paths 172-184 includes six hot subflow paths, with first plurality of hot flow paths 172 having first hot subflow paths 172A-172F (while not labeled in FIG.
  • the other pluralities of hot flow paths 174-184 also include six hot subflow paths of similar configuration and functionality). Between hot subflow paths 172A-172F are transition openings 186, which provide a path through which hot fluid can flow between adjacent hot subflow paths 172A-172F.
  • transition openings 186 Between hot subflow paths 172A-172F are transition openings 186, which provide a path through which hot fluid can flow between adjacent hot subflow paths 172A-172F.
  • the other pluralities of cold flow paths 154-164 and hot flow paths 174-184 have similar configurations and functionalities.
  • Cold fluid flow path 150 includes pluralities of cold flow paths 152-164 that are columns of flow paths arranged so as to be laterally adjacent to at least one other plurality of cold flow paths 152-164.
  • Each of the pluralities of cold flow paths 152-164 extend in first lateral direction 128A such that cold fluid flowing through the plurality of cold flow paths 152-164 flows substantially in first lateral direction 128A.
  • heat exchanger 110 can include a lesser or greater number of pluralities of cold flow paths 152-164 for accommodating cold fluid flow.
  • heat exchanger 110 can include less than six or greater than six cold subflow paths as the design requires (and, for example, space within a gas turbine engine allows).
  • adjacent pluralities of cold flow paths 152-164 do not provide for cold fluid flow therebetween and cold fluid is only able to flow between adjacent cold subflow paths 152A-152F within a single plurality of cold flow paths 152-164.
  • other embodiments of heat exchanger 110 can include openings that allow cold fluid to transition between adjacent pluralities of cold flow paths 152-164.
  • First plurality of cold flow paths 152 is shown in a cross-sectional representation so that cold subflow paths 152A-152F are more easily seen.
  • First plurality of cold flow paths 152 (and other pluralities of cold flow paths 154-164 and 172-184) extend vertically and are bounded by walls 112.
  • First plurality of cold flow paths 152 include cold subflow paths 152A-152F, which allow cold fluid to flow in first lateral direction 128A while also allowing cold fluid to transition between adjacent cold subflow paths 152A-152F.
  • Cold fluid is able to flow between adjacent cold subflow paths 152A-152F by flowing at least partially vertically through transition openings 166 between adjacent cold subflow paths 152A-152F.
  • Each of cold subflow paths 152A-152F have a wave pattern with waves that extend in first lateral direction 128A based on a cosine curve (or sine curve depending on the starting point of the wave). However, cold subflow paths 152A-152F are offset from adjacent cold subflow paths 152A-152F by one-half wavelength in first lateral direction 128A.
  • cold subflow path 152A (a topmost subflow path), cold subflow path 152C, and cold subflow path 152E have the same configuration as one another with waves that propagate in first lateral direction 128A in phase (i.e., crests and troughs of the waves line up vertically).
  • Cold subflow path 152B, cold subflow path 152D, and cold subflow path 152F (a bottommost subflow path) also have the same configuration as one another with waves that propagate in first lateral direction 128A in phase.
  • cold subflow paths 152B, 152D, and 152F are offset from cold subflow paths 152A, 152C, and 152E one-half wavelength such that the crests of cold subflow paths 152A, 152C, and 152E interconnect with the troughs of cold subflow paths 152B, 152D, and 152F (and vice-versa) to form transition openings 166 through which cold fluid can flow into adjacent cold subflow paths 152A-152F.
  • cold subflow paths 152A-152F are shown as having the same amplitude and wavelength, other embodiments can include cold subflow paths 152A-152F that have differing amplitudes and wavelengths.
  • other pluralities of cold flow paths 154-164 can have different configurations such that those cold subflow paths (which are part of each plurality of cold flow paths 154-164) have differing amplitudes, wavelengths, and/or orientations.
  • Transition openings 166 that interconnect cold subflow paths 152A-152F can have as large or small cross-sectional area as desired and, in other embodiments, heat exchanger 110 may not include transition openings 166 and instead cold subflow paths 152A-152F are discrete and fluidically isolated from one another.
  • Cold subflow paths 152A-152F are shown as having a substantially circular cross-sectional area due to walls 112 having a varying thickness to form the circular cross-sectional area. However, cold subflow paths 152A-152F can have other cross-sectional areas, such as any non-circular cross-section including eyelet-type shape or another shape.
  • First plurality of hot flow paths 172 is shown in a cross-sectional representation so that hot subflow paths 172A-172F are more easily seen.
  • First plurality of hot flow paths 172 has the same configuration as first plurality of cold flow paths 152 except that first plurality of hot flow paths 172 extends in second lateral direction 128B and provide flow paths for a different fluid (in this exemplary embodiment, the fluid is a hot fluid).
  • First plurality of hot flow paths 172 include hot subflow paths 172A-172F that allow hot fluid to flow in second lateral direction 128B while also allowing hot fluid to transition between adjacent subflow paths 172A-157F by flowing at least partially vertically through transition openings 186 between adjacent subflow paths 172A-172F.
  • Each of hot subflow paths 172A-172F have a wave pattern with waves that extend in second lateral direction 128B based on a cosine curve (or sine curve depending on the starting point of the wave). However, hot subflow paths 172A-172F are offset from adjacent hot subflow paths 172A-172F by one-half wavelength in second lateral direction 128B.
  • hot subflow path 172A (a topmost subflow path), hot subflow path 172C, and hot subflow path 172E have the same configuration as one another with waves that propagate in second lateral direction 128B in phase (i.e., crests and troughs of the waves line up vertically).
  • Hot subflow path 172B, hot subflow path 172D, and hot subflow path 172F (a bottommost subflow path) also have the same configuration as one another with waves that propagate in second lateral direction 128B in phase.
  • hot subflow paths 172B, 172D, and 172F are offset from hot subflow paths 172A, 172C, and 172E one-half wavelength such that the crests of hot subflow paths 172A, 172C, and 172E interconnect with the troughs of hot subflow paths 172B, 172D, and 172F (and vice-versa) to form transition openings 186 through which hot fluid can flow into adjacent hot subflow paths 172A-172F.
  • hot subflow paths 172A-172F are shown as having the same amplitude and wavelength, other embodiments can include hot subflow paths 172A-172F that have differing amplitudes and wavelengths.
  • other pluralities of hot flow paths 174-184 can have different configurations such that those hot subflow paths (which are part of each plurality of hot flow paths 174-184) have differing amplitudes, wavelengths, and/or orientations.
  • Transition openings 186 that interconnect hot subflow paths 172A-172F can have as large or small cross-sectional areas as desired and, in other embodiments, heat exchanger 110 may not include transition openings 186 and instead hot subflow paths 172A-172F are discrete and fluidically isolated from one another.
  • Hot subflow paths 172A-172F are shown as having a substantially circular cross-sectional area due to walls 112 having a varying thickness to form the circular cross-sectional area. However, hot subflow paths 172A-172F can have other cross-sectional areas, such as any non-circular cross-section including eyelet-type shape or another shape.
  • the wave pattern of cold subflow paths 152A-152F and hot subflow paths 172A-172F create a weaved cross-flow configuration in which each subflow path of cold fluid flow path 150 is adjacent multiple subflow paths of hot fluid flow path 170 (and vice-versa).
  • This configuration provides for increased thermal energy transfer while minimizing the volume needed for heat exchanger 110 (i.e., increasing the thermal energy-to-volume ratio of heat exchanger 110).
  • the wave pattern and transition openings 166 and 186 between subflow paths limits the growth of boundary layers of the cold fluid and hot fluid through cold fluid flow path 150 and hot fluid flow path 170, respectively, thereby increasing the thermal energy transfer capabilities.
  • heat exchanger 110 can be constructed from multiple components such that walls 112 are constructed independently and then fastened together to form heat exchanger 110. Heat exchanger 110 can also be formed as one continuous and monolithic piece through additive manufacturing or other methods.
  • Heat exchanger 10/110 utilizes a weaved cross-flow configuration to provide increased primary surface area to improve the thermal energy transfer capabilities between a first fluid and a second fluid.
  • the weaved configuration is constructed primarily from stacked sheets/walls 12-26/112 (primary surfaces) that include waves in first lateral direction 28A/128A and second lateral direction 28B/128B.
  • Waves 12-26/112 can have a variety of configurations, including waves that are based on a sinusoidal curve.
  • Walls 12-26/112 are primary surfaces that have improved thermal energy transfer capabilities.
  • the waves of one wall 12-26/112 are offset from waves of adjacent walls 12-26/112 by one-half wavelength to form plurality of flow paths 30B-42B/152-164 and 172-184 between adjacent walls 12-26/112 through which the hot or cool fluid flows.
  • Utilizing walls 12-26/112 with waves provides an increase in primary surface area of walls 12-26/112 which in turn increases the thermal energy transfer between fluids flowing adjacent those walls 12-26/112.
  • the increase in surface area of walls 12-26/112 eliminates the need for fins (i.e., additional secondary surfaces), thereby improving efficiency of heat exchanger 10/110 by minimizing the distance thermal energy must transfer to maximize the energy transfer-to-volume ratio.
  • Additive manufacturing can be utilized to create the disclosed heat exchanger 10/110 so that all components of heat exchanger 10/110 are formed during one manufacturing process to form a continuous and monolithic structure. Further, additive manufacturing can easily and reliably form heat exchanger 10/110 with complex walls 12-26/112 or shapes and small tolerances. While the waves of walls 12-26/112 are based on sinusoidal curves in the disclosed embodiments, the waves can have a variety of configurations with alternate amplitudes, wavelengths, and other characteristics as required for optimal thermal energy transfer and to accommodate a designed flow of the first fluid and/or second fluid. Further, the waves of walls 12-26/112 can have other shapes, such as triangular waves with pointed peaks and troughs, rectangular waves with flat tops and bottoms, and/or other configurations.
  • a heat exchanger that extends laterally in a first direction and a second direction and has a first wall, a second wall, and a third wall.
  • the first wall is shaped in a wave pattern with waves that extend in both the first direction and the second direction.
  • the second wall is adjacent to and in contact with the first wall with the second wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction.
  • the waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength.
  • the third wall is adjacent to and in contact with the second wall with the third wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction.
  • the waves of the third wall are offset in the second direction from the second wall by one-half wavelength.
  • the heat exchanger also includes a first plurality of flow paths extending in the second direction with the first plurality of flow paths each bounded by the first wall and the second wall and a second plurality of flow paths extending in the first direction with the second plurality of flow paths each bounded by the second wall and the third wall.
  • the heat exchanger of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations, and/or additional components: A fourth wall adjacent to and in contact with the third wall with the fourth wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction, the waves of the fourth wall being offset from the waves of the third wall in the first direction by one-half wavelength and a third plurality of flow paths extending in the second direction with the third plurality of flow paths each bounded by the third wall and the fourth wall.
  • the waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction
  • the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  • Each flow path of the first plurality of flow paths and the second plurality of flow paths have a substantially circular cross-sectional area.
  • the first plurality of flow paths are laterally interconnected by first transition openings and the second plurality of flow paths are laterally interconnected by second transition openings such that flow through one flow path of the first plurality of flow paths can transition and flow through an adjacent flow path of the first plurality of flow paths and flow through one flow path of the second plurality of flow paths can transition and flow through an adjacent flow path of the second plurality of flow paths.
  • Each flow path of the first plurality of flow paths are fluidically isolated from one another and each flow path of the second plurality of flow paths are fluidically isolated from one another.
  • the first wall contacts and connects to the second wall along a plurality of contact lines extending in the second direction to form the fluidically isolated first plurality of flow paths extending in the second direction.
  • the second wall contacts and connects to the third wall along a plurality of contact lines extending in the first direction to form the fluidically isolated second plurality of flow paths extending in the first direction.
  • the first wall, second wall, and third wall are constructed by additive manufacturing so that the heat exchanger is one continuous and monolithic component.
  • the waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have an amplitude that is greater than an amplitude of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  • the amplitude of the waves in the first direction of the first wall, second wall, and third wall is at least 1.5 times greater than the amplitude of the waves in the second direction of the first wall, second wall, and third wall.
  • the waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have a wavelength that is greater than a wavelength of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  • the first wall, second wall, and third wall are constructed from a material having low thermal conductivity.
  • a gas turbine engine comprising the heat exchanger disclosed above.
  • a first fluid flows through the first plurality of flow paths and a second fluid flows through the second plurality of flow paths.
  • a method of forming a heat exchanger includes forming a first wall with waves that extend laterally in both a first direction and in a second direction.
  • the method also includes forming a second wall adjacent to and in contact with the first wall with waves that are based on a sinusoidal curve and extend laterally in both the first direction and in the second direction.
  • the waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength.
  • the method also includes forming a third wall adjacent to and in contact with the second wall with waves that extend laterally in both the first direction and in the second direction.
  • the waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.
  • the first wall and the second wall bound a first plurality of flow paths that extend in the second direction
  • the second wall and the third wall bound a second plurality of flow paths that extend in the first direction.
  • the waves of the first, second, and third walls can be based on a sinusoidal curve.
  • the method of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations, steps, and/or additional components: Additively manufacturing the first wall, second wall, and third wall.
  • the waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction, and wherein the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  • a method of transferring thermal energy through the use of a heat exchanger includes flowing a first fluid through a first plurality of flow paths bounded by a first wall and a second wall.
  • the first wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both a first direction and a second direction.
  • the second wall is adjacent to and in contact with the first wall and having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction.
  • the waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength.
  • the method also includes flowing a second fluid through a second plurality of flow paths bounded by the second wall and a third wall.
  • the third wall is adjacent to and in contact with the second wall.
  • the third wall has a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction.
  • the waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.

