WO2001081849A1 - Integral fin passage heat exchanger - Google Patents

Integral fin passage heat exchanger Download PDF

Info

Publication number
WO2001081849A1
WO2001081849A1 PCT/US2001/012965 US0112965W WO0181849A1 WO 2001081849 A1 WO2001081849 A1 WO 2001081849A1 US 0112965 W US0112965 W US 0112965W WO 0181849 A1 WO0181849 A1 WO 0181849A1
Authority
WO
WIPO (PCT)
Prior art keywords
fin
heat exchanger
integral
integral fin
passages
Prior art date
Application number
PCT/US2001/012965
Other languages
French (fr)
Inventor
Stephen L. White
Brian S. Naumann
Original Assignee
Honeywell International Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell International Inc. filed Critical Honeywell International Inc.
Publication of WO2001081849A1 publication Critical patent/WO2001081849A1/en

Links

Classifications

    • 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
    • F28D9/0081Heat-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 a single plate-like element ; the conduits for one heat-exchange medium being integrated in one single plate-like element
    • 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
    • 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
    • F28F2250/108Particular pattern of flow of the heat exchange media with combined cross flow and parallel flow

Definitions

  • Reducing the number of parts would simplify the construction of the metal core and reduce the cost of construction. Reducing the number of parts would also reduce the number of brazed joints that could possibly leak
  • FIG. 4 is a flowchart of a method of constructing a heat exchanger according to the present invention.
  • the plates 16 and the extended surfaces 18 are integrally formed. That is, they form a unitary structure.
  • the integral fin passages 12 may be formed by extrusion. Any extrudable material having good heat transfer characteristics may be used for the integral fin passages 12. Such material includes, without limitation, copper and aluminum. Using integral fin passages 12 reduces the parts count of the heat exchanger core 10.
  • Individual closure bars 26 may be located at edges of, and brazed between, plates 16 of adjacent integral fin passages 12. Each individual closure bar 26 may be made of a metal core having a braze cladding. The closure bars 26 provide closure for the second fluid passageways 22 and they provide precise spacing between the integral fin passages 12. Closure for the second fluid passageways 22 may be provided by four straight or two L- shaped closure bars. The topmost closure bars 26 have been omitted for clarity.
  • the heat exchanger core 10 may provide any type of flow path.
  • Types of countercurrent and co-current paths include, without limitation, straight flow paths, 'Z'-flow paths and 'U'-flow paths.
  • a simple cross flow heat exchanger having an entirely straight rectangular fin geometry may be formed by stacking integral fin passages in a z-direction. Integral fin passages for the hot fluid may extend in the x- direction and integral fin passages for the cold fluid may extend along the y- direction.
  • another heat exchanger core 110 includes first and second header plates 126 instead of the individual closure bars.
  • the header plates 126 serve the same function as the individual closure bars: providing closure for the fluid flowing between each of the integral fin passages 112 as well as providing precise spacing between the integral fin passages 112.
  • the header plates 126 may be machined or formed from sheet metal.
  • a heat exchanger core 110 having two header plates 126 has a lower parts count than a core 10 having multiple closure bars 26.
  • the integral fin passages 112 may be brazed or welded to the header plates 126.
  • integral fin passages are not limited to the design shown in the drawings.
  • an alternative integral fin passageway could include a flattened tube and a fin within the flattened tube.
  • Such an alternative integral fin passage would have plates and closure bars that are integrally formed.

Abstract

A plate-fin heat exchanger (10) includes a plurality of integral fin passages (12) and a plurality of fins (14). Each fin (14) is located between and bonded to outer surfaces of adjacent integral fin passages (12). Each integral fin passage (12) has integrally formed plates (16) and extended surfaces (18). The integral fin passages (12) may be formed by extrusion.

