EP1557632A2 - Assemblage d'échange de chaleur - Google Patents
Assemblage d'échange de chaleur Download PDFInfo
- Publication number
- EP1557632A2 EP1557632A2 EP05290174A EP05290174A EP1557632A2 EP 1557632 A2 EP1557632 A2 EP 1557632A2 EP 05290174 A EP05290174 A EP 05290174A EP 05290174 A EP05290174 A EP 05290174A EP 1557632 A2 EP1557632 A2 EP 1557632A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- heat exchanger
- exchanger assembly
- corner
- assembly
- component
- 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.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 claims abstract description 24
- 230000008569 process Effects 0.000 claims abstract description 9
- 239000000463 material Substances 0.000 claims description 36
- 230000007704 transition Effects 0.000 claims description 24
- 238000005219 brazing Methods 0.000 claims description 13
- 230000013011 mating Effects 0.000 claims description 11
- 238000001125 extrusion Methods 0.000 claims description 8
- 239000000203 mixture Substances 0.000 claims description 5
- 230000000712 assembly Effects 0.000 abstract description 15
- 238000000429 assembly Methods 0.000 abstract description 15
- 238000004519 manufacturing process Methods 0.000 description 13
- 239000002184 metal Substances 0.000 description 6
- 238000007789 sealing Methods 0.000 description 5
- 239000007769 metal material Substances 0.000 description 4
- 239000004593 Epoxy Substances 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 238000004904 shortening Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000003339 best practice Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001010 compromised effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 239000010421 standard material Substances 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
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
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/02—Header boxes; End plates
- F28F9/0219—Arrangements for sealing end plates into casing or header box; Header box sub-elements
- F28F9/0224—Header boxes formed by sealing end plates into covers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2275/00—Fastening; Joining
- F28F2275/04—Fastening; Joining by brazing
Definitions
- the present invention relates generally to a heat exchanger and heat exchanger assembly, and, particularly, leak tight heat exchanger assemblies with coined or extruded corners.
- Heat exchangers are used in the automotive industry as essential parts of a vehicle cooling system.
- Modern heat exchangers usually consist of a fin and tube assembly called a core, with variations to the basic design including tube attachments to manifold components on opposite ends of the core.
- the heat exchanger can be placed in an oven along with other attachments and components to 'bake' or braze individual them together, yielding a resultant product that combines fins, tubes, and manifolds bonded together to form a single integrated heat exchanger assembly.
- heat exchangers assemblies are subject to pressure variations and act as pressure vessels.
- vessels can take many shapes and require specific contours in order to deal with the constraints of limited space packaging, etc. of the motor vehicle. They must, however, at the same time, be able to maintain their structural integrity (remain 'leak tight') in often extremely high and /or low pressure environments.
- Compound bonding joints are joints commonly made up of at least two flat intersecting planes forming a sharp corner, mated with two flat intersecting planes connected by a radius. The fit yields a form of bonding joint, and, particularly, a joint that may be bonded or brazed in an oven or the like. Compound bonding joints often have the disadvantage of developing leaks at points where the greatest gap occurs between the radius and sharp corner in the bonding joint. The same problem exists in the prior art in similar designs involving at least three intersecting planes.
- bonding joints are often comprised of various bonding materials of somewhat differing natures, including added bonding materials to increase material mass, addition of other components parts near or around the joint area, or otherwise compensate for structural weakness.
- These manufacturing variations may comprise good joint fitup, or joint integrity and the like. Addition of increased mass or volume of materials near or around the joint area may be a way of providing thicker gage base material to get better bonding results, but is not an ideal way to compensate for poor bonding joint design, as it does not assure the joint will be leak free, and usually results in resultant higher manufacturing costs.
- An object of the present invention is to provide an improved joint, and, in particularly, a "bonded" or bonding joint that would be used in a 'leak tight' heat exchanger assembly. It is further an object of the present invention to provide for a improved heat exchanger assembly that retains its leak tight features while additionally maintaining heat exchanger assembly structural integrity and durability.
- the present invention in its preferred embodiments, eliminates the radius found in the prior art, while maintaining structural integrity and providing for leak tight bonds in the bonding joint area, particularly for heat exchanger assemblies that have brazed bonding joints.
- the heat exchanger assembly is designed to provide for a leak tight seal or connection between heat exchanger assembly components, without the need for a radius for increased structural integrity.
- Preferred aspects of the present invention provide for a leak tight joint or joints at areas of contact between elements of the manifold assembly.
- Particularly preferred aspects of the present invention provide for a leak tight joint at the point of contact or 'intersection' of plane surfaces in a manifold assembly.
