US3542124A - Heat exchanger - Google Patents

Heat exchanger Download PDF

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Publication number
US3542124A
US3542124A US751288A US3542124DA US3542124A US 3542124 A US3542124 A US 3542124A US 751288 A US751288 A US 751288A US 3542124D A US3542124D A US 3542124DA US 3542124 A US3542124 A US 3542124A
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United States
Prior art keywords
fins
passageways
plates
heat exchanger
fluid
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Expired - Lifetime
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US751288A
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Joseph N Manfredo
David G Bridgnell
Soren K Andersen
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Garrett Corp
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Garrett Corp
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    • 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
    • F28F3/027Elements 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 with openings, e.g. louvered corrugated fins; Assemblies of corrugated strips
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00Heat exchange
    • Y10S165/355Heat exchange having separate flow passage for two distinct fluids
    • Y10S165/356Plural plates forming a stack providing flow passages therein
    • Y10S165/387Plural plates forming a stack providing flow passages therein including side-edge seal or edge spacer bar
    • Y10S165/391Plural plates forming a stack providing flow passages therein including side-edge seal or edge spacer bar including intermediate corrugated element

Definitions

  • ABSTRACT In a heat exchanger having passageways formed llli-cl between spaced parallel plates bounded in a stack with fins [50] Field of Search connecting adjacent plates, means are provided for relieving Patented Nov. 24, 1970 r 3,542,124
  • one fluid flows between two adjacent plates to give up heat to another fluid that flows on the opposite side ofthe'respective plates.
  • Finsare' provided between the plates to more readily extract the heat from one fluid and transfer it to the other.
  • the fins aredisposed parallel to the fluid flow, providing a path for heat flow without adding appreciable flow resistance.
  • the thickness of the fins is such as to. provide maximum flow area, maximum wetted surface, and maximum area for heat flow.
  • a relatively thin fin normally satisfies thisr'equirement.
  • a thin fin buckles or bends under relatively light compression loads such as may be encountered at the inlet end for the hot fluid.
  • the fins are subjected to repeated buckling whenever the system is started and stopped due to the thermal cycle formed by theheating and then cooling of the heat exchanger. Then, after a few thermal cycles, the fins become stress fatigued and break. When this happens to the fins within the high pressure passageways, the
  • an object of this invention is to provide added columnar support to the fins without decreasing the area of fluid flow.
  • Another object of this invention is to provide an improved lightweight heat exchanger.
  • the heat exchanger has a plurality of spaced parallel plates 11 having preferably a' rectangular shape. Between alternate spaces formed by the plates lland along opposite edges thereof are bonded edge" closure elements 1 2a and12b. T he edge closure elements 120 and 12b along one of the respective edges are shown, the opposite plate edges, not shown, have, similar edge closure elements bonded thereto to form a plurality of passageways 13a and 13b which are parallel to each other. Passageways Home located outside of passageways 13b and edge closure elements 12a are, for example, one-half as wide as edge closure elements 12b, making passagewaysflSa narrower than passageway 13b.
  • One method of preventing the fins from breaking is to increase the number of fins per inch; but obviously, theflow area for the fluid decreases in about the same relationship as the increase in the number of fins'and, in turn, the flow area decreases almost directly with increases-in buckling strength.
  • Another method is to make the fins thicker. Since the compression strength increases as the cube of the thickness and since the flow area decreases as fin thickness increases, the flow area decreases approximately as the cube root of' the buckling strength increases. in other words, an increase by a factor of two in the fin buckling strength decreases the flow area by approximately one-quarter.
  • This invention teaches another method which is unique and novel, i.e., the use of relatively thick bars in combination with the fins so that the flow area remains substantially constant as the buckling strength is increased. Then where the temperature gradient is less severe, the bars are discontinued and fins only are provided for efficient heat conduction between the fluids.
  • the fins in this embodiment have different configuration within the various passageways; Passageways' 13a have fins 21,
  • each of the passageways 13a and 13b communicates with an inlet manifold (notshown) and the other end communicates with an outletmanifold (not shown).