Description

INTEGRAL FIN PASSAGE HEAT EXCHANGER
BACKGROUND OF THE INVENTION
The present invention relates generally to heat exchangers More specifically, the present invention relates to a plate-fin heat exchanger
A typical plate-fin heat exchanger includes a core and manifolds The core includes a plurality of plates, a plurality of fins located between and bonded to the plates, and a plurality of closure bars. The plates and fins define hot side and cold side passageways. The closure bars provide closure of the fins and precise spacing between the plates. During operation of the heat exchanger, a hot fluid flows through the hot side passageways and a cold fluid flows through the cold side passageways. Heat is transferred from the hot fluid to the cold fluid. The manifolds direct the hot fluid and cold fluid to and from the hot side and cold side passageways.
A large number of parts are assembled during construction of the metal core, and great care is taken to assemble the parts. A large number of welds and braze joints are made during the construction of the metal core
Reducing the number of parts would simplify the construction of the metal core and reduce the cost of construction. Reducing the number of parts would also reduce the number of brazed joints that could possibly leak
Therefore, it is desirable to reduce the parts count of plate-fin heat exchangers.
SUMMARY OF THE INVENTION The core of a plate-fin heat exchanger according to the present invention has a reduced parts count. The heat exchanger core comprises first and second integral fin passages, each integral fin passage having integrally formed plates and extended surfaces; and a fin located between and bonded to outer surfaces of the first and second integral fin passages Reducing the parts count simplifies the construction of the core and reduces the number of brazed joints that could possibly leak. BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is an exploded view of a heat exchanger core according to the present invention;
Figures 2a and 2b are illustrations of two different fin geometries;
Figure 3 is an illustration of a header plate and integral fin passages of another heat exchanger core according to the present invention;
Figure 4 is a flowchart of a method of constructing a heat exchanger according to the present invention; and
Figures 5a and 5b are illustrations of different profiles of passageways within the integral fin passages.
DETAILED DESCRIPTION OF THE INVENTION Reference is made to Figure 1 , which illustrates a heat exchanger core 10. The core 10 includes a plurality of integral fin passages 12 and a plurality of fins 14. Each integral fin passage 12 includes a pair of plates 16 and a plurality of extended surfaces 18 between the plates 16. The plates 16 and the extended surfaces 18 define straight fluid passageways 20. The two extended surfaces 18a and 18b at the edges of the plates 16 also function as closure bars.
The plates 16 and the extended surfaces 18 are integrally formed. That is, they form a unitary structure. For instance, the integral fin passages 12 may be formed by extrusion. Any extrudable material having good heat transfer characteristics may be used for the integral fin passages 12. Such material includes, without limitation, copper and aluminum. Using integral fin passages 12 reduces the parts count of the heat exchanger core 10.
Each fin 14 is located between and bonded to outer surfaces of adjacent integral fin passages 12. Each fin 14 may have a metal core 14a that is clad with a braze material 14b (a portion of the braze material has been removed to show the metal core 14a). The braze material 14b enhances the bond between the fins 14 and the extruded passages 12.
The plates 16 and the fins 14 define second fluid passageways 22. The second fluid passageways 22 may provide any type of flow path. For example, the second fluid passageways 22 may be straight and arranged to provide a cross-flow relative to the first fluid passageways 20. The core 10 may instead include inlet and outlet turning fins 24 for providing co-current (i.e., same direction) or countercurrent (i.e., opposite direction) flow relative to the first fluid passageways 20. The inlet and outlet turning fins 24 may be oriented to provide generally either a Z-flow path or a U-flow path. A Z-flow path begins at one end of the heat exchanger core 10 and ends at an opposite side and opposite corner. A U-flow path begins and ends on the same side, but opposite corners of the core 10. The inlet and outlet turning fins 24 may be oriented at various angles relative to the first fluid passageway 20. Figure 1 happens to show fins 14 providing a Z-flow path, with the turning fins 24 being oriented at a 90 degree angle relative to the first fluid passageway 20.
The integral fin passages 12 and fins 14 may be stacked in an alternating sequence (in the z-direction). Thus, each fin 14 is located between a pair of adjacent integral fin passages 12.
Individual closure bars 26 may be located at edges of, and brazed between, plates 16 of adjacent integral fin passages 12. Each individual closure bar 26 may be made of a metal core having a braze cladding. The closure bars 26 provide closure for the second fluid passageways 22 and they provide precise spacing between the integral fin passages 12. Closure for the second fluid passageways 22 may be provided by four straight or two L- shaped closure bars. The topmost closure bars 26 have been omitted for clarity.
Instead of using individual closure bars 26, closure bars for the sides of the fins 14 (in the direction of the first fluid passageways 20) may be formed integrally with the plates 16 of the integral fin passage 12. An extruded closure bar of one integral passage would be brazed or welded to an adjacent integral fin passage 12. Forming the fin closure bars as part of the integral fin passages 12 further reduces the parts count of the heat exchanger core 10.
The integral fin passages 12 may provide the hot side or cold side passageways. During operation of the heat exchanger shown in Figure 1 , a first fluid enters the first end of the integral fin passages 12, passes straight though the core 10 (in a y-direction) and exits a second end of the integral passages 12. A second fluid enters one corner of the core 10 (in an x- direction), is turned to flow parallel to the first fluid (in the y-direction), and is turned again to flow out of the opposite corner of the core 10 (in the x- direction). Heat is transferred from the hot fluid to the cold fluid. Manifolds (not shown) direct the hot fluid and cold fluid to and from the hot side and cold side passageways.
The fins 14 may have any typical heat transfer fin geometry. For example, the fin geometry may be plain rectangular (Figure 1), rectangular offset (Figure 2a) or wavy (Figure 2b). Other types of fin geometries include, without limitation, perforated geometry, plain triangular geometry and louvered geometry.
The heat exchanger core 10 may provide any type of flow path. Types of countercurrent and co-current paths include, without limitation, straight flow paths, 'Z'-flow paths and 'U'-flow paths.
A simple cross flow heat exchanger having an entirely straight rectangular fin geometry may be formed by stacking integral fin passages in a z-direction. Integral fin passages for the hot fluid may extend in the x- direction and integral fin passages for the cold fluid may extend along the y- direction.
Referring now to Figure 3, another heat exchanger core 110 includes first and second header plates 126 instead of the individual closure bars. The header plates 126 serve the same function as the individual closure bars: providing closure for the fluid flowing between each of the integral fin passages 112 as well as providing precise spacing between the integral fin passages 112. The header plates 126 may be machined or formed from sheet metal. A heat exchanger core 110 having two header plates 126 has a lower parts count than a core 10 having multiple closure bars 26. The integral fin passages 112 may be brazed or welded to the header plates 126.
Reference is now made to Figure 4. A method of fabricating a heat exchanger core includes the following steps. A plurality of integral fin passages are provided, with each integral fin passage having been extruded to form plates and extended surfaces (block 202). Fins and closure structures (e.g., closure bars, header plates) are assembled with the integral fin passages (block 204). The fins and closure structures are brazed or otherwise bonded to the integral fin passages (block 206). Thus, the integral fin passages, the fins and the closure structures are brazed together at the same time. After the core has been brazed, manifolds are welded or otherwise mounted to the closure bars of the heat exchanger core (block 208). The manifolds may also be clad with a braze material.
The integral fin passages are not limited to passageways having rectangular profiles. The passageways may have round or other profiles. See, for example, Figures 5a and 5b.
The integral fin passages are not limited to the design shown in the drawings. For instance, an alternative integral fin passageway could include a flattened tube and a fin within the flattened tube. Such an alternative integral fin passage would have plates and closure bars that are integrally formed.
The present invention is not limited to the specific embodiments described above. Instead, the present invention is construed according to the claims that follow.