- Preferred aspects of the present invention also provide for a method of making a heat exchanger assembly providing leak tight features while maintaining heat exchanger structural integrity and durability by 'coining' or extruding matching component intersecting surfaces in a local area to preferably create shaped contour areas that match or mate with each other at the binding joints.
- More preferred aspects provide for a method a making and a heat exchanger assembly wherein the local area comprises a localized brazing zone at the point or points of contact or mating fits found at or near the intersection of the manifold assembly intersecting planes, creating a so-called 'mating' or 'pairing' surface or surfaces where consistent bonding may occur.
- Even more preferred aspects of the present invention provide for a heat exchanger assembly, with manifold, having corner bonding joint between the header or manifold, formed from a channel, a tube, or a cap, or any combination of the above.
- Also more preferred aspects provide for at least one corner bonding joint that is sharp or angled, and, preferably straight angled corner; in most preferred aspects, the corner comprising the bonding joint is a coined corner.
- heat exchanger assemblies are found with localized transition zone bonds provide for optimized seal formation without compromising structural or braze seal integrity.
- the advantage of this strengthened bond design is components designed for strength also have a properly designed bond joint which provides superior quality bond joints for leak free service, improved fitup of components, no impact to durability of the assembly, and reduced cost to manufacture.
- a coined corner is a corner formed by at two or more straight planes at some angle of intersection.
- three or more straight planes meet at straight (uncurved) angles at a zone of intersection.
- corner bonding joint is meant a joint capable of being bonded, formed at a corner, the corner formed with straight angles, and not utilizing a radius between connecting planes of the bonding joint area.
- coined corner is mean a comer formed by extrusion or press fit, or, preferably, by extrusion and press fitting.
- the coined corner is formed at a localized zone of junction of the tube and header and more preferred, formed at a localized zone between the tube and header. More preferably, it is formed at the transition wherein the tube, or tube and header, all have mating surfaces where a bond joint can be formed. More preferably, the tube at the area of the bond joint has the approximately the same or similar dimension (is equal to or less then twice the size of the tube at the corner area), or is unsplit.
- a method of producing an heat exchanger assembly that is designed for strength and durability, with components that have a strength/bond transition zone for providing proper joint clearances to oven bond leak tight heat exchangers, is provided.
- the heat exchanger assembly is subsequently tested prior to other procedures or immediately leak tested and shipped to the customer thereby shortening the manufacturing process and reducing overall cost.
- the present invention provides for preferred embodiments whose design promotes the use of a single material or materials that have approximately the same metallurgical composition as the bonding material to make the complete heat exchanger thereby supporting recycling mandates.
- this invention reduces cost, and rework, while shortening manufacturing time.
- This invention provides a manifold designed for durability, where needed, and designing proper bond joints, where needed, without compromising either durability or bond joint design.
- the present invention therefore, provides a method of making a heat exchanger assembly wherein maximum durability of the heat exchanger coexists with best practices, i.e. efficient and leak tight assemblies utilizing bond joint designs.
- various materials may be used in the manufacture of the heat exchanger assembly.
- the present invention provides for use of clad or unclad materials. These materials made be metallic or non-metallic materials. Preferred is when the materials used in the heat exchanger are either metallic or non-metallic. Preferred is when at least one of the materials used in the heat exchanger assembly is metallic at a point of surface contact or bonding, or at a joint. Also preferred is when at least one of the materials used in the heat exchanger assembly is non-metallic.
- a heat exchanger assembly using combination of metallic and non-metallic materials. Even more preferred is a heat exchanger assembly wherein the joints and/or surface areas or zones where bonding occur are comprised of metallic or non-metallic materials. Most preferred is wherein the joints and/or surface areas or zones where bonding occur are of essentially the same material. Also preferred is wherein the joints and/or surface areas or zones where bonding occur are more than 90% metallic and are essentially the same material.
- the bond joint uses standard materials (i.e. materials used in normal quantity and of normal quality during assembly and brazing, and not including additional material or products such as glues or resins or other such additional materials) in the construction of heat exchangers comprising the embodiments of the present invention, resulting in reduced overall production costs per unit of the heat exchanger.
- the adjacent surface area is maximized for bonding.
- the present invention uses 'simplified' bond joint designs to provide adjacent surface areas or a zone of a relatively greater nature than those in the prior art designs described hereinabove.
- a standardized method of producing a bond joint is provided.
- the heat exchangers produced thereby provide a substantially or essentially leak tight heat exchanger assembly joint or bond.
- the surfaces that form the joint or bond are 'coined' or extruded contiguous with a transition surface to provide for a long durability bonding between components of the heat exchanger assembly , and , particularly, brazed components.