  • opposite ends of passageways l7 communicate respectively with inlet and outlet manifolds (not shown), in a manner well known in the art.
  • the plates 11 should be of minimum weight and are made as then as possible. l-lowever,'the fluid passing within one group of parallel passageways may be at a higher pressure than the fluid passing within the other group of parallel passageways. This pressure differential tends to bend the thin plates.
  • suitable fins are normally bonded to adjacent plates 11 and these fins are capable of safely withstanding' tensile stresses due to any pressure differential. Therefore, the fins help to maintain the plates 11 flat.
  • the two fluids in addition to having unequal pressures, have inherently unequal temperatures. Therefore, if the hot fluid enters the modate the width' of the respective passageways.
  • the passageways 17 have fins 23 at the inlet side thereof and extend a predetermined distance into the passageway.
  • Fins 23 are followed by fins-24 which preferably give more corrugations per unit length than fins 23.
  • the fins 23 are disposed at the inlet end of the higher pressure fluid, where the tempera- 'ture gradient isgreater so that means, in the form of the aforementioned bars 26, are placed longitudinally within passageways 17 to withstand any compressive force that may thickness, of the various plate elements are not shown to scale.
  • the bar thickness is chosento provide maximum strength and minimum loss to flow area within the passageways.
  • The, bars temperature gradient is less severe as the fluid passes through the heat exchanger.
  • the fins 23 preferably extend along the passageway the same distance as the-bars 26. With this arrangement the flow area through the passageways 17 can be made substantially optimum and uniform. Means, such as bars 26, are placed withinjpassageways 13a and I'Sbbut normally, since the pressure therein is lower than the other passageways, the heat exchanger will not fail if the fins 22 happen to break.
  • a heat exchanger comprising: a plurality of spaced parallel plates; a plurality of first edge closure elements arranged between alternately spaced parallel plates to define a plurality of 7 first passageways for receiving a first fluid;

Description

columnar stresses within the fins.
I Unlted States- Patent 1 1 3,542,124
[72] Inventors Joseph N. Mann-ado 5 R f n s cited UNITED STATES PATENTS m: $223,122 33:35: 2,997,280 8/1961 Keast 165/157X c'mom'h 3,016,921 1/1962 Tadewald 165/166X 2" A I No 751288 3,196,942 7/1965 Prentiss..... 165/166 E f A a 1968 3,262,496 7/1966 Bawabe..... 165/166 [45] Patemed s}; 1970 1,805,652 5/1931 Caracristi... 165/166 in 2,033,402 3/1936 Smith 165/166X [731 mg: 22?": n 3 079 994 3/1963 Kuehl 165/166 I n" on a I a comma creditor. 3,282,334 11/1966 Stahlheber 165/166 Primary Examiner-Robert A. O'Leary Assistant Examiner-Theophil W. Streule Attorney-John N. Hazelwood, Edward B. Johnson, Albert J. g 4 HEAT EXCHANGER Miller and Orville R. Seidner 1 Claim, 1 Drnwln'g Fig; [52] 11.8. (21..., .Q 165/166 ABSTRACT: In a heat exchanger having passageways formed llli-cl between spaced parallel plates bounded in a stack with fins [50] Field of Search connecting adjacent plates, means are provided for relieving Patented Nov. 24, 1970 r 3,542,124
INVENTORS. JOSEPH N. MANFREDO DAVID G- BRIDGNELL BY SOREN K. ANDERSEN ATTORN EY This invention-relates to a heat exchanger; constructed, in
particular, of a plurality of plates'disposed in a stack and spaced from each other'with fins bonded to two adjacent plates. a v
Within heat exchangers of the type above described, one fluid flows between two adjacent plates to give up heat to another fluid that flows on the opposite side ofthe'respective plates. Finsare' provided between the plates to more readily extract the heat from one fluid and transfer it to the other. To minimize friction, the fins aredisposed parallel to the fluid flow, providing a path for heat flow without adding appreciable flow resistance. In addition, the thickness of the fins is such as to. provide maximum flow area, maximum wetted surface, and maximum area for heat flow. A relatively thin fin normally satisfies thisr'equirement. However, a thin fin buckles or bends under relatively light compression loads such as may be encountered at the inlet end for the hot fluid. The fins are subjected to repeated buckling whenever the system is started and stopped due to the thermal cycle formed by theheating and then cooling of the heat exchanger. Then, after a few thermal cycles, the fins become stress fatigued and break. When this happens to the fins within the high pressure passageways, the
platesare subjected to repeated bending by the'higher pressure fluid whereby the plates become fatigued and break,
causing an intermixing of the coolant and fluid to be cooled.
