US20070012425A1 - Heat exchanger - Google Patents
Heat exchanger Download PDFInfo
- Publication number
- US20070012425A1 US20070012425A1 US11/524,422 US52442206A US2007012425A1 US 20070012425 A1 US20070012425 A1 US 20070012425A1 US 52442206 A US52442206 A US 52442206A US 2007012425 A1 US2007012425 A1 US 2007012425A1
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- United States
- Prior art keywords
- tube
- tank
- joint part
- ribs
- tubes
- 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.)
- Abandoned
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
- F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
- F28D1/04—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits
- F28D1/053—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight
- F28D1/0535—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with tubular conduits the conduits being straight the conduits having a non-circular cross-section
- F28D1/05366—Assemblies of conduits connected to common headers, e.g. core type radiators
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- 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
- F28F9/0226—Header boxes formed by sealing end plates into covers with resilient gaskets
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/06—Constructions of heat-exchange apparatus characterised by the selection of particular materials of plastics material
- F28F21/062—Constructions of heat-exchange apparatus characterised by the selection of particular materials of plastics material the heat-exchange apparatus employing tubular conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2265/00—Safety or protection arrangements; Arrangements for preventing malfunction
- F28F2265/26—Safety or protection arrangements; Arrangements for preventing malfunction for allowing differential expansion between elements
Definitions
- the present invention relates to a heat exchanger.
- the heat exchanger can be suitably used as a radiator of a water-cooled internal combustion engine in which heat is exchanged between cooling water and air.
- U.S. Pat. No. 6,988,544 discloses a heat exchanger including a core portion and a tank.
- a heat exchanger including a core portion and a tank.
- the tank is disposed at the ends of the tubes in the longitudinal direction, and includes a core plate and a tank portion.
- the tubes are inserted into the core plate, and the tank portion is fixed to the core plate by caulking.
- the tank portion forms a space of the tank together with the core plate.
- the core plate has tube inserting holes on a tube joint part, and a wall portion at a periphery of the tube joint part.
- the wall portion is bent approximately in perpendicular to the tube joint part.
- ribs are formed parallel to the tube inserting holes on the tube joint part.
- a rigidity of the core plate is enhanced by connecting ends of the ribs to the wall portion such that a deformation of the core plate mainly due to an inner pressure can be reduced.
- the tubes When the heat exchanger is used as a radiator for an automobile, the tubes may be damaged due to a generation of a thermal strain. Especially in a winter season, the tubes may be easily damaged because a temperature difference between cooling water and air is large. Moreover, the temperature difference may become large in a cross-flow heat exchanger, in which a longitudinal direction of the tubes corresponds to a shape of an aperture portion of a grill of the automobile, because one tube is easy to be cooled by air, while another tube is difficult to be cooled by the air.
- the thermal strain can be absorbed in the tank.
- the thermal strain cannot practically be absorbed in the flexible tank.
- a thermal strain not absorbed by the deformation of the tank can be absorbed, because a tube joint part 22 of the core plate 20 can be deformed in the tube longitudinal direction X.
- the part 22 is deformed approximately in a circular arc.
- a dashed line represents a state in which the temperature difference between tubes 10 does not exist, and a full line represents a state in which the temperature difference of the tubes 10 is large.
- an affect of the thermal strain is concentrated on edge portions of the tube 10 in the tube width direction Z, because the tube joint part 22 is deformed approximately in the circular arc.
- a heat exchanger includes a plurality of flat tubes stacked with each other in a tube stacking direction, and a tank connected at an end of each tubes in a tube longitudinal direction to communicate with the tubes.
- Each of the tubes extends in the tube longitudinal direction.
- the tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank.
- the tank further includes a plurality of ribs on the tube joint part. The ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction. The ends of the ribs in the tube width direction are positioned outside of the ends of the tube inserting holes.
- the tube joint part has a deformation allowable portion outside of the ends of the ribs in the tube width direction.
- the deformation allowable portion allows the tube joint part to be deformed in the tube longitudinal direction.
- the tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
- a heat exchanger includes a plurality of flat tubes stacked with each other in a tube stacking direction, and a tank connected at an end of each tubes in a tube longitudinal direction to communicate with the tubes.
- Each of the tubes extends in the tube longitudinal direction.
- the tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank.
- the tank further includes a plurality of ribs on the tube joint part. The ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction.
- the tank further includes a wall portion bent from a periphery portion of the tube joint part.
- a stress concentration on edge portions of a tube in a tube width direction can be reduced, and a stress can be reduced in all area of the tube in the tube width direction.