- additional process steps of component manufacturing found in the prior art are eliminated via the integrality of form tooling, thereby reducing assembly complexity.
- additional formed features such as 'fillers' or other 'gap closers' that have been used to close gaps of normal bend radii at the joint area, are eliminated.
- the present invention provides for a heat exchanger and heat exchanger assembly, particularly a 'one shot' or similar material brazed heat exchanger assembly wherein braze closure is uniform or practically achieved over the entire surface of the joint areas or zone, to form essentially leak proof joints.
- the present invention further provides a multiple component interface braze closure uniform or practically achieved over the entire surfaces of the joint areas or zone at multiple component interfaces.
- the present invention further provides a sealed multiple component assembly useful in a variety of bonding process.
- the present invention preferably provides a braze sealed with a bend radius.
- Preferred embodiments of the present invention provide a light weight heat exchanger, essentially without additional material to ensure braze leak tight joints or correct for joint deficiencies.
- all metal heat exchanger or manifold assembly it is meant a heat exchanger or assembly where all or most parts or components capable of being brazed or joined together in a device such as an oven, are based on metallic materials.
- Preferred are so called 'one shot braze' all metal heat exchanger with manifold assemblies wherein the part or components , as well as any brazing or joining materials, are of a similar or like substance, so as to be capable of being brazed or joined together in an oven while providing for leak tight seals amongst the components at the joints.
- More preferred are all metal heat exchanger or manifold assemblies wherein coining or extrusion features appear at the areas of contact or zones of the joint.
- heat exchanger or manifold assemblies where the edges or surfaces of joints that occur at the junctures of planes in the assembly are coined or extruded.
- the coining or extrusion feature is only done at the naturally reinforced juncture of multiple planes so as it does not impact the durability of the heat exchanger.
- naturally reinforced it is meant that multiple thicknesses of the mating surfaces in the area of the coined corner are bonded together to form a single zone or area, a so called 'single assembly'.
- the present invention provides for structual sections designed for strength and durability with formed sections having two or more planes unconnected by a radius, that increase or enhance the leak proof or leak tight nature of the assembly at the area of the angle and joint formed at the intersection of the two or more planes.
- the heat exchanger comprises a core composed of tubes and fins, with manifolds preferably formed of flat sheet stock, the manifold having a header portion with at least one opening or openings connecting to the at least one tube end or ends; a first and second component portion comprising or consisting of an header or tubes or tanks or channels within or near a corner area with each portion having an extended planer bonding surface that are closely aligned to each other; and, a more preferably third component portion.
- the third component portion has an extended planar bonding surface being adjoined or affixed to the first bonding surface forming intersecting bonding surfaces located near the terminal end of the first and second portion surfaces bonding surfaces.
- the second component portion has matching intersecting surfaces such that the transition contour of the second portion is locally deformed to create a shaped contour that matches the transition area of the first component portion intersecting surface transition area forming bonding joints. More preferably, the bonding joints are bonded with a bonding material.
- a first part of the bonding joint is formed into one section where two or more planes are at an angle with each other (a structural part or section)
- a second part is formed out of the structural section and is coined to form a small section where the planes are at an angle with each other and mate with the first part of the bonding joint to form an improved complete bonding joint.
- the preferred bonding joints of the present invention can be formed with intersection planar surfaces from various components of the heat exchanger assembly.
- the bonding joint preferably occurs at an area where a heat exchanger core tube and header meet at the header ferrule, where a heat exchanger core tube and tank meet , where a tank and a header meet, where a tube and a header meet, or where a bonding joint is itself included as part of a mounting structure to a tank.
- Caps, walls, pans, channels and other such components where flat planes are capable of intersection in a corner transition area are intended as unlimiting examples useful in embodiments of the present invention.
- the first and second component portion within or near a corner area are found, with each portion having an extended planer bonding surface that closely follows or runs in parallel to each other.
- one of the component portions forms a single plane in the area of the bonding joint, and the two other component portions (two structural members) abutt and are parallel to the bonding joint adjacent to the single plane; even more preferred are two component portions parallel to one another and a third forming an angle relative to the two at the intersection area of the joint.
- embodiments of the present invention further have a third component portion having an extended planar bonding surface adjoined or affixed to the first component portion bonding surface, the bonding surfaces intersecting near terminal ends of the first and second component portions planar bonding surfaces, the terminal ends of the bonding surfaces being within or near a corner area.
- the first and second component portion are formed in a "U" channel shape such that the second portion is more narrow and sits or rests within and between the first portion. Also preferred are embodiments wherein the heat exchanger first and second component portion has symmetrically opposed formed transition comers. Even more preferred is wherein the transition area approximately forms a sharp comer.