Claims

WHAT IS CLAIMED IS:
1. A heat exchanger (10) comprising: first and second integral fin passages (12), each integral fin passage having integrally formed plates (16) and extended surfaces (18); and a fin (14) located between and bonded to outer surfaces of the first and second integral fin passages.
2. The heat exchanger of claim 1 , wherein extended surfaces (18a, 18b) at edges of the plates provide closure bars for the integral fin passages.
3. The heat exchanger of claim 2, wherein at least one integral fin passage further includes a closure bar (26) for the fin.
4. The heat exchanger of claim 2, further comprising closure bars (26) for the fin, each closure bar being located between and bonded to the outer surfaces of the first and second integral fin passages.
5. The heat exchanger of claim 1 , further comprising first and second header plates (126), first ends of the integral fin passages (112) fitting into slots in the first header plate, second ends of the integral fin passages fitting into slots in the second header plate, the header plates providing closure for the fin.
6. The heat exchanger of claim 1 , wherein each integral fin passage (12) provides a plurality of straight fluid flow passageways (20).
PCT/US2001/012965 2000-04-25 2001-04-23 Integral fin passage heat exchanger WO2001081849A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/557,347 2000-04-25
US09/557,347 US20020153129A1 (en) 2000-04-25 2000-04-25 Integral fin passage heat exchanger

Publications (1)

Publication Number Publication Date
WO2001081849A1 true WO2001081849A1 (en) 2001-11-01

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Family Applications (1)

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US (1) US20020153129A1 (en)
WO (1) WO2001081849A1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE1018518A3 (en) * 2009-04-06 2011-02-01 Atlas Copco Airpower Nv IMPROVED HEAT EXCHANGER.
WO2011009080A3 (en) * 2009-07-17 2012-03-15 Lockheed Martin Corporation Heat exchanger and method for making
EP2835612A1 (en) * 2013-08-09 2015-02-11 Hamilton Sundstrand Corporation Reduced thermal expansion closure bars for a heat exchanger
US9388798B2 (en) 2010-10-01 2016-07-12 Lockheed Martin Corporation Modular heat-exchange apparatus
EP2618094A3 (en) * 2012-01-23 2016-08-24 Honeywell International Inc. Porous blocker bar for plate-fin heat exchanger
US9541331B2 (en) 2009-07-16 2017-01-10 Lockheed Martin Corporation Helical tube bundle arrangements for heat exchangers
US9670911B2 (en) 2010-10-01 2017-06-06 Lockheed Martin Corporation Manifolding arrangement for a modular heat-exchange apparatus
US9777971B2 (en) 2009-10-06 2017-10-03 Lockheed Martin Corporation Modular heat exchanger
EP3553448A1 (en) * 2018-04-05 2019-10-16 United Technologies Corporation Secondarily applied cold side features for cast heat exchanger