- FIG. 1 is a front view of a heat exchanger according to a first embodiment of the present invention
- FIG. 2 is a perspective cross-sectional view of a tank and tubes in the heat exchanger shown in FIG. 1 ;
- FIG. 3A is a front view of a single core plate shown in FIG. 2
- FIG. 3B is a bottom view of the single core plate shown in FIG. 3A ;
- FIG. 4 is a cross-sectional view of the single core plate taken along line IV-IV shown in FIG. 3B ;
- FIG. 5 is a cross-sectional view of the single core plate taken along line V-V shown in FIG. 3B ;
- FIG. 6 is a pattern diagram showing a deformation example of a core plate and a tube in the heat exchanger shown in FIG. 1 ;
- FIG. 7 is a bottom view of a single core plate in a heat exchanger according to a second embodiment
- FIG. 8 is a cross-sectional view of the single core plate taken along line VIII-VIII shown in FIG. 7 ;
- FIG. 9 is a bottom view of a single core plate in a heat exchanger according to a third embodiment.
- FIG. 10 is a cross-sectional view of the single core plate taken along line X-X shown in FIG. 9 ;
- FIG. 12 is a pattern diagram showing a deformation example of a core plate and a tube in a conventional heat exchanger.
- a heat exchanger in a first embodiment is used for a radiator for cooling an engine (water-cooled internal combustion engine).
- the heat exchanger includes an approximately cuboid-shaped core portion 1 formed by alternately stacking a plurality of tubes 10 and a plurality of corrugate fins 11 along up-and-down direction in FIG. 1 .
- the stacking direction of the tubes 10 and the corrugate fins 11 is defined as a tube stacking direction Y.
- the corrugate fins 11 are made of aluminum alloy, and made in a corrugated shape so as to promote a heat exchange between air and cooling water.
- the tubes 10 have passages therein for flowing the cooling water of the water-cooled internal combustion engine (not shown) mounted to an automobile, and are formed by welding or blazing after a board made of aluminum alloy is bent in a predetermined shape.
- the longitudinal direction of the tubes 10 is defined as a tube longitudinal direction X, which corresponds to a horizontal direction in FIG. 1 .
- the cross-sectional shape of the tubes 10 is formed in a flat shape such that a major diameter direction of the flat shape corresponds to an air flowing direction C, as shown in FIG. 2 .
- a perpendicular direction to both the tube stacking direction Y and the tube longitudinal direction X is defined as a tube width direction Z.
- the tube width direction Z corresponds to the major diameter direction of the tubes 10 and the air flowing direction C.
- the tank 2 includes an inlet pipe 20 , which is connected to an outlet of the engine through a hose (not shown).
- water cooled by exchanging heat with air flows out of each passage of the tubes 10 , and the water is joined together in the tank 3 . Then, the water is discharged toward the engine.
- the tank 3 includes an outlet pipe 30 , which is connected to an inlet of the engine through a hose (not shown).
- side plates 4 for strengthening a structure of the core portion 1 are disposed in both the ends of the core portion 1 in the tube stacking direction Y.
- the side plates 4 are made of an aluminum alloy, and extend parallel to the tube longitudinal direction X such that the ends of the side plates 4 are connected to the tanks 2 , 3 .
- Each of the tanks 2 , 3 include a core plate 20 , a tank portion 21 and a packing (not shown).
- the tubes 10 and the side plates 4 are inserted into the core plate 20 so as to be fixed.
- a space 2 a of the tanks 2 , 3 is constructed by the core plate 20 and the tank portion 21 , as shown in FIG. 2 .
- the core plate 20 is made of aluminum alloy, and the tank portion 21 is made of resin, e.g., glass-reinforced nylon 66 .
- the tank portion 21 is fixed to the core plate 20 by caulking. For example, the tank portion 21 is deformed such that protrusions 251 of the core plate 20 is fastened to the tank portion 21 .
- the protrusions 251 will be described in detail below.
- the core plate 20 has a tube joint part 22 , to which the tubes 10 are connected.
- a groove 20 a is formed in the all periphery of the tube joint part 22 .
- the edges of the tank portion 21 and the packing are inserted into the groove 20 a having a cross-section approximately in a rectangular shape.
- the groove 20 a has three portions. That is, the groove 20 a is formed of an inside wall portion 23 , a bottom wall portion 24 and an outside wall portion 25 . As shown FIGS. 4 and 5 , the inside wall portion 23 is bent approximately perpendicular to the periphery portion of the tube joint part 22 , and extends in the tube longitudinal direction X. The bottom wall portion 24 is bent approximately perpendicular to the inside wall portion 23 , and extends in the tube stacking direction Y The outside wall portion 25 is bent approximately perpendicular to the bottom wall portion 24 , and extends in the tube longitudinal direction X. The protrusions 251 are formed at the end of the outside wall portion 25 .