- a heat exchanger assembly comprising a manifold assembly having at least one tube and a header and, a heat exchanger core, wherein the manifold assembly has at least one coined corner and wherein the assembly is essentially leak tight at the area of the corner.
- Fig 1 shows a design wherein tank 12 forms a braze joint between tank 12 and header wall 11 to form the manifold assembly. Header wall 11 has an additional form 13 to fill a gap caused by fitting the flat side of tank 12 against a formed radius on tank end 14 .
- Fig. 2 refers to an all-metal heat exchanger assembly, for example, wherein a plurality of components is assembled together to create the manifold assembly.
- Sealing Cap 23 , Header Wall 22 , Header Pan 21 , and Cap Crimp Tab 25 are 'baked' of oven 'brazed' to form an integral manifold 26 for an heat exchanger assembly.
- Fig. 2 is a prior art design where header wall 22 butts against header pan 21 and against sealing cap 23 forming the manifold assembly. Header wall 22 , sealing cap 23 , and header pan 21 form a joint where the radius of the header pan 21 fits against the square edges of header wall 22 and sealing cap 23 at location 24 .
- Fig. 3 is an embodiment of the present invention wherein combined header and channel 32 is assembled to a cap 32 to form a manifold assembly with the coined area 33 providing a proper braze joint between header and channel 32 and cap 31 at the junction shown at section A (35).
- Fig 3 shows a preferred embodiment of the present invention wherein header and channel 32 are combined and assembled to a cap 31 to form a manifold assembly.
- Coined area 33 provides a proper braze joint between header and channel 32 and cap 31 at the junction shown at section A 35 .
- a transition or transition zones 42 is created in a component between the area 43 designed for durability and the somewhat small area 44 wherein bonding occurs at the intersection of intersecting planes 47 .
- one half of the bond joint will consist of one or more components.
- Fig. 4 further illustrates intersecting on different planes with a sharp corner 47 at the intersection of said planes.
- Planar component portion P1 and planar component portion P2 has a radius that connects the plane for strength.
- Area 47 of intersecting planes is coined to improve the braze joint by having a sharp or straight angled corner fit into another sharp or straight angled corner.
- Fig. 5 shows a preferred embodiment of the present invention wherein formed components with intersecting planes 65 are connected with a radius 62 , which provides a transition zone for stresses between planes.
- Fig. 5 further illustrates an embodiment wherein the design is particularly suitable for bond joint fitup.
- Intersecting planes 65 include a sharp corner at intersection localized section or zone 64 , to assure appropriate levels of material adjacent to the mating portion or zone of the bond joint over the maximum surface.
- Fig. 5 shows Fig.
- cap 45 has bend radius 43 for strength with connecting transition 42 to coined area 44 which enable proper design for durability and proper design for bonding at the intersection of the intersecting planes 47 .
- Fig 5 is Fig 4 cap 45 rotated 90 degrees, cap 63 is comprised of features of intersecting planes 65 , radius 62 for durability, coined corner 64 for bonding, and transition 61 connecting radius 62 to coined corner 64 .
- Plane demarcations A1 and B1 show a structural strengthening joint area.
- Plan demarcations A1 and B2 show a joint area that allows for improved brazing while surprisingly maintaining structural integrity and providing for reduced possibility for leakage (leak tight joint).
- the mating component Fig. 5 will have matching planes 65 formed into said component with a radius 62 connecting said planes.
- This invention utilizes a coining or extrusion process to reform and remold a localized portion 64 of a component from intersecting planes connected by a radius 62 to intersection planes with a sharp comer at the localized portion 64 at the intersection of the intersecting plane with transition 61 as a key feature.
- the reformed section 44 of the component Fig 4 will then fit adjacent to the mating portion of the bond joint 46 , 41 , 48 , maximizing the surface area of the bond joint and minimizing the gaps between components. This enables the bond joint 47 to be fused in an oven for leak tight service.
- the coining or extrusion process would typically be part of the component form tooling, thereby providing this feature with minimal cost.
- part of the transition area between the two planar component portions forms a radius 62 and part of the transition area forms a sharp or coined corner 64 .
- the total bonding joint is improved by the structural strength sections as well as the leak tight coined corner sections.
- FIG. 6a and 6b is shown typical prior art corner 600 , 601 showing un-sharp 603 and non -coined 604 corner in area 602 .
- First plane component 605 and second plane component 606 meet at intervening radius 607 to form structural feature.
- Gap 608 partially filled by feature 609 .