Landscapes

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

Abstract

A heat exchanger is disclosed herein that includes three walls (12,14,16) that are each shaped in a wave pattern with the waves that extend in both a first lateral direction and a second lateral direction. A second wall is adjacent to and in contact with a first wall with the waves of the second wall being offset from the waves of the first wall by one-half wavelength in the first direction. The third wall is adjacent to and in contact with the second wall with the waves of the third wall being offset from the waves o the second wall by one-half wavelength in the second direction. The first wall and second wall form a first plurality of flow paths (30B) extending in the second direction, and the second wall and the third wall form a second plurality of flow paths (32B) extending in the first direction.

Description

    FIELD OF THE INVENTION
  • The present invention relates to heat exchangers and, in particular, to a method for forming a heat exchanger and to a heat exchanger that utilizes a weaved cross-flow configuration to increase the thermal energy transfer primary surface area of the heat exchanger.
  • BACKGROUND
  • Heat exchangers aim to transfer heat between a hot fluid and a cool fluid. To increase the efficiency of heat exchangers, walls (primary surfaces) and fins (secondary surfaces) are utilized to increase the surface area through which thermal energy can transfer. The heat transfer through primary surface is very good because the walls are thin and the distance the thermal energy needs to travel is relatively small. The heat transfer through secondary surfaces is less efficient than primary surfaces because the thermal energy must travel a longer distance along the length of the fins. However, with conventional manufacturing techniques, the most compact heat exchangers (i.e., high surface area per unit volume) are achieved through increasing secondary surface area by adding fins rather than through the addition of primary surface area.
  • SUMMARY
  • A heat exchanger is disclosed herein that extends laterally in a first direction and a second direction. The heat exchanger includes three walls. A first wall is shaped in a wave pattern with waves that extend in both the first direction and the second direction. These waves can have a variety of configurations, including waves based on a sinusoidal curve in both the first direction and the second direction. The second wall is adjacent to and in contact with the first wall. The second wall is also shaped in a wave pattern with waves that extend in both the first direction and the second direction. The waves of the second wall are offset in the first direction from the first wall by one-half wavelength. The third wall is adjacent to and in contact with the second wall. The third wall is also shaped in a wave pattern with waves that extend in both the first direction and the second direction. The waves of the third wall are offset in the second direction from the second wall by one-half wavelength. The first wall and second wall form a first plurality of flow paths extending in the second direction, and the second wall and third wall form a second plurality of flow paths extending in the first direction.
  • A method of forming a heat exchanger includes forming a first wall with waves that extend laterally in both a first direction and in a second direction. The method also includes forming a second wall adjacent to and in contact with the first wall with waves that are based on a sinusoidal curve and extend laterally in both the first direction and in the second direction. The waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength. The method also includes forming a third wall adjacent to and in contact with the second wall with waves that extend laterally in both the first direction and in the second direction. The waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength. The first wall and the second wall bound a first plurality of flow paths that extend in the second direction, and the second wall and the third wall bound a second plurality of flow paths that extend in the first direction. The waves of the first, second, and third walls can be based on a sinusoidal curve.
  • A method of transferring thermal energy through the use of a heat exchanger includes flowing a first fluid through a first plurality of flow paths bounded by a first wall and a second wall. The first wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both a first direction and a second direction. The second wall is adjacent to and in contact with the first wall and having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction. The waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength. The method also includes flowing a second fluid through a second plurality of flow paths bounded by the second wall and a third wall. The third wall is adjacent to and in contact with the second wall. The third wall has a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction. The waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.
  • BRIEF DESCRIPTION OF THE DRAWINGS
    • FIG. 1A is a perspective view of a portion of a heat exchanger.
    • FIG. 1B is a second perspective view of the heat exchanger in FIG. 1A.
    • FIG. 1C is a perspective view of a plurality of flow paths through the heat exchanger in FIG. 1A.
    • FIG. 2 is a second embodiment of a heat exchanger.
    DETAILED DESCRIPTION
  • A heat exchanger is disclosed herein that utilizes a weaved cross-flow configuration to transfer thermal energy between a first fluid and a second fluid. The weaved configuration is constructed primarily from stacked sheets/walls that include waves in a first lateral direction and a second lateral direction. The waves can have a variety of configurations, including waves that are based on a sinusoidal (i.e., cosine or sine) curve. The walls are primary surfaces that have improved thermal energy transfer capabilities. The waves of one wall are offset from waves of adjacent walls by one-half wavelength to form a plurality of flow paths between adjacent walls through which the first or second fluid flows. Utilizing walls with waves provides an increase in primary surface area of the walls which in turn increases the thermal energy transfer between fluids flowing adjacent those walls. The increase in surface area of the walls eliminates the need for fins (i.e., additional secondary surface), thereby improving efficiency of the heat exchanger by maximizing the energy transfer-to-volume ratio.
  • Additive manufacturing can be utilized to create the disclosed heat exchanger so that all components of the heat exchanger are formed during one manufacturing process to form a continuous and monolithic structure. Further, additive manufacturing can easily and reliably form the heat exchanger with complex walls/shapes and small tolerances. In the context of this application, continuous and monolithic means formed as a single unit without seams, weld lines, adhesive lines, or any other discontinuities. The waves of the walls (which, for example, are based on sinusoidal curves) can have alternate amplitudes, wavelengths, and other characteristics as required for optimal thermal energy transfer and to accommodate a designed flow of the first fluid and/or second fluid. Further, the waves can have a variety of shapes, such as triangular waves with pointed peaks and troughs, rectangular waves with flat tops and bottoms, and/or other configurations.
  • FIG. 1A is a perspective cross-sectional view of a portion of a heat exchanger, FIG. 1B is a second perspective view of the heat exchanger in FIG. 1A, and FIG. 1C is a perspective view of a plurality of flow paths through the heat exchanger in FIG. 1A. Heat exchanger 10 includes first wall 12, second wall 14, third wall 16, fourth wall 18, fifth wall 20, sixth wall 22, seventh wall 24, and eighth wall 26. Walls 12-26 are primary surfaces, extend laterally in first lateral direction 28A and second lateral direction 28B, and are vertically adjacent one another in vertical direction 28C. The terms "lateral" and "vertical" in the context of FIG. 1A and the rest of this application are merely relative terms and not intend to suggest any limitation into the orientation of the disclosed heat exchanger relative to any particular reference point. While the waves of walls 12-26 are described as being based on sinusoidal curves, the waves can have other configurations and/or orientations. Walls 12-26 with waves based on sinusoidal curves is just an exemplary embodiment of heat exchanger 10.
  • First wall 12 and second wall 14 contact one another at first contact lines 30A to form first plurality of flow paths 30B, second wall 14 and third wall 16 contact one another at second contact lines 32A to form second plurality of flow paths 32B, third wall 16 and fourth wall 18 contact one another at third contact lines 34A to form third plurality of flow paths 34B, fourth wall 18 and fifth wall 20 contact one another at fourth contact lines 36A to form fourth plurality of flow paths 36B, fifth wall 20 and sixth wall 22 contact one another at fifth contact lines 38A to form fifth plurality of flow paths 38B, sixth wall 22 and seventh wall 24 contact one another at sixth contact lines 40A to form sixth plurality of flow paths 40B, and seventh wall 24 and eighth wall 26 contact one another at seventh contact line 42A to form seventh plurality of flow paths 42B.
  • First wall 12 includes waves having first wall crests 12A and first wall troughs 12B, second wall 14 includes waves having second wall crests 14A and second wall troughs 14B, third wall 16 includes waves having third wall crests 16A and third wall troughs 16B, fourth wall 18 includes waves having fourth wall crests 18A and fourth wall troughs 18B, fifth wall 20 includes waves having fifth wall crests 20A and fifth wall troughs 20B, sixth wall 22 includes waves having sixth wall crests 22A and sixth wall troughs 22B, seventh wall 24 includes waves having seventh wall crests 24A and seventh wall troughs 24B, and eighth wall 26 includes waves having eighth wall crests 26A and eighth wall troughs 26B.
  • Heat exchanger 10 is formed by stacking walls 12-26 vertically to form a plurality of flow paths 30B-42B (seen most easily in FIG. 1C) through which hot fluid and cold fluid can flow (in a cross-flow configuration) to transfer thermal energy to cool the hot fluid through primary surface walls 12-26. While shown as having eight walls 12-26, heat exchanger 10 can have any number of walls that form the plurality of flow paths 30B-42B, including only three walls 12-16 that form two pluralities of flow paths 30B and 32B or more than eighth walls forming more than seven pluralities of flow paths (as shown in FIG. 1B (unlabeled)). Additionally, heat exchanger 10 can extend in a lateral direction any distance, including in first lateral direction 28A a distance that is equal to a distance that heat exchanger 10 extends in second lateral direction 28B. Alternately, heat exchanger 10 can extend in first lateral direction 28A a different distance than that in second lateral direction 28B to form heat exchanger 10 that has a rectangular footprint or another shape. In such configurations, the waves of walls 12-26 would repeat so as to have multiple wavelengths in first lateral direction 28A and second lateral direction 28B to provide sufficient thermal energy transfer surface area to meet thermal energy transfer requirements.
  • As shown in FIGS. 1A and 1B, walls 12-26 each include waves in both first lateral direction 28A and second lateral direction 28B that are based on a sinusoidal curve. However, adjacent walls are offset from one another either in first lateral direction 28A or second lateral direction 28B by one-half wavelength, resulting in crests 12A-26A contacting troughs 12B-26B of adjacent walls 12-26 to form a plurality of discrete flow paths 30B-42B. Adjacent walls 12-26 being offset by one-half wavelength in either first lateral direction 28A or second lateral direction 28B forms contact lines 30A-42A that, along with adjacent walls 12-26, bound the plurality of discrete flow paths 30B-42B. Such a configuration provides a weaved, cross-flow heat exchanger 10 with increased primary surface area. Nearly the entire surface area of each flow path of the plurality of flow paths 30B-42B is primary heat transfer area resulting in increased heat transfer and reduced volume of heat exchanger 10. Each wall 12-26 will be described below and its relation to adjacent walls. However, other configurations of heat exchanger 10 can have different orientations such that "lateral" and "vertical" are used herein only to describe component in relation to one another with regards to FIG.S 1A-1C and do not require heat exchanger 10 be oriented such that walls 12-26 extend in a horizontal direction or any particular special direction.
  • First wall 12 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. The waves of first wall 12 are based on a sinusoidal curve that repeat in both directions 28A and 28B. Additionally, a person of ordinary skill in the art will recognize that the waves can be based on either cosine or sine curves, which are essentially the same and are only different as to the starting point of each type of wave. For convenience, this application will describe the disclosed heat exchanger 10 using cosine terminology. As shown in FIG. 1A, the waves of first wall 12 show two complete wavelengths in first lateral direction 28A and four complete wavelengths in second lateral direction 28B. In FIG. 1B, walls 12-26 are shown to have at least five waves in both directions 28A and 28B. Multiple first wall crests 12A (the peaks of the waves) and multiple first wall troughs 12B (the valleys of the waves) are in each direction 28A and 28B. However, since the waves extend both in first lateral direction 28A and second lateral direction 28B, first wall crests 12A and first walls troughs 12B are lines that extend in either first lateral direction 28A or second lateral direction 28B. For example, as shown by thick line 30A (first contact lines 30A), first wall 12 contacts second wall 14 along first wall troughs 12B that extend in second lateral direction 28B. However, first contact lines 30A do include multiple first wall crests 12A extending along lines in first lateral direction 28A. Thus, first wall crests 12A and first wall troughs 12B form a checkered pattern with a lowest point of first wall 12 being at a point where first wall troughs 12B in first lateral direction 28A intersect first wall troughs 12B in second lateral direction 28B.