- ribs 223 are formed between the tube inserting holes 221 adjacent to each other, and between the tube inserting hole 221 and the side plate inserting hole 222 .
- the ribs 223 are formed on the surface of the tube joint part 22 by pressing, for example, so as to be protruded and convex outside of the tank.
- the peripheries of the inserting holes 221 , 222 are protruded to be convex inside of the tank by the punching process. As shown in FIG. 4 , between the inserting holes 221 , 222 and the ribs 223 , base faces 224 not protruded from the tube joint part 22 are left, because the pitch of the tubes 10 is relatively large in this embodiment. Boundary lines between the protruded portions of the inserting holes 221 , 222 and the base faces 224 are defined as inserting hole boundary lines 225 , when the tube joint part 22 is seen from the inside of the tank.
- the inserting holes 221 , 222 and the ribs 223 extend in the tube width direction Z, and the ribs 223 are longer than the inserting holes 221 , 222 in the tube width direction Z. Further, the ends of the ribs 223 in the tube width direction Z are more peripheral than the ends of the inserting holes 221 , 222 in the tube width direction Z. Specifically, the ends of the ribs 223 in the tube width direction Z are more outside than the ends of the inserting hole boundary line 225 in the tube width direction Z.
- a dimension L 1 in the tube width direction Z is provided between the end of the tube inserting hole 221 and the inside wall portion 23 .
- a dimension in the tube width direction Z between the end of the tube inserting hole 221 and the end of the rib 223 is defined as a rib protruding length L 2 .
- the rib protruding length L 2 may be about one third of the dimension L 1 .
- the ends of the ribs 223 in the tube width direction Z do not extend to the inside wall portion 23 . That is, the ends of the ribs 223 in the tube width direction Z are not connected to the inside wall portion 23 . Therefore, the tube joint part 22 has a flat face 226 in a more peripheral area than the ends of the inserting holes 221 , 222 and the ribs 223 in the tube width direction Z.
- the flat face 226 is flat over the all area in the tube stacking direction Y
- the deformation of the tube joint part 22 in the tube longitudinal direction X becomes easier due to the flat face 226 . That is, the flat face 226 corresponds to a deformation allowable portion in this embodiment.
- the ends of the ribs 223 in the tube width direction Z are positioned more peripherally than the ends of the tube inserting holes 221 in the tube width direction Z such that the rigidity around the tube inserting hole 221 is enhanced. Therefore, even when the temperature difference between the tubes 10 is large, the tube joint part 22 adjacent to the tube inserting hole 221 is difficult to be deformed approximately in an arc such that the almost linear shape can be maintained in the tube joint part 22 , as shown in FIG. 6 . That is, the difference in the stretching of the tubes 10 between the edge portion and the center portion in the tube width direction Z becomes small such that the stretching of the tube 10 can be uniform in the all area in the tube width direction Z. Accordingly, the stress concentration on the edge portion in the tube width direction Z can be reduced in the tube 10 .
- the flat face 226 is easy to be deformed in the tube longitudinal direction X. Therefore, when the temperature difference between the tubes 10 is large, as shown in FIG. 6 , the core plate 20 is deformed in the tube longitudinal direction X by the deformation of the flat face 226 . Accordingly, the thermal strain of the tubes 10 can be absorbed by the deformation such that the stress in the all area in the tube width direction Z can be decreased in the tube 10 .
- the stress concentration on the edge portion in the tube width direction Z and the stress in the all area in the tube width direction Z can be reduced in the tube 10 .
- the ends of the ribs 223 in the tube width direction Z are more peripheral than the ends of the inserting hole boundary line 225 in the tube width direction Z.
- the rib protruding length L 2 is about one third of the dimension L 1 , the rigidity around the tube inserting holes 221 is enhanced. Therefore, the periphery of the tube inserting hole 221 is restricted to be deformed in an arc, and the flat face 226 is easily deformed in the tube longitudinal direction X.
- the tube inserting holes 221 may be formed by a burring process.
- the other parts can be made similarly to the above-described first embodiment.
- the tube inserting hole 221 and the rib 223 may be connected without the base face 224 .
- the tube inserting holes 221 are formed at tip ends of plural V-shaped grooves in cross-section
- the ribs 223 are formed at opposite tip ends of the plural V-shaped grooves in cross-section.
- the core plate 20 has a plurality of approximately V-shaped cross-sections such that the strength of the core plate 20 is increased.
- the V-shaped parts can be blazed together to form the tube inserting holes 221 and the ribs 223 , after being separately formed.
- the both ends of the V-shaped grooves in the tube width direction Z are connected to the flat face 226 smoothly in a curve.
- the tube joint part 22 of the core plate 20 is formed in zigzag without a flat surface between the rib 223 and the tube inserting hole 221 in the tube stacking direction, the performance of the heat exchanger can be more improved.
