US3542124A - Heat exchanger - Google Patents
Heat exchanger Download PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- fins
- passageways
- plates
- heat exchanger
- fluid
- 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.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/02—Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
- F28F3/025—Elements 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
- F28F3/027—Elements 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
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S165/00—Heat exchange
- Y10S165/355—Heat exchange having separate flow passage for two distinct fluids
- Y10S165/356—Plural plates forming a stack providing flow passages therein
- Y10S165/387—Plural plates forming a stack providing flow passages therein including side-edge seal or edge spacer bar
- Y10S165/391—Plural 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;
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- 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)
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.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US75128868A | 1968-08-08 | 1968-08-08 |
Publications (1)
Publication Number | Publication Date |
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US3542124A true US3542124A (en) | 1970-11-24 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US751288A Expired - Lifetime US3542124A (en) | 1968-08-08 | 1968-08-08 | Heat exchanger |
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Cited By (42)
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 |
US20100043433A1 (en) * | 2008-08-19 | 2010-02-25 | Kelly Patrick J | Heat Balancer for Steam-Based Generating Systems |
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 |
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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 |
-
1968
- 1968-08-08 US US751288A patent/US3542124A/en not_active Expired - Lifetime
Cited By (60)
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 |
US20100045034A1 (en) * | 2008-08-19 | 2010-02-25 | Hinders Edward B | Steam-Based Electric Power Plant Operated on Renewable Energy |
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 |
US20100043433A1 (en) * | 2008-08-19 | 2010-02-25 | Kelly Patrick J | Heat Balancer for Steam-Based Generating Systems |
US20100314088A1 (en) * | 2009-06-11 | 2010-12-16 | Agency For Defense Development | Heat exchanger having micro-channels |
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