  • First wall 12 can have any thickness, including a constant thickness in one or both directions 28A and 28B or a varying thickness depending on structural and/or thermal energy transfer needs. The thickness of first wall 12 (and other walls 14-26) can be configured to alter the cross-sectional flow area of the plurality of flow paths 30B-42B. For example, the cross-sectional flow area can be substantially circular (as shown in FIG. 2) or another shape. Additionally, the amplitude and/or wavelength of first wall 12 can be anything suitable for thermal energy transfer, can be the same or different than the amplitude and/or wavelength of the other walls 14-26, and/or can be different in first lateral direction 28A as compared to second lateral direction 28B. For example, the waves of first wall 12 in first lateral direction 28A can be at least 1.5 times greater in amplitude than the waves of first wall 12 in second lateral direction 28B. However, for walls 12-26 to line up, first wall 12, third wall 16, fifth wall 20, and seventh wall 24 may need to have the same amplitude and wavelength (and similarly, second wall 14, fourth wall 18, sixth wall 20, and eighth wall 26).
  • Second wall 14 is similar to first wall 12 in that second wall 14 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Second wall 14 is adjacent to and in contact with first wall 14 (on a top side) and third wall 18 (on a bottom side). The waves of second wall 14 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of second wall 14 are offset from first wall 12 in first lateral direction 28A by one-half wavelength. Because second wall 14 is offset from first wall 12 in first lateral direction 28A, second wall crests 14A (in first lateral direction 28A) contact first wall troughs 12B (in first lateral direction 28A) to form first contact lines 30A, which extend in second lateral direction 28B. First contact lines 30A are where first wall 12 and second wall 14 connect to one another to bound first plurality of flow paths 30B. As with first wall 12, second wall 14 has multiple second wall crests 14A and troughs 14B in both first lateral direction 28A and second lateral direction 28B. The waves of second wall 14 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12 in one or both directions 28A and 28B. Additionally, similar to first wall 12, the thickness of second wall 12 can be constant or varying in any direction 28A and 28B.
  • First plurality of flow paths 30B are formed and bounded by first wall 12 and second wall 14 (and first contact lines 30A) and extend in second lateral direction 28B. As seen most easily in FIG. 1C, which shows plurality of flow paths 30B-42B without the presence of walls 12-26, first plurality of flow paths 30B have undulating cross-sectional flow areas due to the waves of first wall 12 and second wall 14, which enhances heat transfer by limiting boundary layer growth through first plurality of flow paths 30B. In FIGS. 1A-1C, each of the first plurality of flow paths 30B are fluidically isolated from adjacent flow paths of first plurality of flow paths 30B. However, as shown in FIG. 2, first plurality of flow paths 30B can be laterally or vertically interconnected such that flow through one flow path of first plurality of flow paths 30B can transition and flow through an adjacent flow path of first plurality of flow paths 30B or adjacent pluralities of flow paths 32B-42B. With such a configuration, first contact lines 30A are not continuous along an entire distance of first wall 12 and second wall 14 in second lateral direction 28B and rather there are transition openings between adjacent flow paths of first plurality of flow paths 30B. The cross-sectional flow area of each of the first plurality of flow paths 30B can be similar to adjacent flow paths or can be differing, such as flow paths of the first plurality of flow paths 30B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape. Fluid flowing through each of first plurality of flow paths 30B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Third wall 16 is similar to second wall 14 in that third wall 16 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Third wall 16 is adjacent to and in contact with second wall 14 (on a top side) and fourth wall 18 (on a bottom side). The waves of third wall 16 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of third wall 16 are offset from second wall 14 in second lateral direction 28B by one-half wavelength. Because third wall 16 is offset from second wall 14 in second lateral direction 28B, third wall crests 16A (in second lateral direction 28B) contact second wall troughs 14B (in second lateral direction 28B) to form second contact lines 32A, which extend in first lateral direction 28A. Second contact lines 32A are where second wall 14 and third wall 16 connect to one another to bound second plurality of flow paths 32B. As with second wall 14, third wall 16 has multiple third wall crests 16A and third wall troughs 16B in both first lateral direction 28A and second lateral direction 28B. The waves of third wall 16 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12 and/or second wall 14 in one or both directions 28A and 28B. In one embodiment, the waves in first lateral direction 28A of first wall 12, second wall 14, and third wall 16 have an amplitude and/or wavelength that is greater than an amplitude and/or wavelength of the waves in second lateral direction 28B of first wall 12, second wall 14, and third wall 16. Additionally, similar to first wall 12 and second wall 14, a thickness of third wall 16 can be constant or varying in any direction 28A and 28B.
  • Second plurality of flow paths 32B are formed and bounded by second wall 14 and third wall 16 (and second contact lines 32A) and extend in first lateral direction 28A. Second plurality of flow paths 32B form a weaved, cross-flow pattern with first plurality of flow paths 30B and third plurality of flow paths 34B. For example, hot fluid can flow through second plurality of flow paths 32B while cold fluid flows through first plurality of flow paths 30B and third plurality of flow paths 34B such that thermal energy transfers across second wall 14 and third wall 16. Second plurality of flow paths 32B can be similar in configuration and functionality to first plurality of flow paths 30B (except that second plurality of flow paths 32B extend in first lateral direction 28A). In FIGS. 1A-1C, each flow path of second plurality of flow paths 32B are fluidically isolated from adjacent flow paths of second plurality of flow paths 32B. However, as shown in FIG. 2, second plurality of flow paths 32B can be laterally or vertically interconnected such that flow through one flow path of second plurality of flow paths 32B can transition and flow through an adjacent flow path of second plurality of flow paths 32B. With such a configuration, second contact lines 32A are not continuous along an entire distance of second wall 14 and third wall 16 in first lateral direction 28A and rather there are transition openings between adj acent flow paths of second plurality of flow paths 32B. The cross-sectional flow area of each of the second plurality of flow paths 32B can be similar to adjacent flow paths or can be differing, such as flow paths of the second plurality of flow paths 32B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape. Fluid flowing through each of second plurality of flow paths 32B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Fourth wall 18 is similar to third wall 16 in that fourth wall 18 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Fourth wall 18 is adjacent to and in contact with third wall 16 (on a top side) and fifth wall 20 (on a bottom side). The waves of fourth wall 18 are based on a cosine curve (or sine curve) that repeat in both directions 28A and 28B. The waves of fourth wall 18 are offset from third wall 16 in first lateral direction 28A by one-half wavelength. Because fourth wall 18 is offset from third wall 16 in first lateral direction 28A, fourth wall crests 18A (in second lateral direction 28B) contact third wall troughs 16B (in second lateral direction 28B) to form third contact lines 34A, which extend in second lateral direction 28B. Third contact lines 34A are where third wall 16 and fourth wall 18 connect to one another to bound third plurality of flow paths 34B. As with third wall 16, fourth wall 18 has multiple fourth wall crests 18A and fourth wall troughs 18B in both first lateral direction 28A and second lateral direction 28B. The waves of fourth wall 18 can have the same or differing amplitudes and/or wavelengths as the waves of first wall 12, second wall 14, and/or third wall 16 in one or both directions 28A and 28B. Additionally, similar to first wall 12, second wall 14, and third wall 16, the thickness of fourth wall 18 can be constant or varying in any direction 28A and 28B.
  • Third plurality of flow paths 34B are formed and bounded by third wall 16 and fourth wall 18 (and third contact lines 34A) and extend in second lateral direction 28B. Third plurality of flow paths 34B form a weaved, cross-flow pattern with second plurality of flow paths 32B and fourth plurality of flow paths 36B. For example, hot fluid can flow through first plurality of flow paths 30B and third plurality of flow paths 34B while cold fluid flows through second plurality of flow paths 32B and fourth plurality of flow paths 36B such that thermal energy transfers through second wall 14, third wall 16, and fourth wall 18. Third plurality of flow paths 34B can be similar in configuration and functionality to first plurality of flow paths 30B and second plurality of flow paths 32B (except that third plurality of flow paths 34B extend in second lateral direction 28B and are offset from first plurality of flow paths 30B by one-half wavelength in first lateral direction 28A). In FIGS. 1A-1C, each flow path of third plurality of flow paths 34B are fluidically isolated from adjacent flow paths of third plurality of flow paths 34B. However, as shown in FIG. 2, third plurality of flow paths 34B can be laterally or vertically interconnected such that flow through one flow path of third plurality of flow paths 34B can transition and flow through an adjacent flow path of third plurality of flow paths 34B. With such a configuration, third contact lines 34A are not continuous along an entire distance of third wall 16 and fourth wall 18 in second lateral direction 28B and rather there are transition openings between adjacent flow paths of third plurality of flow paths 34B. The cross-sectional flow area of each of the third plurality of flow paths 34B can be similar to adjacent flow paths or can be differing, such as flow paths of the third plurality of flow paths 34B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape. Fluid flowing through each of third plurality of flow paths 34B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Fifth wall 20 is similar to fourth wall 18 in that fifth wall 20 is shaped in a wave pattern with waves extending both in first lateral direction 28A and second lateral direction 28B. Fifth wall 20 is adjacent to and in contact with fourth wall 18 (on a top side) and sixth wall 22 (on a bottom side). Fifth wall 20 has the same orientation as first wall 12 with the waves of fifth wall 20 being offset from fourth wall 18 in second lateral direction 28B by one-half wavelength. The configuration of heat exchanger 10 downward from fifth wall 20 repeats so as to have the same configuration of heat exchanger 10 between first wall 12 and fifth wall 20. Because fifth wall 20 is offset from fourth wall 18 in second lateral direction 28B, fifth wall crests 20A (in first lateral direction 28A) contact fourth wall troughs 18B (in first lateral direction 28A) to form fourth contact lines 36A, which extend in first lateral direction 28A. Fourth contact lines 36A are where fourth wall 18 and fifth wall 20 connect to one another to bound fourth plurality of flow paths 36B. As with fourth wall 18, fifth wall 20 has multiple fifth wall crests 20A and fifth wall troughs 20B in both first lateral direction 28A and second lateral direction 28B. The waves of fifth wall 20 can have the same or differing amplitudes and/or wavelengths as the waves of walls 12-18 in one or both directions 28A and 28B. Additionally, similar to walls 12-18, the thickness of fifth wall 20 can be constant or varying in any direction 28A and 28B.
  • Fourth plurality of flow paths 36B are formed and bounded by fourth wall 18 and fifth wall 20 (and fourth contact lines 36A) and extend in first lateral direction 28A. Fourth plurality of flow paths 36B form a weaved, cross-flow pattern with third plurality of flow paths 34B and fifth plurality of flow paths 38B. For example, hot fluid can flow through first plurality of flow paths 30B and third plurality of flow paths 34B while cold fluid flows through second plurality of flow paths 32B and fourth plurality of flow paths 36B such that thermal energy transfers through second wall 14, third wall 16, fourth wall 18, and fifth wall 20. Fourth plurality of flow paths 36B can be similar in configuration and functionality to other pluralities of flow paths 30B-42B. In FIGS. 1A-1C, each flow path of fourth plurality of flow paths 36B are fluidically isolated from adjacent flow paths of fourth plurality of flow paths 36B. However, as shown in FIG. 2, fourth plurality of flow paths 36B can be laterally or vertically interconnected such that flow through one flow path of fourth plurality of flow paths 36B can transition and flow through an adjacent flow path of fourth plurality of flow paths 36B. With such a configuration, fourth contact lines 36A are not continuous along an entire distance of fourth wall 18 and fifth wall 20 in first lateral direction 28A and rather there are transition openings between adjacent flow paths of fourth plurality of flow paths 36B. The cross-sectional flow area of each of the fourth plurality of flow paths 36B can be similar to adjacent flow paths or can be differing, such as flow paths of the fourth plurality of flow paths 36B alternating between a flow path that has a circular cross-sectional flow area and a flow path that has an eyelet-type shape. Fluid flowing through each of fourth plurality of flow paths 36B can be hot or cold gas or liquid, and the fluid can flow in alternating directions (i.e., fluid in one flow path flows in the opposite direction to fluid in another/adjacent flow path).