- burring portions 227 may be formed at the peripheries of the tube inserting holes 221 in the above-described embodiments.
- the rib 223 is formed at each portion between adjacent tube inserting holes 221 in the tube stacking direction Y.
- the ribs 223 may be formed partially between the adjacent tube inserting holes 221 in the tube stacking direction Y.
- the ribs 223 may be formed in every other portion between the holes 221 .
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Details Of Heat-Exchange And Heat-Transfer (AREA)
Abstract
A heat exchanger includes a plurality of flat tubes stacked with each other, and a tank connected at an end of each tubes to communicate with the tubes. The tank includes a tube joint part having a plurality of tube inserting holes, and a plurality of ribs extending in a tube width direction on the tube joint part. The ends of the ribs are positioned outside of the ends of the tube inserting holes. The tube joint part has a deformation allowable portion at an outside of the ends of the ribs so as to allow the tube joint part to be deformed in a tube longitudinal direction. The tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
Description
- This application is based on Japanese Patent Application No. 2005-105815 filed on Apr. 1, 2005, the disclosure of which is incorporated herein by reference in its entirety.
- 1. Field of the Invention
- The present invention relates to a heat exchanger. For example, the heat exchanger can be suitably used as a radiator of a water-cooled internal combustion engine in which heat is exchanged between cooling water and air.
- 2. Description of Related Art
- U.S. Pat. No. 6,988,544 (corresponding to JP-A-2004-219044) discloses a heat exchanger including a core portion and a tank. In the core portion, a plurality of tubes and a plurality of corrugate fins are alternately stacked. The tank is disposed at the ends of the tubes in the longitudinal direction, and includes a core plate and a tank portion. The tubes are inserted into the core plate, and the tank portion is fixed to the core plate by caulking. The tank portion forms a space of the tank together with the core plate.
- The core plate has tube inserting holes on a tube joint part, and a wall portion at a periphery of the tube joint part. The wall portion is bent approximately in perpendicular to the tube joint part. Moreover, ribs are formed parallel to the tube inserting holes on the tube joint part. A rigidity of the core plate is enhanced by connecting ends of the ribs to the wall portion such that a deformation of the core plate mainly due to an inner pressure can be reduced.
- When the heat exchanger is used as a radiator for an automobile, the tubes may be damaged due to a generation of a thermal strain. Especially in a winter season, the tubes may be easily damaged because a temperature difference between cooling water and air is large. Moreover, the temperature difference may become large in a cross-flow heat exchanger, in which a longitudinal direction of the tubes corresponds to a shape of an aperture portion of a grill of the automobile, because one tube is easy to be cooled by air, while another tube is difficult to be cooled by the air.
- When the tank is flexible in the tube stacking direction, that is, when the tank is independently deformable in the tube longitudinal direction in accordance with a thermal strain of each tube, the thermal strain can be absorbed in the tank. However, the thermal strain cannot practically be absorbed in the flexible tank.
- As shown in
FIG. 12 , in a heat exchanger not having ribs on acore plate 20 of a tank, a thermal strain not absorbed by the deformation of the tank can be absorbed, because atube joint part 22 of thecore plate 20 can be deformed in the tube longitudinal direction X. Thepart 22 is deformed approximately in a circular arc. InFIG. 12 , a dashed line represents a state in which the temperature difference betweentubes 10 does not exist, and a full line represents a state in which the temperature difference of thetubes 10 is large. When the temperature difference is large, an affect of the thermal strain is concentrated on edge portions of thetube 10 in the tube width direction Z, because thetube joint part 22 is deformed approximately in the circular arc. Thereby, the stretching of the edge portion ES is larger than a stretching of a center portion CS in the tube width direction Z, as shown inFIG. 12 . Thus, especially a large stress may be generated at the edge portion of thetube 10 in the tube width direction Z. - In contrast, in the heat exchanger disclosed in U.S. Pat. No. 6,988,544, the core plate is difficult to be deformed in the tube longitudinal direction, because the rigidity of the core plate is enhanced by the ribs. Thus, the margin for absorbing a thermal strain of the tube is small in the core plate such that a large stress is equally generated in all area in the tube width direction.
- In view of the foregoing and other problems, it is an object of the present invention to provide a heat exchanger, in which a stress concentration on edge portions of a tube in the tube width direction is reduced and a stress is reduced in all area in the tube width direction.