Therefore, an object of this invention is to provide added columnar support to the fins without decreasing the area of fluid flow.
Another object of this invention is to provide an improved lightweight heat exchanger.
These and other objects, features and advantages will become more apparent from the following description of the invention and shown in the accompanying drawing wherein the sole figure schematically shows an enlarged pictorial view of the heat exchanger incorporating the invention.
Referring to'the drawing, the heat exchanger has a plurality of spaced parallel plates 11 having preferably a' rectangular shape. Between alternate spaces formed by the plates lland along opposite edges thereof are bonded edge" closure elements 1 2a and12b. T he edge closure elements 120 and 12b along one of the respective edges are shown, the opposite plate edges, not shown, have, similar edge closure elements bonded thereto to form a plurality of passageways 13a and 13b which are parallel to each other. Passageways Home located outside of passageways 13b and edge closure elements 12a are, for example, one-half as wide as edge closure elements 12b, making passagewaysflSa narrower than passageway 13b. This arrangement is preferredsince, as it will become apparent, the fluid in the outer passageways 13a can only absorb or give up heat on one side thereof instead of two sides like the fluid within passageways 13b. The remaining spaces between the plates have edge closure elements 16 bonded to the two other opposing edges of the plates 11. Only the edge closure elements 16 along one of the other edges are shown, but
similar edge closure elements are understood to be bonded to the opposite edgesto form parallel passageways 17. One end passageways 17 through the ends thereof shown in the drawir" words, all the plates'and fins experience thermal expansion but are restrained by the corner edges. This restraint imposes compression loading on the fins. When the temperature gradientis too large, the fins in some of the passageways have been observed tobend and buckle. The fins 23 fatigue when the fins are repeatedly buckled under this compression loadingdue to the cycle of thermal expansion and contraction. When the fins in a high pressure passageway crack or break, the plates 11 bend due to the pressure differential thereacross. Themafter more cycling of the heat exchanger, plates 11 fatigue and break causing the hot and cold fluids to intermix.
One method of preventing the fins from breaking is to increase the number of fins per inch; but obviously, theflow area for the fluid decreases in about the same relationship as the increase in the number of fins'and, in turn, the flow area decreases almost directly with increases-in buckling strength. Another method is to make the fins thicker. Since the compression strength increases as the cube of the thickness and since the flow area decreases as fin thickness increases, the flow area decreases approximately as the cube root of' the buckling strength increases. in other words, an increase by a factor of two in the fin buckling strength decreases the flow area by approximately one-quarter. This invention teaches another method which is unique and novel, i.e., the use of relatively thick bars in combination with the fins so that the flow area remains substantially constant as the buckling strength is increased. Then where the temperature gradient is less severe, the bars are discontinued and fins only are provided for efficient heat conduction between the fluids.
The fins in this embodiment have different configuration within the various passageways; Passageways' 13a have fins 21,
.be'encount'ered. For. clarity in the drawing, the relative 26 do not extend the full length of the passageway since the of each of the passageways 13a and 13b communicates with an inlet manifold (notshown) and the other end communicates with an outletmanifold (not shown). In addition, opposite ends of passageways l7 communicate respectively with inlet and outlet manifolds (not shown), in a manner well known in the art.