  • Sixth wall 22 has the same orientation, configuration, and functionality as second wall 14. Sixth wall 22 is adjacent to and in contact with fifth wall 20 (along fifth contact lines 38A) to form fifth plurality of flow paths 38B. Fifth plurality of flow paths 38B has the same orientation, configuration, and functionality as first plurality of flow paths 30B. Seventh wall 24 has the same orientation, configuration, and functionality as third wall 16. Seventh wall 24 is adjacent to and in contact with sixth wall 22 (along sixth contact lines 40A) to form sixth plurality of flow paths 40B. Sixth plurality of flow paths 40B has the same orientation, configuration, and functionality as second plurality of flow paths 32B. Eighth wall 26 has the same orientation, configuration, and functionality as fourth wall 18. Eighth wall 26 is adjacent to and in contact with seventh wall 24 (along seventh contact lines 42A) to form seventh plurality of flow paths 42B. Seventh plurality of flow paths 42B has the same orientation, configuration, and functionality as third plurality of flow paths 34B.
  • Heat exchanger 10 can extend in vertical direction 28C by including additional walls having the same orientation as walls 12-26 (as shown in FIG. 1B) and/or by increasing the amplitude of the waves of walls 12-26. Heat exchanger 10 can be constructed from a variety of materials, including conventional materials and materials that have lower thermal conductivity properties than materials conventionally used to construct heat exchangers. Because the primary thermal energy transfer surface area of each flow path of the plurality of flow paths 30B-42B is increased due to the wave pattern of walls 12-26 of heat exchanger 10, the amount of thermal energy transfer of heat exchanger 10 is increased as compared to prior art heat exchangers. With an increase in primary surface area, heat exchanger 10 can be constructed from materials that have low thermal conductivity properties, such as plastics or composites. For example, heat exchanger 10 may be constructed from reinforced nylon, acrylonitrile butadiene styrene, epoxy, or urethane methacrylate. If desired, heat exchanger 10 can be located within a machine that requires increased thermal energy transfer capabilities and a small volume, such as a gas turbine engine.
  • While heat exchanger 10 can be constructed from multiple components such that each of walls 12-26 is constructed independently and then fastened together along contact lines 30A-42A, heat exchanger 10 can be formed as one continuous and monolithic piece through additive manufacturing or other methods such that heat exchanger 10 is formed as a single unit without seams, weld lines, adhesive lines, or any other discontinuities. To construct heat exchanger 10, first wall 12 is formed with waves based on a cosine curve extending in both first lateral direction 28A and second lateral direction 28B.
  • Next, second wall 14 is formed with waves based on a cosine curve extending in both directions 28A and 28B with the waves being offset in first lateral direction 28A from first wall 12 by one-half wavelength to form first plurality of flow paths 30B. Second wall 14 is adjacent to first wall 12 and can be either fastened to first wall 12 along first contact lines 30A, or second wall 14 can be formed simultaneously with first wall 12 such that first wall 12 and second wall 14 are one continuous and monolithic piece.
  • Then, third wall 16 is formed with waves based on a cosine curve extending in both directions 28A and 28B with the waves being offset in second lateral direction 28A from second wall 14 by one-half wavelength to form second plurality of flow paths 32B. Third wall 16 is adjacent to second wall 14 and can be either fastened to second wall 14 along second contact liens 32A, or third wall 16 can be formed simultaneously with second wall 14 (and possibly first wall 12) such that second wall 14 and third wall 16 are one continuous and monolithic piece. Subsequent walls 18-26 (or more) can be formed utilizing similar steps. Additionally, a method of forming heat exchanger 10 can start at a bottom wall (a wall that is on a bottom side of heat exchanger 10) and build up walls from there, or the method can form heat exchanger 10 building the walls in first lateral direction 28A or second lateral direction 28B.
  • While the disclosed heat exchanger 10 will be described as transferring thermal energy between two fluids, a first fluid and a second fluid, a person skilled in the art will recognize that the disclosed heat exchanger 10 may be used with more than two fluids provided it is constructed with sufficient pluralities of flow paths to accommodate more than two heat exchange fluids. First, the first fluid (which can be a hot fluid or cold fluid) is conveyed/flowed in second lateral direction 28B through first plurality of flow paths 30B and, if necessary, third plurality of flow paths 34B, fifth plurality of flow paths 38B, and seventh plurality of flow paths 42B. Then, the second fluid (which can be a hot fluid or a cold fluid but should be a fluid that has a different temperature than the first fluid) is conveyed/flowed in first lateral direction 28A through second plurality of flow paths 32B and, if necessary, fourth plurality of flow paths 36B and sixth plurality of flow paths 40B. Because of the weaved, cross-flow configuration of heat exchanger 10 having walls 12-26 with a wave pattern, thermal energy transfer between the first fluid and second fluid is rapid because the thermal energy transfer surface areas of each flow path of the pluralities of flow paths 30B-42B is large and direct from the hot fluid to the cold fluid (i.e., no conduction along a fin) and the undulating nature of each flow path creates enhances heat transfer.
  • FIG. 2 is a second embodiment of a heat exchanger. Heat exchanger 110 is similar to heat exchanger 10 in FIGS. 1A-1C except that heat exchanger 110 includes sub flow paths as part of a plurality of flow paths that are vertically connected by transition openings. In FIG. 2, a plurality of flow paths includes multiple subflow paths that are connected to adjacent subflow paths vertically to allow for a fluid flowing through the plurality of flow paths to transition and flow through an adjacent subflow path while still providing an increase in primary surface area for optimal heat transfer. While FIG. 2 shows subflow paths connected to adjacent subflow paths vertically, the orientation and configuration of heat exchanger 110 can be such that subflow paths can be connected to adjacent subflow paths horizontally (i.e., the pluralities of flow paths 30B-42B in heat exchanger 10 are connected to one another by transition openings between adjacent flow paths). While the pluralities of flow paths of heat exchanger 110 can be described with regards to walls in a similar fashion to that of heat exchanger 10, it may be easier to understand the configuration of heat exchanger 110 by describing the pluralities of flow paths through heat exchanger 110 rather than the walls that bound the pluralities of flow paths.
  • Heat exchanger 110 includes walls 112 bounding cold fluid flow path 150 (which encompasses all cold fluid flow paths, including the pluralities of cold flow paths as well as subflow paths) extending in first lateral direction 128A and hot fluid flow path 170 (which encompasses all hot fluid flow paths, including the pluralities of hot flow paths as well as subflow paths) extending in second lateral direction 128B. While this disclosure describes the flow paths as being for "hot" fluid and "cold" fluid, this is done for simplicity such that the temperature and/or type of fluid is exemplary and any type of fluid and even more than two fluids can be utilized in heat exchanger 110. Cold fluid flow path 150 includes first plurality of cold flow paths 152, second plurality of cold flow paths 154, third plurality of cold flow paths 156, fourth plurality of cold flow paths 158, fifth plurality of cold flow paths 160, sixth plurality of cold flow paths 162, and seventh plurality of cold flow paths 164. Each cold plurality of cold flow paths 152-164 includes six cold subflow paths, with first plurality of cold flow paths 152 having first cold subflow paths 152A-152F (while not labeled in FIG. 2 for simplicity, the other pluralities of flow paths 154-164 also include six cold subflow paths of similar configuration and functionality). Between cold subflow paths 152A-152F are transition openings 166, which provide a path through which cold fluid can flow between adjacent cold subflow paths 152A-152F. Similarly, hot fluid flow path 170 includes first plurality of hot flow paths 172, second plurality of hot flow paths 174, third plurality of hot flow paths 176, fourth plurality of hot flow paths 178, fifth plurality of hot flow paths 180, sixth plurality of hot flow paths 182, and seventh plurality of hot flow paths 184. Each plurality of hot flow paths 172-184 includes six hot subflow paths, with first plurality of hot flow paths 172 having first hot subflow paths 172A-172F (while not labeled in FIG. 2 for simplicity, the other pluralities of hot flow paths 174-184 also include six hot subflow paths of similar configuration and functionality). Between hot subflow paths 172A-172F are transition openings 186, which provide a path through which hot fluid can flow between adjacent hot subflow paths 172A-172F. The below disclosure will focus on first plurality of cold flow paths 152 of cold fluid flow path 150 and first plurality of hot flow paths 172 of hot fluid flow path 170. However, the other pluralities of cold flow paths 154-164 and hot flow paths 174-184 have similar configurations and functionalities.
  • Cold fluid flow path 150 includes pluralities of cold flow paths 152-164 that are columns of flow paths arranged so as to be laterally adjacent to at least one other plurality of cold flow paths 152-164. Each of the pluralities of cold flow paths 152-164 extend in first lateral direction 128A such that cold fluid flowing through the plurality of cold flow paths 152-164 flows substantially in first lateral direction 128A. As shown, there are seven pluralities of cold flow paths 152-164. However, for more or less thermal energy transfer capabilities, heat exchanger 110 can include a lesser or greater number of pluralities of cold flow paths 152-164 for accommodating cold fluid flow. Additionally, while each plurality of cold flow paths 152-164 is shown as having six cold subflow paths 152A-152F, heat exchanger 110 can include less than six or greater than six cold subflow paths as the design requires (and, for example, space within a gas turbine engine allows). In the embodiment of heat exchanger 110 shown in FIG. 2, adjacent pluralities of cold flow paths 152-164 do not provide for cold fluid flow therebetween and cold fluid is only able to flow between adjacent cold subflow paths 152A-152F within a single plurality of cold flow paths 152-164. However, other embodiments of heat exchanger 110 can include openings that allow cold fluid to transition between adjacent pluralities of cold flow paths 152-164.
  • First plurality of cold flow paths 152 is shown in a cross-sectional representation so that cold subflow paths 152A-152F are more easily seen. First plurality of cold flow paths 152 (and other pluralities of cold flow paths 154-164 and 172-184) extend vertically and are bounded by walls 112. First plurality of cold flow paths 152 include cold subflow paths 152A-152F, which allow cold fluid to flow in first lateral direction 128A while also allowing cold fluid to transition between adjacent cold subflow paths 152A-152F. Cold fluid is able to flow between adjacent cold subflow paths 152A-152F by flowing at least partially vertically through transition openings 166 between adjacent cold subflow paths 152A-152F. Each of cold subflow paths 152A-152F have a wave pattern with waves that extend in first lateral direction 128A based on a cosine curve (or sine curve depending on the starting point of the wave). However, cold subflow paths 152A-152F are offset from adjacent cold subflow paths 152A-152F by one-half wavelength in first lateral direction 128A.
  • For example, as shown in FIG. 2, cold subflow path 152A (a topmost subflow path), cold subflow path 152C, and cold subflow path 152E have the same configuration as one another with waves that propagate in first lateral direction 128A in phase (i.e., crests and troughs of the waves line up vertically). Cold subflow path 152B, cold subflow path 152D, and cold subflow path 152F (a bottommost subflow path) also have the same configuration as one another with waves that propagate in first lateral direction 128A in phase. However, cold subflow paths 152B, 152D, and 152F are offset from cold subflow paths 152A, 152C, and 152E one-half wavelength such that the crests of cold subflow paths 152A, 152C, and 152E interconnect with the troughs of cold subflow paths 152B, 152D, and 152F (and vice-versa) to form transition openings 166 through which cold fluid can flow into adjacent cold subflow paths 152A-152F. While cold subflow paths 152A-152F are shown as having the same amplitude and wavelength, other embodiments can include cold subflow paths 152A-152F that have differing amplitudes and wavelengths. Further, other pluralities of cold flow paths 154-164 can have different configurations such that those cold subflow paths (which are part of each plurality of cold flow paths 154-164) have differing amplitudes, wavelengths, and/or orientations.