- According to a first example of the present invention, a heat exchanger includes a plurality of flat tubes stacked with each other in a tube stacking direction, and a tank connected at an end of each tubes in a tube longitudinal direction to communicate with the tubes. Each of the tubes extends in the tube longitudinal direction. The tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank. The tank further includes a plurality of ribs on the tube joint part. The ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction. The ends of the ribs in the tube width direction are positioned outside of the ends of the tube inserting holes. The tube joint part has a deformation allowable portion outside of the ends of the ribs in the tube width direction. The deformation allowable portion allows the tube joint part to be deformed in the tube longitudinal direction. The tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
- According to a second example of the present invention, a heat exchanger includes a plurality of flat tubes stacked with each other in a tube stacking direction, and a tank connected at an end of each tubes in a tube longitudinal direction to communicate with the tubes. Each of the tubes extends in the tube longitudinal direction. The tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank. The tank further includes a plurality of ribs on the tube joint part. The ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction. The tank further includes a wall portion bent from a periphery portion of the tube joint part. The ends of the ribs in the tube width direction are positioned outside of the ends of the tube inserting holes, without being connected to the wall portion. The tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
- According to the first or second example, a stress concentration on edge portions of a tube in a tube width direction can be reduced, and a stress can be reduced in all area of the tube in the tube width direction.
- The above and other objects, features and advantages of the present invention will become more apparent from the following detailed description made with reference to the accompanying drawings. In the drawings:
-
FIG. 1 is a front view of a heat exchanger according to a first embodiment of the present invention; -
FIG. 2 is a perspective cross-sectional view of a tank and tubes in the heat exchanger shown inFIG. 1 ; -
FIG. 3A is a front view of a single core plate shown inFIG. 2 , andFIG. 3B is a bottom view of the single core plate shown inFIG. 3A ; -
FIG. 4 is a cross-sectional view of the single core plate taken along line IV-IV shown inFIG. 3B ; -
FIG. 5 is a cross-sectional view of the single core plate taken along line V-V shown inFIG. 3B ; -
FIG. 6 is a pattern diagram showing a deformation example of a core plate and a tube in the heat exchanger shown inFIG. 1 ; -
FIG. 7 is a bottom view of a single core plate in a heat exchanger according to a second embodiment; -
FIG. 8 is a cross-sectional view of the single core plate taken along line VIII-VIII shown inFIG. 7 ; -
FIG. 9 is a bottom view of a single core plate in a heat exchanger according to a third embodiment; -
FIG. 10 is a cross-sectional view of the single core plate taken along line X-X shown inFIG. 9 ; -
FIG. 11 is a cross-sectional view showing a burring portion of a single core plate according to other embodiments; and -
FIG. 12 is a pattern diagram showing a deformation example of a core plate and a tube in a conventional heat exchanger. - (First Embodiment)
- A heat exchanger in a first embodiment is used for a radiator for cooling an engine (water-cooled internal combustion engine). As shown in
FIG. 1 , the heat exchanger includes an approximately cuboid-shapedcore portion 1 formed by alternately stacking a plurality oftubes 10 and a plurality ofcorrugate fins 11 along up-and-down direction inFIG. 1 . The stacking direction of thetubes 10 and thecorrugate fins 11 is defined as a tube stacking direction Y. Thecorrugate fins 11 are made of aluminum alloy, and made in a corrugated shape so as to promote a heat exchange between air and cooling water. Thetubes 10 have passages therein for flowing the cooling water of the water-cooled internal combustion engine (not shown) mounted to an automobile, and are formed by welding or blazing after a board made of aluminum alloy is bent in a predetermined shape. - In this embodiment, the longitudinal direction of the
tubes 10 is defined as a tube longitudinal direction X, which corresponds to a horizontal direction inFIG. 1 . The cross-sectional shape of thetubes 10 is formed in a flat shape such that a major diameter direction of the flat shape corresponds to an air flowing direction C, as shown inFIG. 2 . A perpendicular direction to both the tube stacking direction Y and the tube longitudinal direction X is defined as a tube width direction Z. The tube width direction Z corresponds to the major diameter direction of thetubes 10 and the air flowing direction C. - As shown in
FIG. 1 ,tanks tube 10 in the tube longitudinal direction X. Thetanks spaces 2 a therein, and extend approximately in the tube stacking direction Y. The ends of thetubes 10 in the tube longitudinal direction X are inserted intotube inserting holes 221 of thetanks tanks tubes 10. The insertingholes 221 will be described in detail below. Thus, each passage of thetubes 10 and thespace 2 a in thetanks - High-temperature cooling water discharged from the engine is distributed into the