- Gap 610 for potential leak path not filled during bonding.
- FIGs. 7a and 7b is shown sharp 701 and coined 702 corners, with improved leak tight areas 703 , 704 , illustrated.
- Coined corner 705 has, preferably, all bonding surfaces at a constant distance apart 707 .
- components of the heat exchanger manifold, after assembly, are bonded together using a heating means such as a 'furnace' or 'oven'.
- a heating means such as a 'furnace' or 'oven'.
- the first or second component is made of material that has essentially the same metallurgical composition as the bonding material. It is possible, however, that depending on materials, component material can differ in metallurgical composition from the bonding material.
- a method of providing for a heat exchanger assembly with manifold and first and second component portions at the area of at least one corner by: coining the manifold and portions in the area of the corner by press fitting or extrusion; forming a bond joint at the area of the corner between surfaces at their mating areas; brazing the heat exchanger assembly; so that the heat exchanger assembly two component portions meet at a sharp angle to one another in at least one coined corner that is essentially leak tight after brazing.
- heat exchangers in accordance with the present invention preferably have a joint or joints bonded by an oven baking or brazing process. In particularly preferred embodiments in accordance with the present invention, the joints are bonded by a flame braze process.
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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)
- Details Of Heat-Exchange And Heat-Transfer (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US53936804P | 2004-01-26 | 2004-01-26 | |
US539368P | 2004-01-26 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1557632A2 true EP1557632A2 (fr) | 2005-07-27 |
EP1557632A3 EP1557632A3 (fr) | 2008-04-02 |
Family
ID=34633033
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05290174A Withdrawn EP1557632A3 (fr) | 2004-01-26 | 2005-01-26 | Assemblage d'échange de chaleur |
Country Status (2)
Country | Link |
---|---|
US (1) | US20050161207A1 (fr) |
EP (1) | EP1557632A3 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7798206B2 (en) * | 2006-02-07 | 2010-09-21 | Showa Denko K.K. | Heat exchanger and method of manufacturing the same |
US20080156455A1 (en) * | 2006-12-14 | 2008-07-03 | Powers Michael V | Heat exchanger manifolds with retention tabs |
JP5741470B2 (ja) * | 2012-02-10 | 2015-07-01 | 株式会社デンソー | 熱交換器、およびその製造方法 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08327278A (ja) * | 1995-05-30 | 1996-12-13 | Sanden Corp | 熱交換器のタンク |
EP0838652A2 (fr) * | 1996-10-23 | 1998-04-29 | Denso Corporation | Echangeur de chaleur |
US20030217838A1 (en) * | 2002-05-23 | 2003-11-27 | Valeo Engine Cooling, Inc. | Heat exchanger header assembly |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2488627A (en) * | 1946-02-28 | 1949-11-22 | Young Radiator Co | Tube and header-plate assembly for heat-exchange units |
US4960169A (en) * | 1989-06-20 | 1990-10-02 | Modien Manufacturing Co. | Baffle for tubular heat exchanger header |
US5172761A (en) * | 1992-05-15 | 1992-12-22 | General Motors Corporation | Heat exchanger tank and header |
JP3624486B2 (ja) * | 1994-12-20 | 2005-03-02 | 株式会社デンソー | 熱交換器およびその製法 |
US5842515A (en) * | 1995-09-30 | 1998-12-01 | Halla Climate Control Corporation | Heat exchanger and method of manufacturing header pipe for the same |
JP3857791B2 (ja) * | 1996-11-19 | 2006-12-13 | カルソニックカンセイ株式会社 | 熱交換器用タンク |
DE10103570A1 (de) * | 2001-01-26 | 2002-08-01 | Modine Mfg Co | Wärmetauscher und Herstellungsverfahren |
US20030159813A1 (en) * | 2002-02-28 | 2003-08-28 | Norsk Hydro | Heat exchanger manifold and method of assembly |
-
2005
- 2005-01-26 EP EP05290174A patent/EP1557632A3/fr not_active Withdrawn
- 2005-01-26 US US11/043,310 patent/US20050161207A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08327278A (ja) * | 1995-05-30 | 1996-12-13 | Sanden Corp | 熱交換器のタンク |
EP0838652A2 (fr) * | 1996-10-23 | 1998-04-29 | Denso Corporation | Echangeur de chaleur |
US20030217838A1 (en) * | 2002-05-23 | 2003-11-27 | Valeo Engine Cooling, Inc. | Heat exchanger header assembly |
Also Published As
Publication number | Publication date |
---|---|
US20050161207A1 (en) | 2005-07-28 |
EP1557632A3 (fr) | 2008-04-02 |
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