  • Transition openings 166 that interconnect cold subflow paths 152A-152F can have as large or small cross-sectional area as desired and, in other embodiments, heat exchanger 110 may not include transition openings 166 and instead cold subflow paths 152A-152F are discrete and fluidically isolated from one another.
  • Cold subflow paths 152A-152F are shown as having a substantially circular cross-sectional area due to walls 112 having a varying thickness to form the circular cross-sectional area. However, cold subflow paths 152A-152F can have other cross-sectional areas, such as any non-circular cross-section including eyelet-type shape or another shape.
  • First plurality of hot flow paths 172 is shown in a cross-sectional representation so that hot subflow paths 172A-172F are more easily seen. First plurality of hot flow paths 172 has the same configuration as first plurality of cold flow paths 152 except that first plurality of hot flow paths 172 extends in second lateral direction 128B and provide flow paths for a different fluid (in this exemplary embodiment, the fluid is a hot fluid).
  • First plurality of hot flow paths 172 include hot subflow paths 172A-172F that allow hot fluid to flow in second lateral direction 128B while also allowing hot fluid to transition between adjacent subflow paths 172A-157F by flowing at least partially vertically through transition openings 186 between adjacent subflow paths 172A-172F. Each of hot subflow paths 172A-172F have a wave pattern with waves that extend in second lateral direction 128B based on a cosine curve (or sine curve depending on the starting point of the wave). However, hot subflow paths 172A-172F are offset from adjacent hot subflow paths 172A-172F by one-half wavelength in second lateral direction 128B.
  • For example, as shown in FIG. 2, hot subflow path 172A (a topmost subflow path), hot subflow path 172C, and hot subflow path 172E have the same configuration as one another with waves that propagate in second lateral direction 128B in phase (i.e., crests and troughs of the waves line up vertically). Hot subflow path 172B, hot subflow path 172D, and hot subflow path 172F (a bottommost subflow path) also have the same configuration as one another with waves that propagate in second lateral direction 128B in phase. However, hot subflow paths 172B, 172D, and 172F are offset from hot subflow paths 172A, 172C, and 172E one-half wavelength such that the crests of hot subflow paths 172A, 172C, and 172E interconnect with the troughs of hot subflow paths 172B, 172D, and 172F (and vice-versa) to form transition openings 186 through which hot fluid can flow into adjacent hot subflow paths 172A-172F. While hot subflow paths 172A-172F are shown as having the same amplitude and wavelength, other embodiments can include hot subflow paths 172A-172F that have differing amplitudes and wavelengths. Further, other pluralities of hot flow paths 174-184 can have different configurations such that those hot subflow paths (which are part of each plurality of hot flow paths 174-184) have differing amplitudes, wavelengths, and/or orientations.
  • Transition openings 186 that interconnect hot subflow paths 172A-172F can have as large or small cross-sectional areas as desired and, in other embodiments, heat exchanger 110 may not include transition openings 186 and instead hot subflow paths 172A-172F are discrete and fluidically isolated from one another.
  • Hot subflow paths 172A-172F are shown as having a substantially circular cross-sectional area due to walls 112 having a varying thickness to form the circular cross-sectional area. However, hot subflow paths 172A-172F can have other cross-sectional areas, such as any non-circular cross-section including eyelet-type shape or another shape.
  • As shown in FIG. 2, the wave pattern of cold subflow paths 152A-152F and hot subflow paths 172A-172F create a weaved cross-flow configuration in which each subflow path of cold fluid flow path 150 is adjacent multiple subflow paths of hot fluid flow path 170 (and vice-versa). This configuration provides for increased thermal energy transfer while minimizing the volume needed for heat exchanger 110 (i.e., increasing the thermal energy-to-volume ratio of heat exchanger 110). Additionally, the wave pattern and transition openings 166 and 186 between subflow paths limits the growth of boundary layers of the cold fluid and hot fluid through cold fluid flow path 150 and hot fluid flow path 170, respectively, thereby increasing the thermal energy transfer capabilities.
  • As with heat exchanger 10 in FIGS. 1A-1C, heat exchanger 110 can be constructed from multiple components such that walls 112 are constructed independently and then fastened together to form heat exchanger 110. Heat exchanger 110 can also be formed as one continuous and monolithic piece through additive manufacturing or other methods.
  • Heat exchanger 10/110 utilizes a weaved cross-flow configuration to provide increased primary surface area to improve the thermal energy transfer capabilities between a first fluid and a second fluid. The weaved configuration is constructed primarily from stacked sheets/walls 12-26/112 (primary surfaces) that include waves in first lateral direction 28A/128A and second lateral direction 28B/128B. Waves 12-26/112 can have a variety of configurations, including waves that are based on a sinusoidal curve. Walls 12-26/112 are primary surfaces that have improved thermal energy transfer capabilities. The waves of one wall 12-26/112 are offset from waves of adjacent walls 12-26/112 by one-half wavelength to form plurality of flow paths 30B-42B/152-164 and 172-184 between adjacent walls 12-26/112 through which the hot or cool fluid flows. Utilizing walls 12-26/112 with waves provides an increase in primary surface area of walls 12-26/112 which in turn increases the thermal energy transfer between fluids flowing adjacent those walls 12-26/112. The increase in surface area of walls 12-26/112 eliminates the need for fins (i.e., additional secondary surfaces), thereby improving efficiency of heat exchanger 10/110 by minimizing the distance thermal energy must transfer to maximize the energy transfer-to-volume ratio.
  • Additive manufacturing can be utilized to create the disclosed heat exchanger 10/110 so that all components of heat exchanger 10/110 are formed during one manufacturing process to form a continuous and monolithic structure. Further, additive manufacturing can easily and reliably form heat exchanger 10/110 with complex walls 12-26/112 or shapes and small tolerances. While the waves of walls 12-26/112 are based on sinusoidal curves in the disclosed embodiments, the waves can have a variety of configurations with alternate amplitudes, wavelengths, and other characteristics as required for optimal thermal energy transfer and to accommodate a designed flow of the first fluid and/or second fluid. Further, the waves of walls 12-26/112 can have other shapes, such as triangular waves with pointed peaks and troughs, rectangular waves with flat tops and bottoms, and/or other configurations.
  • Discussion of Possible Embodiments
  • The following are non-exclusive descriptions of possible embodiments of the present invention.
  • A heat exchanger that extends laterally in a first direction and a second direction and has a first wall, a second wall, and a third wall. The first wall is shaped in a wave pattern with waves that extend in both the first direction and the second direction. The second wall is adjacent to and in contact with the first wall with the second wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction. The waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength. The third wall is adjacent to and in contact with the second wall with the third wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction. The waves of the third wall are offset in the second direction from the second wall by one-half wavelength. The heat exchanger also includes a first plurality of flow paths extending in the second direction with the first plurality of flow paths each bounded by the first wall and the second wall and a second plurality of flow paths extending in the first direction with the second plurality of flow paths each bounded by the second wall and the third wall.
  • The heat exchanger of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations, and/or additional components:
    A fourth wall adjacent to and in contact with the third wall with the fourth wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction, the waves of the fourth wall being offset from the waves of the third wall in the first direction by one-half wavelength and a third plurality of flow paths extending in the second direction with the third plurality of flow paths each bounded by the third wall and the fourth wall.
  • The waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction, and the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  • Each flow path of the first plurality of flow paths and the second plurality of flow paths have a substantially circular cross-sectional area.
  • The first plurality of flow paths are laterally interconnected by first transition openings and the second plurality of flow paths are laterally interconnected by second transition openings such that flow through one flow path of the first plurality of flow paths can transition and flow through an adjacent flow path of the first plurality of flow paths and flow through one flow path of the second plurality of flow paths can transition and flow through an adjacent flow path of the second plurality of flow paths.
  • Each flow path of the first plurality of flow paths are fluidically isolated from one another and each flow path of the second plurality of flow paths are fluidically isolated from one another.
  • The first wall contacts and connects to the second wall along a plurality of contact lines extending in the second direction to form the fluidically isolated first plurality of flow paths extending in the second direction.
  • The second wall contacts and connects to the third wall along a plurality of contact lines extending in the first direction to form the fluidically isolated second plurality of flow paths extending in the first direction.
  • The first wall, second wall, and third wall are constructed by additive manufacturing so that the heat exchanger is one continuous and monolithic component.
  • The waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have an amplitude that is greater than an amplitude of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  • The amplitude of the waves in the first direction of the first wall, second wall, and third wall is at least 1.5 times greater than the amplitude of the waves in the second direction of the first wall, second wall, and third wall.
  • The waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have a wavelength that is greater than a wavelength of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  • The first wall, second wall, and third wall are constructed from a material having low thermal conductivity.
  • A gas turbine engine comprising the heat exchanger disclosed above.
  • A first fluid flows through the first plurality of flow paths and a second fluid flows through the second plurality of flow paths.
  • A method of forming a heat exchanger includes forming a first wall with waves that extend laterally in both a first direction and in a second direction. The method also includes forming a second wall adjacent to and in contact with the first wall with waves that are based on a sinusoidal curve and extend laterally in both the first direction and in the second direction. The waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength. The method also includes forming a third wall adjacent to and in contact with the second wall with waves that extend laterally in both the first direction and in the second direction. The waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength. The first wall and the second wall bound a first plurality of flow paths that extend in the second direction, and the second wall and the third wall bound a second plurality of flow paths that extend in the first direction. The waves of the first, second, and third walls can be based on a sinusoidal curve.
  • The method of the preceding paragraph can optionally include, additionally and/or alternatively, any one or more of the following features, configurations, steps, and/or additional components:
    Additively manufacturing the first wall, second wall, and third wall.
  • Forming a fourth wall adjacent to and in contact with the third wall with waves that extend laterally in both the first direction and in the second direction, the waves being offset in the first direction from the waves of the third wall by one-half wavelength, and wherein the third wall and fourth wall bound a third plurality of flow paths that extend in the second direction.
  • The waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction, and wherein the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  • A method of transferring thermal energy through the use of a heat exchanger includes flowing a first fluid through a first plurality of flow paths bounded by a first wall and a second wall. The first wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both a first direction and a second direction. The second wall is adjacent to and in contact with the first wall and having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction. The waves of the second wall are offset in the first direction from the waves of the first wall by one-half wavelength. The method also includes flowing a second fluid through a second plurality of flow paths bounded by the second wall and a third wall. The third wall is adjacent to and in contact with the second wall. The third wall has a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction. The waves of the third wall are offset in the second direction from the waves of the second wall by one-half wavelength.
  • While the invention has been described with reference to an exemplary embodiment(s), 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 invention as defined by the claims. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the scope of the invention. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims (15)