tubes 10 through thetank 2. Thetank 2 includes aninlet pipe 20, which is connected to an outlet of the engine through a hose (not shown). In contrast, water cooled by exchanging heat with air flows out of each passage of thetubes 10, and the water is joined together in thetank 3. Then, the water is discharged toward the engine. Thetank 3 includes anoutlet pipe 30, which is connected to an inlet of the engine through a hose (not shown). - As shown in
FIG. 1 ,side plates 4 for strengthening a structure of thecore portion 1 are disposed in both the ends of thecore portion 1 in the tube stacking direction Y. Theside plates 4 are made of an aluminum alloy, and extend parallel to the tube longitudinal direction X such that the ends of theside plates 4 are connected to thetanks tanks core plate 20, atank portion 21 and a packing (not shown). Thetubes 10 and theside plates 4 are inserted into thecore plate 20 so as to be fixed. Aspace 2 a of thetanks core plate 20 and thetank portion 21, as shown inFIG. 2 . - The
core plate 20 is made of aluminum alloy, and thetank portion 21 is made of resin, e.g., glass-reinforced nylon 66. Thetank portion 21 is fixed to thecore plate 20 by caulking. For example, thetank portion 21 is deformed such thatprotrusions 251 of thecore plate 20 is fastened to thetank portion 21. Theprotrusions 251 will be described in detail below. When thetank portion 21 is fixed to thecore plate 20, a packing made of rubber for keeping a sealed property is sandwiched between thecore plate 20 and thetank portion 21. - As shown in
FIG. 3B , thecore plate 20 has a tubejoint part 22, to which thetubes 10 are connected. Agroove 20 a is formed in the all periphery of the tubejoint part 22. The edges of thetank portion 21 and the packing are inserted into thegroove 20 a having a cross-section approximately in a rectangular shape. - The
groove 20 a has three portions. That is, thegroove 20 a is formed of aninside wall portion 23, abottom wall portion 24 and anoutside wall portion 25. As shownFIGS. 4 and 5 , theinside wall portion 23 is bent approximately perpendicular to the periphery portion of the tubejoint part 22, and extends in the tube longitudinal direction X. Thebottom wall portion 24 is bent approximately perpendicular to theinside wall portion 23, and extends in the tube stacking direction Y Theoutside wall portion 25 is bent approximately perpendicular to thebottom wall portion 24, and extends in the tube longitudinal direction X. Theprotrusions 251 are formed at the end of theoutside wall portion 25. - The
tube inserting holes 221 are formed in the tubejoint part 22 of thecore plate 20 at predetermined position in the tube stacking direction Y, and thetubes 10 are inserted into theholes 221 so as to be blazed. As shown inFIG. 3B , sideplate inserting holes 222 are formed at both end portions of the tubejoint part 22 in the tube stacking direction Y. Theside plates 4 are inserted into the sideplate inserting holes 222 so as to be blazed. Thetube inserting holes 221 and the sideplate inserting holes 222 are formed by a punching process, for example. - Moreover,
ribs 223 are formed between thetube inserting holes 221 adjacent to each other, and between thetube inserting hole 221 and the sideplate inserting hole 222. Theribs 223 are formed on the surface of the tubejoint part 22 by pressing, for example, so as to be protruded and convex outside of the tank. - The peripheries of the inserting
holes FIG. 4 , between the insertingholes ribs 223, base faces 224 not protruded from the tubejoint part 22 are left, because the pitch of thetubes 10 is relatively large in this embodiment. Boundary lines between the protruded portions of the insertingholes hole boundary lines 225, when the tubejoint part 22 is seen from the inside of the tank. - The inserting
holes ribs 223 extend in the tube width direction Z, and theribs 223 are longer than the insertingholes ribs 223 in the tube width direction Z are more peripheral than the ends of the insertingholes ribs 223 in the tube width direction Z are more outside than the ends of the insertinghole boundary line 225 in the tube width direction Z. - As shown in
FIG. 3B , a dimension L1 in the tube width direction Z is provided between the end of thetube inserting hole 221 and theinside wall portion 23. Also, a dimension in the tube width direction Z between the end of thetube inserting hole 221 and the end of therib 223 is defined as a rib protruding length L2. Then, the rib protruding length L2 may be about one third of the dimension L1. - The ends of the
ribs 223 in the tube width direction Z do not extend to theinside wall portion 23. That is, the ends of theribs 223 in the tube width direction Z are not connected to theinside wall portion 23. Therefore, the tubejoint part 22 has aflat face 226 in a more peripheral area than the ends of the insertingholes ribs 223 in the tube width direction Z. Theflat face 226 is flat over the all area in the tube stacking direction Y The deformation of the tubejoint part 22 in the tube longitudinal direction X becomes easier due to theflat face 226. That is, theflat face 226 corresponds to a deformation allowable portion in this embodiment. - According to the first embodiment, the ends of the