The plates 11 should be of minimum weight and are made as then as possible. l-lowever,'the fluid passing within one group of parallel passageways may be at a higher pressure than the fluid passing within the other group of parallel passageways. This pressure differential tends to bend the thin plates. As mentioned above, suitable fins are normally bonded to adjacent plates 11 and these fins are capable of safely withstanding' tensile stresses due to any pressure differential. Therefore, the fins help to maintain the plates 11 flat. However, the two fluids, in addition to having unequal pressures, have inherently unequal temperatures. Therefore, if the hot fluid enters the modate the width' of the respective passageways. The passageways 17 have fins 23 at the inlet side thereof and extend a predetermined distance into the passageway. Fins 23 are followed by fins-24 which preferably give more corrugations per unit length than fins 23. The fins 23 are disposed at the inlet end of the higher pressure fluid, where the tempera- 'ture gradient isgreater so that means, in the form of the aforementioned bars 26, are placed longitudinally within passageways 17 to withstand any compressive force that may thickness, of the various plate elements are not shown to scale.
The bar thickness is chosento provide maximum strength and minimum loss to flow area within the passageways. The, bars temperature gradient is less severe as the fluid passes through the heat exchanger. The fins 23 preferably extend along the passageway the same distance as the-bars 26. With this arrangement the flow area through the passageways 17 can be made substantially optimum and uniform. Means, such as bars 26, are placed withinjpassageways 13a and I'Sbbut normally, since the pressure therein is lower than the other passageways, the heat exchanger will not fail if the fins 22 happen to break. Various other modifications may be contemplated by those skilled in the art without departing from the spirit and scope of the invention as hereinafter defined by the following claim. We claim:
l. A heat exchanger comprising: a plurality of spaced parallel plates; a plurality of first edge closure elements arranged between alternately spaced parallel plates to define a plurality of 7 first passageways for receiving a first fluid;
a plurality of second edge closure elements arranged between the alternately spaced parallel plates not includa plurality of first corrugated fins disposed between adjacent parallel plates at the inlet ends of the first and second passageways, said first corrugated fins offset to provide lateral support alternately to the long sides of said bars; and
a plurality of second corrugated fms disposed throughout the remainder of said first and second passageways, said second offset corrugated fins having more corrugations per unit length than said first offset corrugated fins to provide substantially the same flow area as the flow area at the inlet ends of the first and second passageways having said first corrugated fins and said bars.
US751288A 1968-08-08 1968-08-08 Heat exchanger Expired - Lifetime US3542124A (en)

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Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3983932A (en) * 1974-05-10 1976-10-05 Nippondenso Co., Ltd. Heat exchanger
US4049051A (en) * 1974-07-22 1977-09-20 The Garrett Corporation Heat exchanger with variable thermal response core
US4139054A (en) * 1977-10-28 1979-02-13 Sea Solar Power Plate-fin heat exchanger
US4231420A (en) * 1978-11-20 1980-11-04 Sea Solar Power Heat exchanger with controls therefor
US4282927A (en) * 1979-04-02 1981-08-11 United Aircraft Products, Inc. Multi-pass heat exchanger circuit