  1. A heat exchanger extending laterally in a first direction and a second direction, the heat exchanger comprising:
    a first wall (12) shaped in a wave pattern with waves that extend in both the first direction and the second direction;
    a second wall (14) adjacent to and in contact with the first wall with the second wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction, the waves of the second wall being offset in the first direction from the waves of the first wall by one-half wavelength;
    a third wall (16) adjacent to and in contact with the second wall with the third wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction, the waves of the third wall being offset in the second direction from the second wall by one-half wavelength;
    a first plurality of flow paths (30B) extending in the second direction with the first plurality of flow paths each bounded by the first wall and the second wall; and
    a second plurality of flow paths (32B) extending in the first direction with the second plurality of flow paths each bounded by the second wall and the third wall.
  2. The heat exchanger of claim 1, further comprising:
    a fourth wall (18) adjacent to and in contact with the third wall with the fourth wall being shaped in a wave pattern with waves that extend in both the first direction and the second direction, the waves of the fourth wall being offset from the waves of the third wall in the first direction by one-half wavelength; and
    a third plurality of flow paths (34B) extending in the second direction with the third plurality of flow paths each bounded by the third wall and the fourth wall.
  3. The heat exchanger of claim 1 or 2, wherein the waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction, and wherein the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  4. The heat exchanger of claim 1, 2 or 3, wherein each flow path of the first plurality of flow paths and the second plurality of flow paths have a substantially circular cross-sectional area.
  5. The heat exchanger of claim 4, wherein the first plurality of flow paths are laterally interconnected by first transition openings and the second plurality of flow paths are laterally interconnected by second transition openings such that flow through one flow path of the first plurality of flow paths can transition and flow through an adjacent flow path of the first plurality of flow paths and flow through one flow path of the second plurality of flow paths can transition and flow through an adjacent flow path of the second plurality of flow paths.
  6. The heat exchanger of any preceding claim, wherein each flow path of the first plurality of flow paths are fluidically isolated from one another and each flow path of the second plurality of flow paths are fluidically isolated from one another, and preferably wherein the first wall contacts and connects to the second wall along a plurality of contact lines extending in the second direction to form the fluidically isolated first plurality of flow paths extending in the second direction, and/or wherein the second wall contacts and connects to the third wall along a plurality of contact lines extending in the first direction to form the fluidically isolated second plurality of flow paths extending in the first direction.
  7. The heat exchanger of any preceding claim, wherein the first wall, second wall, and third wall are constructed by additive manufacturing so that the heat exchanger is one continuous and monolithic component.
  8. The heat exchanger of any preceding claim, wherein the waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have an amplitude that is greater than an amplitude of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  9. The heat exchanger of claim 8, wherein the amplitude of the waves in the first direction of the first wall, second wall, and third wall is at least 1.5 times greater than the amplitude of the waves in the second direction of the first wall, second wall, and third wall, and/or wherein the waves in the first direction of the first wall, the waves in the first direction of the second wall, and the waves in the first direction of the third wall have a wavelength that is greater than a wavelength of the waves in the second direction of the first wall, the waves in the second direction of the second wall, and the waves in the second direction of the third wall.
  10. A gas turbine engine comprising the heat exchanger of any preceding claim.
  11. A method of forming a heat exchanger, the method comprising:
    forming a first wall with waves that extend laterally in both a first direction and in a second direction;
    forming a second wall adjacent to and in contact with the first wall with waves that extend laterally in both the first direction and in the second direction, the waves of the second wall being offset in the first direction from the waves of the first wall by one-half wavelength;
    forming a third wall adjacent to and in contact with the second wall with waves that extend laterally in both the first direction and in the second direction, the waves of the third wall being offset in the second direction from the waves of the second wall by one-half wavelength,
    wherein the first wall and the second wall bound a first plurality of flow paths that extend in the second direction, and wherein the second wall and the third wall bound a second plurality of flow paths that extend in the first direction.
  12. The method of claim 11, further comprising:
    additively manufacturing the first wall, second wall, and third wall.
  13. The method of claim 11 or 12, further comprising:
    forming a fourth wall adjacent to and in contact with the third wall with waves that extend laterally in both the first direction and in the second direction, the waves being offset in the first direction from the waves of the third wall by one-half wavelength,
    wherein the third wall and fourth wall bound a third plurality of flow paths that extend in the second direction.
  14. The method of claim 11, 12 or 13, wherein the waves of the first wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction, and wherein the waves of the second wall are based on a sinusoidal curve in the first direction and a sinusoidal curve in the second direction.
  15. A method of transferring thermal energy through the use of a heat exchanger, the method comprising:
    flowing a first fluid through a first plurality of flow paths bounded by a first wall and a second wall, the first wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both a first direction and a second direction, the second wall being adjacent to and in contact with the first wall and having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction, the waves of the second wall being offset in the first direction from the waves of the first wall by one-half wavelength;
    flowing a second fluid through a second plurality of flow paths bounded by the second wall and a third wall, the third wall being adjacent to and in contact with the second wall, the third wall having a wave pattern with waves that are based on a sinusoidal curve and extend laterally in both the first direction and the second direction, the waves of the third wall being offset in the second direction from the waves of the second wall by one-half wavelength.
EP19207464.9A 2018-11-27 2019-11-06 Weaved cross-flow heat exchanger and method of forming a heat exchanger Pending EP3660434A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16/201,321 US20200166293A1 (en) 2018-11-27 2018-11-27 Weaved cross-flow heat exchanger and method of forming a heat exchanger