ribs 223 in the tube width direction Z are positioned more peripherally than the ends of thetube inserting holes 221 in the tube width direction Z such that the rigidity around thetube inserting hole 221 is enhanced. Therefore, even when the temperature difference between thetubes 10 is large, the tubejoint part 22 adjacent to thetube inserting hole 221 is difficult to be deformed approximately in an arc such that the almost linear shape can be maintained in the tubejoint part 22, as shown inFIG. 6 . That is, the difference in the stretching of thetubes 10 between the edge portion and the center portion in the tube width direction Z becomes small such that the stretching of thetube 10 can be uniform in the all area in the tube width direction Z. Accordingly, the stress concentration on the edge portion in the tube width direction Z can be reduced in thetube 10. - Further, when the
tank portion 21 is made of resin, the rigidity of themetallic core plate 20 greatly effects an entire rigidity of the tank. Therefore, the effect of theribs 223 becomes relatively larger in the heat exchanger having thetank portion 21 made of resin. - Moreover, because the ends of the
ribs 223 in the tube width direction Z do not extend to theinside wall portion 23, theflat face 226 is easy to be deformed in the tube longitudinal direction X. Therefore, when the temperature difference between thetubes 10 is large, as shown inFIG. 6 , thecore plate 20 is deformed in the tube longitudinal direction X by the deformation of theflat face 226. Accordingly, the thermal strain of thetubes 10 can be absorbed by the deformation such that the stress in the all area in the tube width direction Z can be decreased in thetube 10. - Accordingly, when the temperature difference between the
tubes 10 is large, the stress concentration on the edge portion in the tube width direction Z and the stress in the all area in the tube width direction Z can be reduced in thetube 10. - Further, because the
ribs 223 are formed between thetube inserting holes 221 adjacent to each other, the rigidity of the periphery of thetube inserting holes 221 can be enhanced such that the periphery of thetube inserting hole 221 is restricted to be deformed in an arc. - Furthermore, the ends of the
ribs 223 in the tube width direction Z are more peripheral than the ends of the insertinghole boundary line 225 in the tube width direction Z. Thereby, when the temperature difference between thetubes 10 is large, the deformation is generated at a more peripheral part than the insertinghole boundary line 225 such that the stress concentration on the insertinghole boundary line 225, i.e., bent portion, can be reduced. - Moreover, because the rib protruding length L2 is about one third of the dimension L1, the rigidity around the
tube inserting holes 221 is enhanced. Therefore, the periphery of thetube inserting hole 221 is restricted to be deformed in an arc, and theflat face 226 is easily deformed in the tube longitudinal direction X. - (Second Embodiment)
- The above-described embodiment is only an example for the heat exchanger of the present invention. It is to be noted that various changes and modifications will be become apparent to those skilled in the art.
- As shown in
FIGS. 7 and 8 , thetube inserting holes 221 may be formed by a burring process. In the second embodiment, the other parts can be made similarly to the above-described first embodiment. - (Third Embodiment)
- As shown in
FIGS. 9 and 10 , when the pitch between thetubes 10 adjacent to each other is small, thetube inserting hole 221 and therib 223 may be connected without thebase face 224. In this case, thetube inserting holes 221 are formed at tip ends of plural V-shaped grooves in cross-section, and theribs 223 are formed at opposite tip ends of the plural V-shaped grooves in cross-section. - The
core plate 20 has a plurality of approximately V-shaped cross-sections such that the strength of thecore plate 20 is increased. The V-shaped parts can be blazed together to form thetube inserting holes 221 and theribs 223, after being separately formed. In this case, the both ends of the V-shaped grooves in the tube width direction Z are connected to theflat face 226 smoothly in a curve. In the third embodiment, because the tubejoint part 22 of thecore plate 20 is formed in zigzag without a flat surface between therib 223 and thetube inserting hole 221 in the tube stacking direction, the performance of the heat exchanger can be more improved. - (Other Embodiments)
- As shown in
FIG. 11 , burringportions 227 may be formed at the peripheries of thetube inserting holes 221 in the above-described embodiments. - In the above-described embodiments, the
rib 223 is formed at each portion between adjacenttube inserting holes 221 in the tube stacking direction Y. However, theribs 223 may be formed partially between the adjacenttube inserting holes 221 in the tube stacking direction Y. For example, theribs 223 may be formed in every other portion between theholes 221. - Such changes and modifications are to be understood as being within the scope of the present invention as defined by the appended claims.