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FR2824895B1 (en) * 2001-05-18 2005-12-16 Air Liquide CORRELATED WIND THRUST FOR PLATE HEAT EXCHANGER, AND PLATE EXCHANGER WITH THESE FINS
DE10304077A1 (en) 2003-01-31 2004-08-12 Heinz Schilling Kg Air / water heat exchanger with partial water paths
DE102006005362A1 (en) * 2006-02-07 2007-08-09 Modine Manufacturing Co., Racine Exhaust gas heat exchanger in an exhaust gas recirculation arrangement
US8915292B2 (en) 2006-02-07 2014-12-23 Modine Manufacturing Company Exhaust gas heat exchanger and method of operating the same
US8079508B2 (en) * 2008-05-30 2011-12-20 Foust Harry D Spaced plate heat exchanger
DE102016122455A1 (en) * 2015-11-27 2017-06-01 Hanon Systems Heat exchanger for exhaust gas cooling in motor vehicles and method for producing the heat exchanger
EP3465049B1 (en) * 2016-06-03 2021-04-07 FlexEnergy Energy Systems, Inc. Counter-flow heat exchanger
KR20200012850A (en) * 2017-05-30 2020-02-05 쉘 인터내셔날 리써취 마트샤피지 비.브이. How to use an indirect heat exchanger and equipment for treating liquefied natural gas comprising such a heat exchanger
US20230392880A1 (en) * 2022-06-03 2023-12-07 Raytheon Technologies Corporation Conformal heat exchanger

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US4738311A (en) * 1985-10-25 1988-04-19 Ingo Bleckman Heat exchanger
JPH0539992A (en) * 1991-08-02 1993-02-19 Showa Alum Corp Heat exchanger
DE19519511A1 (en) * 1994-05-31 1995-12-07 Tjiok Mouw Ching Heat exchanger using hollow plate

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US4276927A (en) * 1979-06-04 1981-07-07 The Trane Company Plate type heat exchanger
US4738311A (en) * 1985-10-25 1988-04-19 Ingo Bleckman Heat exchanger
JPH0539992A (en) * 1991-08-02 1993-02-19 Showa Alum Corp Heat exchanger
DE19519511A1 (en) * 1994-05-31 1995-12-07 Tjiok Mouw Ching Heat exchanger using hollow plate

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WO2010115246A3 (en) * 2009-04-06 2011-03-03 Atlas Copco Airpower Improved heat exchanger
US9574828B2 (en) 2009-04-06 2017-02-21 Atlas Copco Airpower Naamloze Vennootschap Heat exchanger
CN102483309A (en) * 2009-04-06 2012-05-30 阿特拉斯·科普柯空气动力股份有限公司 Improved heat exchanger
BE1018518A3 (en) * 2009-04-06 2011-02-01 Atlas Copco Airpower Nv IMPROVED HEAT EXCHANGER.
US9541331B2 (en) 2009-07-16 2017-01-10 Lockheed Martin Corporation Helical tube bundle arrangements for heat exchangers
CN102812320A (en) * 2009-07-17 2012-12-05 洛克希德马丁公司 Heat Exchanger And Method For Making
AU2010273997B2 (en) * 2009-07-17 2014-04-17 Lockheed Martin Corporation Heat exchanger and method for making
JP2012533723A (en) * 2009-07-17 2012-12-27 ロッキード マーティン コーポレーション Heat exchanger and manufacturing method thereof
WO2011009080A3 (en) * 2009-07-17 2012-03-15 Lockheed Martin Corporation Heat exchanger and method for making
US10209015B2 (en) 2009-07-17 2019-02-19 Lockheed Martin Corporation Heat exchanger and method for making
US9777971B2 (en) 2009-10-06 2017-10-03 Lockheed Martin Corporation Modular heat exchanger
US9388798B2 (en) 2010-10-01 2016-07-12 Lockheed Martin Corporation Modular heat-exchange apparatus
US9670911B2 (en) 2010-10-01 2017-06-06 Lockheed Martin Corporation Manifolding arrangement for a modular heat-exchange apparatus
EP2618094A3 (en) * 2012-01-23 2016-08-24 Honeywell International Inc. Porous blocker bar for plate-fin heat exchanger
EP2835612A1 (en) * 2013-08-09 2015-02-11 Hamilton Sundstrand Corporation Reduced thermal expansion closure bars for a heat exchanger
JP2015036617A (en) * 2013-08-09 2015-02-23 ハミルトン・サンドストランド・コーポレイションHamilton Sundstrand Corporation Reduced thermal expansion closure bar for heat exchanger
US9777970B2 (en) 2013-08-09 2017-10-03 Hamilton Sundstrand Coporation Reduced thermal expansion closure bars for a heat exchanger
EP3553448A1 (en) * 2018-04-05 2019-10-16 United Technologies Corporation Secondarily applied cold side features for cast heat exchanger

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