Publications (1)

Publication Number Publication Date
EP3660434A1 true EP3660434A1 (en) 2020-06-03

Family

ID=68470395

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19207464.9A Pending EP3660434A1 (en) 2018-11-27 2019-11-06 Weaved cross-flow heat exchanger and method of forming a heat exchanger

Country Status (2)

Country Link
US (1) US20200166293A1 (en)
EP (1) EP3660434A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4015956A1 (en) * 2020-12-18 2022-06-22 Hamilton Sundstrand Corporation Multi-scale heat exchanger core
GB2607136A (en) * 2020-12-16 2022-11-30 Meggitt Aerospace Ltd Cross-flow heat exchangers and methods of making the same

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7161354B2 (en) * 2018-09-21 2022-10-26 住友精密工業株式会社 Heat exchanger
FR3105387B1 (en) * 2019-12-20 2021-11-26 Liebherr Aerospace Toulouse Sas HEAT EXCHANGER WITH OPTIMIZED FLUID PASSAGES
US11802736B2 (en) 2020-07-29 2023-10-31 Hamilton Sundstrand Corporation Annular heat exchanger
CN112414199B (en) * 2020-11-24 2021-12-03 浙江银轮机械股份有限公司 Heat dissipation fin construction method and related device and heat dissipation fin
DE102021201532A1 (en) * 2021-02-17 2022-08-18 JustAirTech GmbH HEAT EXCHANGER, METHOD OF OPERATING A HEAT EXCHANGER, METHOD OF MANUFACTURE OF A HEAT EXCHANGER, GAS REFRIGERATION MACHINE WITH A HEAT EXCHANGER AS A RECUPERATOR, DEVICE FOR TREATMENT OF GAS AND AIR CONDITIONING DEVICE
US20220412658A1 (en) * 2021-06-23 2022-12-29 Hamilton Sundstrand Corporation Wavy adjacent passage heat exchanger core
EP4155654A1 (en) * 2021-09-24 2023-03-29 Hamilton Sundstrand Corporation Heat exchanger core design
US20230323813A1 (en) * 2022-04-08 2023-10-12 General Electric Company Heat exchanger with cooling architecture

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4919200A (en) * 1989-05-01 1990-04-24 Stanislas Glomski Heat exchanger wall assembly
EP2607831A1 (en) * 2011-12-19 2013-06-26 Rolls-Royce plc A heat exchanger
EP3193125A1 (en) * 2016-01-14 2017-07-19 Hamilton Sundstrand Corporation Heat exchanger channels