Claims (12)
1. A heat exchanger comprising:
a plurality of flat tubes stacked with each other in a tube stacking direction, each of the tubes extends in a tube longitudinal direction;
a tank connected at an end of each tubes in the tube longitudinal direction to communicate with the tubes, wherein the tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank; and
a plurality of ribs on the tube joint part, wherein the ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction, wherein:
ends of the ribs in the tube width direction are positioned outside of ends of the tube inserting holes;
the tube joint part has a deformation allowable portion outside of the ends of the ribs;
the deformation allowable portion allows the tube joint part to be deformed in the tube longitudinal direction; and
the tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
2. A heat exchanger comprising:
a plurality of flat tubes stacked with each other in a tube stacking direction, each of the tubes extends in a tube longitudinal direction;
a tank connected at an end of each tubes in the tube longitudinal direction to communicate with the tubes, wherein the tank includes a tube joint part having a plurality of tube inserting holes, into which the ends of the tubes are inserted so as to be connected to the tank; and
a plurality of ribs on the tube joint part, wherein the ribs extend in a tube width direction being perpendicular to the tube stacking direction and the tube longitudinal direction, wherein:
the tank further includes a wall portion bent from a periphery portion of the tube joint part;
ends of the ribs in the tube width direction are positioned outside of ends of the tube inserting holes, without being connected to the wall portion; and
the tube joint part has a plurality of approximately V-shaped cross-sections, in which the tube inserting hole and the rib are provided without a flat face therebetween.
3. The heat exchanger according to claim 1 , wherein:
the ribs are disposed between the tube inserting holes adjacent to each other in the tube stacking direction.
4. The heat exchanger according to claim 1 , wherein:
the tank includes a core plate made of metal, and a tank portion made of resin for forming a tank space together with the core plate; and
the core plate includes the tube joint part joined to the tube, and a tank joint part joined to the tank portion.
5. The heat exchanger according to claim 1 , wherein:
the tubes are fixed to the tube inserting holes by blazing.
6. The heat exchanger according to claim 1 , wherein:
the tube inserting hole is provided to have a burring portion in its periphery.
7. The heat exchanger according to claim 1 , wherein:
the ribs are convex protruding outside from the tank at tip ends of the V-shaped cross-sections; and
the deformation allowable portion is connected to the ends of the ribs in a curve.
8. The heat exchanger according to claim 2 , wherein:
the ribs are disposed between the tube inserting holes adjacent to each other in the tube stacking direction.
9. The heat exchanger according to claim 2 , wherein:
the tank includes a core plate made of metal, and a tank portion made of resin for forming a tank space together with the core plate; and
the core plate includes the tube joint part joined to the tube, and a tank joint part joined to the tank portion.
10. The heat exchanger according to claim 2 , wherein:
the tubes are fixed to the tube inserting holes by blazing.
11. The heat exchanger according to claim 2 , wherein:
the tube inserting hole is provided to have a burring portion in its periphery.
12. The heat exchanger according to claim 2 , wherein:
the ribs are convex protruding outside from the tank at tip ends of the V-shaped cross-sections;
the tube joint part has a deformation allowable portion outside of the ends of the ribs; and
the deformation allowable portion is connected to the ends of the ribs in a curve.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2005-105815 | 2005-04-01 | ||
JP2005105815A JP2006284107A (en) | 2005-04-01 | 2005-04-01 | Heat exchanger |
Publications (1)
Publication Number | Publication Date |
---|---|
US20070012425A1 true US20070012425A1 (en) | 2007-01-18 |
Family
ID=37406221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/524,422 Abandoned US20070012425A1 (en) | 2005-04-01 | 2006-09-20 | Heat exchanger |
Country Status (2)
Country | Link |
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US (1) | US20070012425A1 (en) |
JP (1) | JP2006284107A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2009088516A1 (en) * | 2008-01-10 | 2009-07-16 | Modine Manufacturing Company | Heat exchanger |
US8074708B2 (en) | 2006-06-29 | 2011-12-13 | Denso Corporation | Heat exchanger |
US20130160973A1 (en) * | 2010-03-31 | 2013-06-27 | Valeo Systemes Thermiques | Heat exchanger having enhanced performance |
US20160091263A1 (en) * | 2014-09-26 | 2016-03-31 | Noritz Corporation | Header of heat exchanger and heat exchanger provided with the same |
US20170010058A1 (en) * | 2015-07-07 | 2017-01-12 | Mahle International Gmbh | Tube header for heat exchanger |
US10508865B2 (en) | 2015-12-10 | 2019-12-17 | Denso Corporation | Heat exchanger |
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JP5082387B2 (en) * | 2006-11-02 | 2012-11-28 | 株式会社デンソー | Heat exchanger |
KR101497364B1 (en) * | 2012-08-07 | 2015-03-02 | 한라비스테온공조 주식회사 | A heat exchanger |
JP6394202B2 (en) * | 2013-11-27 | 2018-09-26 | 株式会社デンソー | Heat exchanger |
JP2015206507A (en) * | 2014-04-18 | 2015-11-19 | 株式会社デンソー | heat exchanger |
JP6919472B2 (en) * | 2017-09-29 | 2021-08-18 | 株式会社デンソー | Heat exchanger |
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Also Published As
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JP2006284107A (en) | 2006-10-19 |
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