US4282834A (en) * 1979-07-19 1981-08-11 Sea Solar Power Boiler structure embodying a plurality of heat exchange units
US4350201A (en) * 1981-01-12 1982-09-21 United Aircraft Products, Inc. Self fixturing heat exchanger
US4890670A (en) * 1984-06-28 1990-01-02 M.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft Cross-flow heat exchanger
DE3936800A1 (en) * 1989-11-04 1991-05-08 Funke Waerme Apparate Kg Plate-type heat-exchanger - has double plates in sections spaced apart held in packet by pressure plates
DE4337634A1 (en) * 1993-11-04 1995-05-11 Funke Waerme Apparate Kg Plate heat exchanger (interchanger)
WO1998022771A1 (en) * 1996-11-19 1998-05-28 Valeo Engine Cooling Ab Arrangement for flow reduction in plate oil cooler
US5845399A (en) * 1995-06-05 1998-12-08 Alliedsignal Inc. Composite plate pin or ribbon heat exchanger
US6203771B1 (en) * 1992-10-28 2001-03-20 Alliedsignal Inc. Catalytic converter with metal monolith having an integral catalyst
US6213158B1 (en) 1999-07-01 2001-04-10 Visteon Global Technologies, Inc. Flat turbulator for a tube and method of making same
US6263960B1 (en) 1997-11-28 2001-07-24 Denso Corporation Oil cooler with cooling water side fin and oil side fin
US6375905B1 (en) * 2000-02-11 2002-04-23 Engelhard Corporation Corrugated metal substrate and coated product for ozone conversion
US6415855B2 (en) * 2000-04-17 2002-07-09 Nordon Cryogenie Snc Corrugated fin with partial offset for a plate-type heat exchanger and corresponding plate-type heat exchanger
US6590770B1 (en) 2002-03-14 2003-07-08 Modine Manufacturing Company Serpentine, slit fin heat sink device
US6648062B2 (en) * 2000-07-31 2003-11-18 Honda Giken Kogyo Kabushiki Kaisha Heat sink-type cooling device
US20040031587A1 (en) * 2001-11-29 2004-02-19 Fong Wang Ching Heat-exchanging fin device fro enhancing heat exchange efficiency
US20040066623A1 (en) * 2002-10-07 2004-04-08 Cheng-Kuo Lu Structure of a heat dissipation device for computers
US20040099408A1 (en) * 2002-11-26 2004-05-27 Shabtay Yoram Leon Interconnected microchannel tube
US20040177668A1 (en) * 2003-02-06 2004-09-16 Sagasser Rob J. Insert for heat exchanger tube
WO2004085947A1 (en) * 2003-03-26 2004-10-07 Behr Industry Gmbh & Co. Kg Heat exchanger, in particular air/air cooler
US6830097B2 (en) 2002-09-27 2004-12-14 Modine Manufacturing Company Combination tower and serpentine fin heat sink device
US20050121181A1 (en) * 2002-01-17 2005-06-09 Claire Szulman Heat exchange fin and the production method thereof
US6951245B1 (en) * 2002-10-01 2005-10-04 L'Air Liquide, Société Anonyme à Directoire et Conseil de Surveillance pour l'Etude et l'Exploitation des Procédés Georges Claude Plate-type heat exchanger comprising a thick fin, and use of such a heat exchanger
US20090095456A1 (en) * 2007-10-04 2009-04-16 Ktm Kuhler Gmbh Plate heat exchanger
US20100045034A1 (en) * 2008-08-19 2010-02-25 Hinders Edward B Steam-Based Electric Power Plant Operated on Renewable Energy
US20100314088A1 (en) * 2009-06-11 2010-12-16 Agency For Defense Development Heat exchanger having micro-channels
US20130299144A1 (en) * 2012-05-10 2013-11-14 Hamilton Sundstrand Corporation Heat exchanger
WO2014037122A1 (en) * 2012-09-10 2014-03-13 Valeo Systemes Thermiques Heat exchanger insert
US20140116664A1 (en) * 2012-10-31 2014-05-01 The Boeing Company Cross-Flow Heat Exchanger Having Graduated Fin Density
US20160025425A1 (en) * 2014-07-25 2016-01-28 Hamilton Sundstrand Corporation Heat exchanger with slotted guard fin
US20160195342A1 (en) * 2015-01-07 2016-07-07 Hamilton Sundstrand Corporation Heat exchanger with fin wave control
US20160377350A1 (en) * 2015-06-29 2016-12-29 Honeywell International Inc. Optimized plate fin heat exchanger for improved compliance to improve thermal life
DE102015110974A1 (en) * 2015-07-07 2017-01-12 Halla Visteon Climate Control Corporation Exhaust gas heat exchanger with several heat exchanger channels
US10184732B2 (en) 2013-03-27 2019-01-22 Modine Manufacturing Company Air to air heat exchanger
US10782074B2 (en) 2017-10-20 2020-09-22 Api Heat Transfer, Inc. Heat exchanger with a cooling medium bar
US11193722B2 (en) * 2018-05-01 2021-12-07 Dana Canada Corporation Heat exchanger with multi-zone heat transfer surface
US11221186B2 (en) * 2019-07-18 2022-01-11 Hamilton Sundstrand Corporation Heat exchanger closure bar with shield
EP3943863A1 (en) * 2020-07-23 2022-01-26 Valeo Autosystemy SP. Z.O.O. A heat exchanger

Cited By (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3983932A (en) * 1974-05-10 1976-10-05 Nippondenso Co., Ltd. Heat exchanger
US4049051A (en) * 1974-07-22 1977-09-20 The Garrett Corporation Heat exchanger with variable thermal response core
US4139054A (en) * 1977-10-28 1979-02-13 Sea Solar Power Plate-fin heat exchanger
US4231420A (en) * 1978-11-20 1980-11-04 Sea Solar Power Heat exchanger with controls therefor
US4282927A (en) * 1979-04-02 1981-08-11 United Aircraft Products, Inc. Multi-pass heat exchanger circuit
US4282834A (en) * 1979-07-19 1981-08-11 Sea Solar Power Boiler structure embodying a plurality of heat exchange units
US4350201A (en) * 1981-01-12 1982-09-21 United Aircraft Products, Inc. Self fixturing heat exchanger
US4890670A (en) * 1984-06-28 1990-01-02 M.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft Cross-flow heat exchanger
DE3936800A1 (en) * 1989-11-04 1991-05-08 Funke Waerme Apparate Kg Plate-type heat-exchanger - has double plates in sections spaced apart held in packet by pressure plates
US6203771B1 (en) * 1992-10-28 2001-03-20 Alliedsignal Inc. Catalytic converter with metal monolith having an integral catalyst
DE4337634A1 (en) * 1993-11-04 1995-05-11 Funke Waerme Apparate Kg Plate heat exchanger (interchanger)
US5845399A (en) * 1995-06-05 1998-12-08 Alliedsignal Inc. Composite plate pin or ribbon heat exchanger
US6216775B1 (en) 1996-11-19 2001-04-17 Valeo Engine Cooling Ab Arrangement for flow reduction in plate oil cooler
WO1998022771A1 (en) * 1996-11-19 1998-05-28 Valeo Engine Cooling Ab Arrangement for flow reduction in plate oil cooler
US6263960B1 (en) 1997-11-28 2001-07-24 Denso Corporation Oil cooler with cooling water side fin and oil side fin
US6453711B2 (en) 1999-07-01 2002-09-24 Visteon Global Technologies, Inc. Flat turbulator for a tube and method of making same
US6213158B1 (en) 1999-07-01 2001-04-10 Visteon Global Technologies, Inc. Flat turbulator for a tube and method of making same
US6375905B1 (en) * 2000-02-11 2002-04-23 Engelhard Corporation Corrugated metal substrate and coated product for ozone conversion
US6415855B2 (en) * 2000-04-17 2002-07-09 Nordon Cryogenie Snc Corrugated fin with partial offset for a plate-type heat exchanger and corresponding plate-type heat exchanger
US6648062B2 (en) * 2000-07-31 2003-11-18 Honda Giken Kogyo Kabushiki Kaisha Heat sink-type cooling device
US20040031587A1 (en) * 2001-11-29 2004-02-19 Fong Wang Ching Heat-exchanging fin device fro enhancing heat exchange efficiency
US7445040B2 (en) * 2002-01-17 2008-11-04 L'air Liquide, Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude Heat exchange fin and the production method thereof
US20050121181A1 (en) * 2002-01-17 2005-06-09 Claire Szulman Heat exchange fin and the production method thereof
US6590770B1 (en) 2002-03-14 2003-07-08 Modine Manufacturing Company Serpentine, slit fin heat sink device
US6830097B2 (en) 2002-09-27 2004-12-14 Modine Manufacturing Company Combination tower and serpentine fin heat sink device
US6951245B1 (en) * 2002-10-01 2005-10-04 L'Air Liquide, Société Anonyme à Directoire et Conseil de Surveillance pour l'Etude et l'Exploitation des Procédés Georges Claude Plate-type heat exchanger comprising a thick fin, and use of such a heat exchanger
US20040066623A1 (en) * 2002-10-07 2004-04-08 Cheng-Kuo Lu Structure of a heat dissipation device for computers
US20040099408A1 (en) * 2002-11-26 2004-05-27 Shabtay Yoram Leon Interconnected microchannel tube
US20050241816A1 (en) * 2002-11-26 2005-11-03 Shabtay Yoram L Interconnected microchannel tube
US7255159B2 (en) * 2003-02-06 2007-08-14 Modine Manufacturing Company Insert for heat exchanger tube
US20040177668A1 (en) * 2003-02-06 2004-09-16 Sagasser Rob J. Insert for heat exchanger tube
CN1764816B (en) * 2003-03-26 2010-09-29 贝洱工业技术公司 Heat exchanger, in particular air/air cooler
WO2004085947A1 (en) * 2003-03-26 2004-10-07 Behr Industry Gmbh & Co. Kg Heat exchanger, in particular air/air cooler
US7628199B2 (en) 2003-03-26 2009-12-08 Behr Industrietechnik Gmbh & Co. Heat exchanger, in particular air/air cooler
US20060231240A1 (en) * 2003-03-26 2006-10-19 Behr Industrietechnik Gmbh & Co. Heat exchanger, in particular air/air cooler
US20090095456A1 (en) * 2007-10-04 2009-04-16 Ktm Kuhler Gmbh Plate heat exchanger
US8418752B2 (en) * 2007-10-04 2013-04-16 Mahle International Gmbh Plate heat exchanger having a turbulence generator
US20100043433A1 (en) * 2008-08-19 2010-02-25 Kelly Patrick J Heat Balancer for Steam-Based Generating Systems
US8169101B2 (en) 2008-08-19 2012-05-01 Canyon West Energy, Llc Renewable energy electric generating system
US8256219B2 (en) 2008-08-19 2012-09-04 Canyon West Energy, Llc Methods for enhancing efficiency of steam-based generating systems
US8281590B2 (en) 2008-08-19 2012-10-09 Canyon West Energy, Llc Steam-based electric power plant operated on renewable energy
US20100045034A1 (en) * 2008-08-19 2010-02-25 Hinders Edward B Steam-Based Electric Power Plant Operated on Renewable Energy
US20100314088A1 (en) * 2009-06-11 2010-12-16 Agency For Defense Development Heat exchanger having micro-channels
CN103557728A (en) * 2012-05-10 2014-02-05 哈米尔顿森德斯特兰德公司 Improved heat exchanger
US9448010B2 (en) * 2012-05-10 2016-09-20 Hamilton Sundstrand Corporation Heat exchanger
US20130299144A1 (en) * 2012-05-10 2013-11-14 Hamilton Sundstrand Corporation Heat exchanger
WO2014037122A1 (en) * 2012-09-10 2014-03-13 Valeo Systemes Thermiques Heat exchanger insert
FR2995397A1 (en) * 2012-09-10 2014-03-14 Valeo Systemes Thermiques INTERCALAR OF HEAT EXCHANGER.
US20140116664A1 (en) * 2012-10-31 2014-05-01 The Boeing Company Cross-Flow Heat Exchanger Having Graduated Fin Density
US9377250B2 (en) * 2012-10-31 2016-06-28 The Boeing Company Cross-flow heat exchanger having graduated fin density
US10184732B2 (en) 2013-03-27 2019-01-22 Modine Manufacturing Company Air to air heat exchanger
US20160025425A1 (en) * 2014-07-25 2016-01-28 Hamilton Sundstrand Corporation Heat exchanger with slotted guard fin
US20160195342A1 (en) * 2015-01-07 2016-07-07 Hamilton Sundstrand Corporation Heat exchanger with fin wave control
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DE102015110974A1 (en) * 2015-07-07 2017-01-12 Halla Visteon Climate Control Corporation Exhaust gas heat exchanger with several heat exchanger channels
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US11193722B2 (en) * 2018-05-01 2021-12-07 Dana Canada Corporation Heat exchanger with multi-zone heat transfer surface
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