Family Cites Families (113)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1380003A (en) * 1971-07-23 1975-01-08 Thermo Electron Corp Jet impingement heat exchanger
US4116271A (en) * 1975-02-04 1978-09-26 Guido Amandus De Lepeleire Counter-current bumped plates heat exchanger
US4484451A (en) * 1978-09-05 1984-11-27 United Air Specialists, Inc. Two-stage gas condenser with feedback cooling
US4293033A (en) * 1979-06-29 1981-10-06 Linde Aktiengesellschaft Plate-type heat exchanger
DE3220774C2 (en) * 1982-06-02 1986-09-25 W. Schmidt GmbH & Co KG, 7518 Bretten Plate evaporator or condenser
JPS61262593A (en) * 1985-05-15 1986-11-20 Showa Alum Corp Heat exchanger
IL93319A (en) * 1990-02-08 1993-06-10 Pessach Seidel Heat exchanger assembly and panel therefor
US5228515A (en) * 1992-07-31 1993-07-20 Tran Hai H Modular, compact heat exchanger
GB0008897D0 (en) * 2000-04-12 2000-05-31 Cheiros Technology Ltd Improvements relating to heat transfer
CA2372399C (en) * 2002-02-19 2010-10-26 Long Manufacturing Ltd. Low profile finned heat exchanger
US6919504B2 (en) * 2002-12-19 2005-07-19 3M Innovative Properties Company Flexible heat sink
DE10335510A1 (en) * 2003-07-31 2005-03-10 Stockhausen Chem Fab Gmbh Coated catalyst carrier body
US7032654B2 (en) * 2003-08-19 2006-04-25 Flatplate, Inc. Plate heat exchanger with enhanced surface features
GB0324348D0 (en) * 2003-10-17 2003-11-19 Oxycom Bv Heat exchange laminate
KR20050032888A (en) * 2003-10-02 2005-04-08 엘에스전선 주식회사 Flat plate heat transfer device
US20070107875A1 (en) * 2003-11-27 2007-05-17 Young-Duck Lee Flat plate heat transfer device
KR100581115B1 (en) * 2003-12-16 2006-05-16 엘에스전선 주식회사 Flat plate heat transferring apparatus and Method for manufacturing the same
FR2865028B1 (en) * 2004-01-12 2006-12-29 Ziepack THERMAL EXCHANGER AND EXCHANGE MODULE RELATING THERETO
US20050150649A1 (en) * 2004-01-13 2005-07-14 Japan Matex Kabushiki Kaisha (Japan Corporation) Heat release sheet and heat sink
EP1713557A2 (en) * 2004-02-10 2006-10-25 The Texas A&M University System Vapor-compression evaporation system and method
US7140421B2 (en) * 2004-09-03 2006-11-28 Hul-Chun Hsu Wick structure of heat pipe
US20060090820A1 (en) * 2004-11-01 2006-05-04 Metglas, Inc. Iron-based brazing filler metals
CA2585772C (en) * 2004-11-03 2013-12-24 Velocys, Inc. Partial boiling in mini and micro-channels
US7618598B2 (en) * 2004-11-29 2009-11-17 Modine Manufacturing Company Catalytic reactor/heat exchanger
US7599626B2 (en) * 2004-12-23 2009-10-06 Waytronx, Inc. Communication systems incorporating control meshes
TWI276768B (en) * 2005-01-03 2007-03-21 Taiwan Textile Res Inst Heat exchange structure with at least three different airflow direction
US7254953B2 (en) * 2005-01-06 2007-08-14 Caterpillar Inc Thermoelectric heat exchange element
TWI259895B (en) * 2005-03-18 2006-08-11 Foxconn Tech Co Ltd Heat pipe
US20060250205A1 (en) * 2005-05-04 2006-11-09 Honeywell International Inc. Thermally conductive element for cooling an air gap inductor, air gap inductor including same and method of cooling an air gap inductor
DE202005009948U1 (en) * 2005-06-23 2006-11-16 Autokühler GmbH & Co. KG Heat exchange element and thus produced heat exchanger
GB2429054A (en) * 2005-07-29 2007-02-14 Howden Power Ltd A heating surface element
US20070029073A1 (en) * 2005-08-04 2007-02-08 Denso Corporation Production method of offset-shaped fins, fins, and method and apparatus for changing pitch of fins
JP2007113793A (en) * 2005-10-17 2007-05-10 Calsonic Kansei Corp Evaporator
US7357126B2 (en) * 2005-12-20 2008-04-15 Caterpillar Inc. Corrosive resistant heat exchanger
US20080099188A1 (en) * 2005-12-30 2008-05-01 Igor Victorovich Touzov Perforated heat pipes
US20070151703A1 (en) * 2005-12-30 2007-07-05 Touzov Igor V Grid and yarn membrane heat pipes
DE102006000885B3 (en) * 2006-01-04 2007-08-02 Daimlerchrysler Ag Method for producing a heat exchanger tube bundle for heat exchangers of electrochemical energy storage devices
US20070227707A1 (en) * 2006-03-31 2007-10-04 Machiroutu Sridhar V Method, apparatus and system for providing for optimized heat exchanger fin spacing
CN101351901B (en) * 2006-04-03 2012-06-20 株式会社渊上微 Heat pipe
US7896064B2 (en) * 2006-06-27 2011-03-01 Tranter, Inc. Plate-type heat exchanger
US7866372B2 (en) * 2006-12-20 2011-01-11 The Boeing Company Method of making a heat exchanger core component
US20090056912A1 (en) * 2007-08-29 2009-03-05 Tom Kerber Thermal device for heat exchange
TWI326760B (en) * 2007-08-31 2010-07-01 Chen Cheng-Tsun Heat exchanger
DE102007044461A1 (en) * 2007-09-11 2009-03-12 Daimler Ag Heat exchanger unit and electrochemical energy storage with a heat exchanger unit
US20090211977A1 (en) * 2008-02-27 2009-08-27 Oregon State University Through-plate microchannel transfer devices
US8230903B2 (en) * 2008-04-18 2012-07-31 International Business Machines Corporation Low profile heat sink for semiconductor devices
US20090277611A1 (en) * 2008-04-21 2009-11-12 Vasanth Vailoor Air-cooled radiator assembly for oil-filled electrical quipment
US8151617B2 (en) * 2008-05-23 2012-04-10 Dana Canada Corporation Turbulizers and method for forming same
SE533453C2 (en) * 2008-08-06 2010-10-05 Sven Melker Nilsson Duct
US8568495B2 (en) * 2008-09-05 2013-10-29 Samsung Sdi Co., Ltd. Evaporator and fuel reformer having the same
FR2938323B1 (en) * 2008-11-12 2010-12-24 Astrium Sas THERMAL REGULATION DEVICE WITH A NETWORK OF INTERCONNECTED CAPILLARY CALODUCES
JP4706754B2 (en) * 2008-12-24 2011-06-22 ソニー株式会社 Heat transport device and electronic equipment
EP2228615B1 (en) * 2009-03-12 2018-04-25 MAHLE Behr GmbH & Co. KG Plate heat exchanger, in particular for heat recovery from exhaust gases of a motor vehicle
TWM371233U (en) * 2009-04-16 2009-12-21 Asia Vital Components Co Ltd Inclined wave-shape plate and its heat exchanger
DE102009018247A1 (en) * 2009-04-21 2010-10-28 Linde Aktiengesellschaft Plate heat exchanger with profiles
CN102414533A (en) * 2009-04-28 2012-04-11 三菱电机株式会社 Heat exchange element
DE102009052045A1 (en) * 2009-11-05 2011-05-12 Rvt Process Equipment Gmbh Corrugated packing grid and ordered, composed of several packing lattice pack
US20110120934A1 (en) * 2009-11-24 2011-05-26 Air To Air Sweden Ab Method of producing multiple channels for use in a device for exchange of solutes between fluid flows
US9683789B2 (en) * 2009-11-24 2017-06-20 Air To Air Sweden Ab Method of producing multiple channels for use in a device for exchange of solutes or heat between fluid flows
US20110132570A1 (en) * 2009-12-08 2011-06-09 Wilmot George E Compound geometry heat exchanger fin
US20140318753A1 (en) * 2013-04-29 2014-10-30 Ford Global Technologies, Llc Heat exchanger
JP5733900B2 (en) * 2010-02-26 2015-06-10 三菱電機株式会社 Manufacturing method of plate heat exchanger and plate heat exchanger
US8522861B2 (en) * 2010-03-29 2013-09-03 Hamilton Sundstrand Space Systems International, Inc. Integral cold plate and structural member
US10852069B2 (en) * 2010-05-04 2020-12-01 Fractal Heatsink Technologies, LLC System and method for maintaining efficiency of a fractal heat sink
JP5545260B2 (en) * 2010-05-21 2014-07-09 株式会社デンソー Heat exchanger
PT2591303E (en) * 2010-07-08 2015-11-16 Swep Int Ab A plate heat exchanger
DE102012201710A1 (en) * 2011-02-14 2012-08-16 Denso Corporation heat exchangers
US9644899B2 (en) * 2011-06-01 2017-05-09 Arvos, Inc. Heating element undulation patterns
DE102011080782B4 (en) * 2011-08-10 2014-09-04 Eberspächer Exhaust Technology GmbH & Co. KG Latent heat storage and catalyst
KR101299072B1 (en) * 2011-11-29 2013-08-27 주식회사 코렌스 Wavy fin
JP6109473B2 (en) * 2011-11-30 2017-04-05 東京ラヂエーター製造株式会社 EGR cooler
US20130146532A1 (en) * 2011-12-09 2013-06-13 General Electric Company Feed spacer for spiral wound membrane element
US20130168042A1 (en) * 2012-01-04 2013-07-04 General Electric Company Heat exchanger having corrugated sheets
US9784505B2 (en) * 2012-05-15 2017-10-10 Lockheed Martin Corporation System, apparatus, and method for micro-capillary heat exchanger
CA2879447C (en) * 2012-07-19 2018-02-06 Asahi Kasei Fibers Corporation Multilayered structure comprising fine fiber cellulose layer
US9017539B2 (en) * 2012-08-22 2015-04-28 Infineon Technologies Ag Method for fabricating a heat sink, and a heat sink
EP2711163A1 (en) * 2012-09-21 2014-03-26 Hirschberg Engineering Three-dimensional body
US10337806B2 (en) * 2012-10-04 2019-07-02 Parker-Hannifin Corporation Fin plate, frame comprising at least one such plate and heat exchanger comprising said frame
US9377250B2 (en) * 2012-10-31 2016-06-28 The Boeing Company Cross-flow heat exchanger having graduated fin density
US10371467B2 (en) * 2012-12-05 2019-08-06 Hamilton Sundstrand Corporation Heat exchanger with variable thickness coating
US9243850B1 (en) * 2013-02-07 2016-01-26 Hy-Tek Manufacturing Company, Inc. Rotary high density heat exchanger
CN105144374A (en) * 2013-04-23 2015-12-09 亚历克西乌和特里德控股公司 Heat sink having a cooling structure with decreasing structure density
PL3047225T3 (en) * 2013-09-19 2019-04-30 Howden Uk Ltd Heat exchange element profile with enhanced cleanability features
JP5809759B2 (en) * 2013-10-15 2015-11-11 隆啓 阿賀田 Method for improving fluid flow characteristics, heat exchanger to which the improvement method is applied, distillation apparatus, deodorizing apparatus, and cut plate used in the improvement method
US10175006B2 (en) * 2013-11-25 2019-01-08 Arvos Ljungstrom Llc Heat transfer elements for a closed channel rotary regenerative air preheater
ES2673292T3 (en) * 2013-12-18 2018-06-21 Alfa Laval Corporate Ab Heat transfer plate and plate heat exchanger
TW201525398A (en) * 2013-12-25 2015-07-01 Hao Pai Wick structure having braided flat fiber and ultrathin heat pipe having the same
CN103791758B (en) * 2014-03-07 2016-07-20 丹佛斯微通道换热器(嘉兴)有限公司 For the heat exchanger plate of plate type heat exchanger and have the plate type heat exchanger of this heat exchanger plate
US9394825B2 (en) * 2014-04-07 2016-07-19 Hanon Systems Charge air cooler internal condensation separator
WO2016023393A1 (en) * 2014-08-12 2016-02-18 丹佛斯微通道换热器(嘉兴)有限公司 Heat exchange plate and plate-type heat exchanger
KR101675553B1 (en) * 2014-12-09 2016-11-11 서울시립대학교 산학협력단 A Wavy Fin and Flat Tube Heat Exchanger having the same
KR101706263B1 (en) * 2015-04-16 2017-02-15 서울시립대학교 산학협력단 Wavy fin, heat exchanger having the same, apparatus for manufacturing the same, method for manufacturing the same and computer recordable medium storing the method
CN106643263B (en) * 2015-07-29 2019-02-15 丹佛斯微通道换热器(嘉兴)有限公司 Fin component for heat exchanger and the heat exchanger with the fin component
US10160545B2 (en) * 2015-10-19 2018-12-25 Hamilton Sundstrand Corporation Ram air heat exchanger
US10422586B2 (en) * 2015-11-10 2019-09-24 Hamilton Sundstrand Corporation Heat exchanger
US20170146305A1 (en) * 2015-11-24 2017-05-25 Hamilton Sundstrand Corporation Header for heat exchanger
US11243030B2 (en) * 2016-01-13 2022-02-08 Hamilton Sundstrand Corporation Heat exchangers
US10113818B2 (en) * 2016-01-27 2018-10-30 Garrett Transportation I Inc. Bimetallic fin with themo-adjusting turbulation feature
CN107036480B (en) * 2016-02-04 2020-07-10 丹佛斯微通道换热器(嘉兴)有限公司 Heat exchange plate and plate heat exchanger using same
CN107036479B (en) * 2016-02-04 2020-05-12 丹佛斯微通道换热器(嘉兴)有限公司 Heat exchange plate and plate heat exchanger using same
JP6615316B2 (en) * 2016-03-16 2019-12-04 三菱電機株式会社 Finless type heat exchanger, outdoor unit of air conditioner equipped with the finless type heat exchanger, and indoor unit of air conditioner equipped with the finless type heat exchanger
CN105806109B (en) * 2016-03-24 2020-01-07 南京工业大学 Counter-flow finned plate heat exchanger for gas-gas heat exchange
JP6428701B2 (en) * 2016-04-06 2018-11-28 株式会社デンソー Thermoelectric generator
GB2552956A (en) * 2016-08-15 2018-02-21 Hs Marston Aerospace Ltd Heat exchanger device
US20190316847A9 (en) * 2016-11-28 2019-10-17 Carrier Corporation Plate heat exchanger with dual flow path
US10578367B2 (en) * 2016-11-28 2020-03-03 Carrier Corporation Plate heat exchanger with alternating symmetrical and asymmetrical plates
US10704841B2 (en) * 2017-01-03 2020-07-07 Titan Tensor LLC Monolithic bicontinuous labyrinth structures and methods for their manufacture
US10495000B2 (en) * 2017-03-20 2019-12-03 General Electric Company Contoured evaporative cooling medium
GB2565143B (en) * 2017-08-04 2021-08-04 Hieta Tech Limited Heat exchanger
US11090225B2 (en) * 2018-03-08 2021-08-17 Thaddeus Medical Systems, Inc. Protection device that promotes air flow for heat transfer
US10465992B2 (en) * 2018-03-16 2019-11-05 Hamilton Sundstrand Corporation Parting sheet in heat exchanger core
US10932395B2 (en) * 2018-06-04 2021-02-23 GM Global Technology Operations LLC Thermal management device for use on electronics in a transportation vehicle
US20200033070A1 (en) * 2018-07-25 2020-01-30 Andreas Vlahinos Minimal surface heat exchanger

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4919200A (en) * 1989-05-01 1990-04-24 Stanislas Glomski Heat exchanger wall assembly
EP2607831A1 (en) * 2011-12-19 2013-06-26 Rolls-Royce plc A heat exchanger
EP3193125A1 (en) * 2016-01-14 2017-07-19 Hamilton Sundstrand Corporation Heat exchanger channels

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2607136A (en) * 2020-12-16 2022-11-30 Meggitt Aerospace Ltd Cross-flow heat exchangers and methods of making the same
EP4015956A1 (en) * 2020-12-18 2022-06-22 Hamilton Sundstrand Corporation Multi-scale heat exchanger core
US20220205735A1 (en) * 2020-12-18 2022-06-30 Hamilton Sundstrand Corporation Multi-scale heat exchanger core
US11555659B2 (en) * 2020-12-18 2023-01-17 Hamilton Sundstrand Corporation Multi-scale heat exchanger core

Also Published As

Publication number Publication date
US20200166293A1 (en) 2020-05-28

Similar Documents

Publication Publication Date Title
EP3660434A1 (en) Weaved cross-flow heat exchanger and method of forming a heat exchanger
JP6496368B2 (en) Heat exchanger with foam fins
KR100990309B1 (en) Heat exchanger
US20060185835A1 (en) Heat exchange plate
US10677538B2 (en) Indirect heat exchanger
JP6163190B2 (en) Heat exchanger
EP3101376B1 (en) Heat exchanging board and board-type heat exchanger provided with heat exchanging board
JP5872859B2 (en) Heat exchanger
US4919200A (en) Heat exchanger wall assembly
JP4827905B2 (en) Plate type heat exchanger and air conditioner equipped with the same
US10578367B2 (en) Plate heat exchanger with alternating symmetrical and asymmetrical plates
US20150267966A1 (en) Adaptable heat exchanger and fabrication method thereof
CN101158561A (en) Plate heat exchanger composite corrugated plate bind
CN210374731U (en) Wave-shaped fluid channel heat exchange fin of plate heat exchanger
CN109945698B (en) Micro-channel heat exchanger structure design method and device for cooperatively enhancing heat exchange
KR101303234B1 (en) Heat exchanger for exhaust-heat recovery
CN108548437B (en) Bionic-based fishbone-type micro-staggered alveolar heat exchanger core and heat exchanger
JP2009192140A (en) Plate type heat exchanger
US20050150645A1 (en) Plate for heat exchange and heat exchange unit
US20120125580A1 (en) Embossed plate external oil cooler
CN112146484B (en) Plate heat exchanger
JP4369223B2 (en) Element for heat exchanger
GB2183811A (en) Rotary regenerative heat exchanger
US20210247143A1 (en) A plate of plate heat exchangers
CN107735639A (en) Plate type heat exchanger

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20201203

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR