US20060157233A1 - Heat exchanger - Google Patents
Heat exchanger Download PDFInfo
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- US20060157233A1 US20060157233A1 US11/331,439 US33143906A US2006157233A1 US 20060157233 A1 US20060157233 A1 US 20060157233A1 US 33143906 A US33143906 A US 33143906A US 2006157233 A1 US2006157233 A1 US 2006157233A1
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- 238000000034 method Methods 0.000 claims 8
- 238000004590 computer program Methods 0.000 claims 3
- 230000005540 biological transmission Effects 0.000 claims 1
- 238000001816 cooling Methods 0.000 abstract description 15
- 239000012530 fluid Substances 0.000 description 15
- 239000000498 cooling water Substances 0.000 description 12
- 238000011144 upstream manufacturing Methods 0.000 description 6
- 238000004904 shortening Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 239000002699 waste material Substances 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 101700004678 SLIT3 Proteins 0.000 description 1
- 102100027339 Slit homolog 3 protein Human genes 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
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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
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
- F28F1/126—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element consisting of zig-zag shaped fins
- F28F1/128—Fins with openings, e.g. louvered fins
Definitions
- the present invention relates to a heat exchanger which is effective when applied to a radiator etc. for heat exchange between cooling water and air of an internal combustion engine.
- the fins in a conventional heat exchanger have louvers.
- the edge effect of the louvers enables the heat conductivity of the fins to be improved.
- the flow of the cooling air is changed to guide the cooling air to the louver passages between the adjoining louvers and thereby improve the heat conductivity of the fins (for example, see Japanese Patent Publication (A) No. 2003-83690).
- the present invention in consideration of the above points, has as its object the improvement of the heat conductivity of the fins without shortening the louver pitch.
- a heat exchanger provided with a plurality of tubes through the inside of which an inside fluid is circulated and arranged stacked over each other and fins arranged between the tubes and having flat parts substantially parallel to the direction of circulation of the outside fluid flowing between the tubes, a plurality of louvers twisted by a predetermined angle with respect to the flat parts being provided at the flat parts along the direction of circulation of the outside fluid and louver passages being formed between the adjoining louver, characterized in that when the direction along a predetermined angle is made the louver width direction, a step difference projecting out to the louver passage side is provided at an intermediate part of each louver in the louver width direction.
- the step difference is provided at the louver passage side positioned at the upstream side in the direction of circulation of the outside fluid in the louver passages positioned at the two sides of the louvers.
- the flow of the outside fluid is strongly disrupted, so the heat conductivity of the fins can be further improved.
- a heat exchanger provided with a plurality of tubes through the inside of which an inside fluid is circulated and arranged stacked over each other and fins arranged between the tubes and having flat parts substantially parallel to the direction of circulation of the outside fluid flowing between the tubes, a plurality of louvers twisted by a predetermined angle with respect to the flat parts being provided at the flat parts along the direction of circulation of the outside fluid and louver passages being formed between the adjoining louver, characterized in that when the direction along a predetermined angle is made the louver width direction, a communicating passage for communicating the louver passages positioned at the two sides of each louver is provided at an intermediate part of the louver in the louver width direction.
- the communicating passages are long slits extending in the stacking direction of the tubes formed by making cuts along the stacking direction of the tubes, then deforming the two sides of the cuts.
- the heat exchanger may use fins formed to corrugated shapes so as to have a plurality of flat parts arranged along the direction of circulation of the inside fluid and curved parts connecting the adjoining flat parts.
- FIG. 1 ( a ) is a front view of a heat exchanger according to a first embodiment of the present invention
- FIG. 1 ( b ) is an enlarged view of part A of FIG. 1 ( a ).
- FIG. 2 ( a ) is a partially cutaway perspective view of the fins 3 of FIG. 1
- FIG. 2 ( b ) is an enlarged view of part B of FIG. 2 ( a ).
- FIG. 3 ( a ) is a sectional view of the fins 3 of FIG. 1 seen from the tube stacking direction X 3
- FIG. 3 ( b ) is an enlarged view of part C of FIG. 3 ( a ).
- FIG. 4 ( a ) is a graph showing the local heat conductivity and average heat conductivity of fins 3 in a heat exchanger according to a first embodiment
- FIG. 4 ( b ) is a graph showing the local heat conductivity and average heat conductivity of fins 3 in a conventional heat exchanger.
- FIG. 5 gives sectional views of principal parts showing modifications of the fins 3 in the heat exchanger according to the first embodiment.
- FIG. 6 is a perspective view of fins 3 in a heat exchange according to a second embodiment of the present invention.
- FIG. 7 is a perspective view of fins 3 in a heat exchange according to a third embodiment of the present invention.
- FIG. 8 ( a ) is a partially cutaway perspective view of fins 3 in a heat exchange according to a fourth embodiment of the present invention, while FIG. 8 ( b ) is an enlarged view of a part D of FIG. 8 ( a ).
- FIG. 9 ( a ) is a sectional view of the fins 3 of FIG. 8 as seen from the tube stacking direction X 3
- FIG. 9 ( b ) is an enlarged view of a part E of FIG. 9 ( a ).
- FIG. 1 ( a ) is a front view of the radiator 1
- FIG. 1 ( b ) is an enlarged view of part A of FIG. 1 ( a )
- FIG. 2 ( a ) is a partially cutaway perspective view of the fins 3 of FIG. 1
- FIG. 2 ( b ) is an enlarged view of part B of FIG. 2 ( a )
- FIG. 3 ( a ) is a sectional view of the fins 3 of FIG. 1 seen from the tube stacking direction X 3
- FIG. 3 ( b ) is an enlarged view of part C of FIG. 3 ( a ).
- the radiator 1 has tubes 2 through the inside of which engine cooling water flows, corrugated-shaped fins 3 bonded to the outside surfaces of the tubes 2 , header tanks 4 provided at the ends of the tubes 2 in the direction of circulation X 1 of the cooling water (hereinafter referred to as the “cooling water circulation direction X 1 ”) and communicating with the tubes 2 , etc.
- the engine cooling water corresponds to the inside fluid of the present invention.
- the tubes 2 are made of metal (in the present embodiment, aluminum alloy). Cooling water passages through which the cooling water flows are formed inside them and are formed as flat shapes. Further, a plurality of the tubes 2 are stacked over each other. The fins 3 are arranged between the adjoining tubes 2 . Cooling air is designed to be able to flow between the adjoining tubes 2 . Note that the cooling air corresponds to the outside fluid of the present invention.
- the fins 3 promote the heat exchange between the cooling air and the cooling water and are comprised of a metal (in the present embodiment, aluminum alloy) and produced by press forming or rolling.
- These fins 3 have flat parts 3 a having surfaces substantially parallel with the direction of circulation X 2 of the cooling air flowing between the tubes 2 (hereinafter referred to as the “air flow direction X 2 ”) and curved parts 3 b connecting the adjoining flat parts 3 a and are formed to corrugated shapes seen from the air flow direction X 2 .
- a plurality of these flat parts 3 a are arranged along the cooling water circulation direction X 1 .
- the flat parts 3 a are formed integrally with louvers 3 c by cutting and raising the flat parts 3 a.
- the louvers 3 c when seen from the stacking direction X 3 of the tubes 3 (hereinafter referred to as the “tube stacking direction X 3 ”), are twisted from the flat parts 3 a by a predetermined angle ⁇ 1 (hereinafter referred to as the “twist angle ⁇ 1”).
- a plurality are provided at the flat parts 3 a along the air flow direction X 2 .
- louver passages 5 are formed between the adjoining louvers 3 c.
- twist direction of the louvers 3 c positioned at the upstream side in the air flow direction X 2 and the twist direction of the louvers 3 c positioned at the downstream side in the air flow direction X 2 differ.
- the twist angle ⁇ 1 is, in the present embodiment, made 23°.
- each louver 3 c in louver width direction X 4 is provided with a step difference 3 d extending in the tube stacking direction X 3 and projecting out to the louver passage 5 side.
- One step difference 3 d is provided at each louver 3 c.
- the step difference 3 d is provided at the louver passage 5 side positioned upstream in the air flow direction X 2 among the louver passages 5 positioned at the two sides of each louver 3 c. Further, the bending angle ⁇ 2 when viewing the step difference 3 d from the tube stacking direction X 3 is, in the present embodiment, made 90°.
- the fins 3 are made of aluminum alloy, the thickness t of the fins 3 is 0.05 mm, the length L of the louvers 3 c in the louver width direction X 4 (hereinafter referred to as the “louver width L”) is 0.8 mm, and the amount of projection S of the step differences 3 d is made 0.05 mm.
- the amount of projection S of the step differences 3 d is preferably at least the thickness t of the fins 3 . Further, when the length of one period of the fins 3 formed in the corrugated shape is the fin pitch FP and the dimension of the cooling water circulation direction X 1 in the louvers 3 c is the louver pitch height HLP, it is preferable that FP/HLP be 10 or less.
- FIG. 4 ( a ) shows the change in the local heat conductivity of the fins 3 according to the present embodiment
- FIG. 4 ( b ) shows the change in the local heat conductivity of the fins having configurations similar to that described in Patent Publication 1.
- the radiator 1 of the present embodiment has step differences 3 d projecting out to the louver passage 5 sides.
- step differences 3 d projecting out to the louver passage 5 sides.
- step differences 3 d are provided at the louver passage 5 side positioned at the upstream side in the air flow direction X 2 , compared even with the case of providing the step differences 3 d at the louver passage 5 side positioned at the downstream side of the air flow direction X 2 , the flow of the cooling air is strongly disrupted. Therefore, the heat conductivity of the fins 3 can be further improved.
- FIG. 5 shows modifications of the fins 3 of the present embodiment and gives views of the step differences 3 d seen from the tube stacking direction X 3 .
- FIG. 5 ( a ) shows a step difference 3 d with a blunted bending angle ⁇ 2.
- FIG. 5 ( b ) shows a step difference 3 d with a louver width L 1 at one end and a louver width L 2 at the other end made different.
- FIG. 5 ( c ) shows a plurality of step differences 3 d provided at a louver 3 c .
- FIG. 6 is a perspective view of fins 3 in a heat exchanger according to a second embodiment.
- the present embodiment is provided with, in place of the step differences 3 d in the first embodiment, holes 3 e in the louvers 3 c .
- the other points are common with the first embodiment.
- the holes 3 e pass through the louvers 3 c so as to communicate the louver passages 5 positioned at the two sides. Further, the holes 3 e are oval in shape. A plurality are provided at the intermediate parts of the louvers 3 c in the louver width direction X 4 and at the louvers 3 c along the tube stacking direction X 3 (in this example, three). Note that the holes 3 e correspond to the communicating passages of the present invention.
- FIG. 7 is a perspective view of fins 3 in a heat exchanger according to the third embodiment.
- the holes 3 e were formed by punching, but in the present embodiment, the holes 3 e are formed by cutting and raising up parts of the louvers 3 c . Due to this, it is possible to form holes 3 e without generating waste material. Note that the 3 f is a piece which is cut and raised up.
- FIG. 8 ( a ) is a partially cutaway perspective view of the fins 3 in a heat exchanger according to the fourth embodiment
- FIG. 8 ( b ) is an enlarged view of the part D of FIG. 8 ( a )
- FIG. 9 ( a ) is a sectional view of the fins 3 of FIG. 8 seen along the tube stacking direction X 3
- FIG. 9 ( b ) is an enlarged view of the part E of FIG. 9 ( a ).
- each louver 3 c was provided with a plurality of holes 3 e to communicate the louver passages 5 positioned at the two sides of the louver 3 c , but the present embodiment each louver 3 c is provided with one long slit 3 g extending in the tube stacking direction X 3 so as to communicate the louver passages 5 positioned at the two sides of the louver 3 c .
- the slits 3 g correspond to the communicating passages of the present invention.
- the slits 3 g are formed as follows: That is, a cut is made in the intermediate part of each louver 3 c in the louver width direction X 4 along the tube stacking direction X 3 , then the two sides of the cut are deformed. Due to this, it is possible to form the slits 3 g without generating any waste material.
- the twist direction of the louvers 3 c positioned at the upstream side in the air flow direction X 2 and the twist direction of the louvers 3 c positioned at the downstream side in the air flow direction X 2 were made different, but it is also possible to make the twist directions of all of the louvers 3 the same.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
A heat exchanger with louvers twisted by a predetermined angle with respect to flat parts of fins and with louver passages formed between adjoining louvers, wherein step differences projecting out to the louver passage side are provided at the louvers. According to this, when cooling air flows through the louver passages, the flow of the cooling air is disrupted by the step differences and temperature boundary layers are destroyed, so the local heat conductivity is again raised at the locations of the step differences.
Description
- The present invention relates to a heat exchanger which is effective when applied to a radiator etc. for heat exchange between cooling water and air of an internal combustion engine.
- The fins in a conventional heat exchanger have louvers. The edge effect of the louvers enables the heat conductivity of the fins to be improved. Further, by tilting the louvers with respect to the flat parts by a predetermined angle, the flow of the cooling air is changed to guide the cooling air to the louver passages between the adjoining louvers and thereby improve the heat conductivity of the fins (for example, see Japanese Patent Publication (A) No. 2003-83690).
- However, in the above conventional heat exchanger, if the louver pitch is shortened to further improve the performance, there was the problem that the cooling air ended up no longer being guided to the louver passages, the edge effect was not improved, and as a result the heat conductivity of the fins could not be improved.
- The present invention, in consideration of the above points, has as its object the improvement of the heat conductivity of the fins without shortening the louver pitch.
- To achieve the above object, in the present invention, there is provided a heat exchanger provided with a plurality of tubes through the inside of which an inside fluid is circulated and arranged stacked over each other and fins arranged between the tubes and having flat parts substantially parallel to the direction of circulation of the outside fluid flowing between the tubes, a plurality of louvers twisted by a predetermined angle with respect to the flat parts being provided at the flat parts along the direction of circulation of the outside fluid and louver passages being formed between the adjoining louver, characterized in that when the direction along a predetermined angle is made the louver width direction, a step difference projecting out to the louver passage side is provided at an intermediate part of each louver in the louver width direction.
- According to this, when the outside fluid flows through the louver passages, the flow of the outside fluid is disrupted by the step difference and the temperature boundary layer is destroyed, so at the location of the step differences, the local heat conductivity is again improved. Therefore, it is possible to improve the heat conductivity of the fins without shortening the louver pitch.
- Further, in the present invention, the step difference is provided at the louver passage side positioned at the upstream side in the direction of circulation of the outside fluid in the louver passages positioned at the two sides of the louvers.
- According to this, the flow of the outside fluid is strongly disrupted, so the heat conductivity of the fins can be further improved.
- Further, in the present invention, there is provided a heat exchanger provided with a plurality of tubes through the inside of which an inside fluid is circulated and arranged stacked over each other and fins arranged between the tubes and having flat parts substantially parallel to the direction of circulation of the outside fluid flowing between the tubes, a plurality of louvers twisted by a predetermined angle with respect to the flat parts being provided at the flat parts along the direction of circulation of the outside fluid and louver passages being formed between the adjoining louver, characterized in that when the direction along a predetermined angle is made the louver width direction, a communicating passage for communicating the louver passages positioned at the two sides of each louver is provided at an intermediate part of the louver in the louver width direction.
- According to this, when the outside fluid flows through the louver passages, the outside fluid passes through the communicating passages whereby the development of temperature boundary layers is suppressed. Therefore, it is possible to improve the heat conductivity of the fins without shortening the louver pitch.
- Further, in the present invention, the communicating passages are long slits extending in the stacking direction of the tubes formed by making cuts along the stacking direction of the tubes, then deforming the two sides of the cuts.
- According to this, it is possible to form communicating passages without generating waste material.
- Further, in the present invention, the heat exchanger may use fins formed to corrugated shapes so as to have a plurality of flat parts arranged along the direction of circulation of the inside fluid and curved parts connecting the adjoining flat parts.
- Below, the present invention will be able to be more sufficiently understood from the attached drawings and the preferred embodiments of the present invention.
-
FIG. 1 (a) is a front view of a heat exchanger according to a first embodiment of the present invention, whileFIG. 1 (b) is an enlarged view of part A ofFIG. 1 (a). -
FIG. 2 (a) is a partially cutaway perspective view of thefins 3 ofFIG. 1 , whileFIG. 2 (b) is an enlarged view of part B ofFIG. 2 (a). -
FIG. 3 (a) is a sectional view of thefins 3 ofFIG. 1 seen from the tube stacking direction X3, while FIG. 3(b) is an enlarged view of part C ofFIG. 3 (a). -
FIG. 4 (a) is a graph showing the local heat conductivity and average heat conductivity offins 3 in a heat exchanger according to a first embodiment, whileFIG. 4 (b) is a graph showing the local heat conductivity and average heat conductivity offins 3 in a conventional heat exchanger. -
FIG. 5 gives sectional views of principal parts showing modifications of thefins 3 in the heat exchanger according to the first embodiment. -
FIG. 6 is a perspective view offins 3 in a heat exchange according to a second embodiment of the present invention. -
FIG. 7 is a perspective view offins 3 in a heat exchange according to a third embodiment of the present invention. -
FIG. 8 (a) is a partially cutaway perspective view offins 3 in a heat exchange according to a fourth embodiment of the present invention, whileFIG. 8 (b) is an enlarged view of a part D ofFIG. 8 (a). -
FIG. 9 (a) is a sectional view of thefins 3 ofFIG. 8 as seen from the tube stacking direction X3, whileFIG. 9 (b) is an enlarged view of a part E ofFIG. 9 (a). - The present embodiment applies the heat exchanger according to the present invention to a radiator 1 for heat exchange between cooling water of a running engine (internal combustion engine) and air so as to cool the cooling water.
FIG. 1 (a) is a front view of the radiator 1,FIG. 1 (b) is an enlarged view of part A ofFIG. 1 (a),FIG. 2 (a) is a partially cutaway perspective view of thefins 3 ofFIG. 1 ,FIG. 2 (b) is an enlarged view of part B ofFIG. 2 (a),FIG. 3 (a) is a sectional view of thefins 3 ofFIG. 1 seen from the tube stacking direction X3, andFIG. 3 (b) is an enlarged view of part C ofFIG. 3 (a). - As shown in
FIG. 1 , the radiator 1 hastubes 2 through the inside of which engine cooling water flows, corrugated-shaped fins 3 bonded to the outside surfaces of thetubes 2,header tanks 4 provided at the ends of thetubes 2 in the direction of circulation X1 of the cooling water (hereinafter referred to as the “cooling water circulation direction X1”) and communicating with thetubes 2, etc. Note that the engine cooling water corresponds to the inside fluid of the present invention. - The
tubes 2 are made of metal (in the present embodiment, aluminum alloy). Cooling water passages through which the cooling water flows are formed inside them and are formed as flat shapes. Further, a plurality of thetubes 2 are stacked over each other. Thefins 3 are arranged between theadjoining tubes 2. Cooling air is designed to be able to flow between the adjoiningtubes 2. Note that the cooling air corresponds to the outside fluid of the present invention. - The
fins 3 promote the heat exchange between the cooling air and the cooling water and are comprised of a metal (in the present embodiment, aluminum alloy) and produced by press forming or rolling. - These
fins 3, as shown inFIG. 2 andFIG. 3 , haveflat parts 3 a having surfaces substantially parallel with the direction of circulation X2 of the cooling air flowing between the tubes 2 (hereinafter referred to as the “air flow direction X2”) andcurved parts 3 b connecting the adjoiningflat parts 3 a and are formed to corrugated shapes seen from the air flow direction X2. A plurality of theseflat parts 3 a are arranged along the cooling water circulation direction X1. - Further, the
flat parts 3 a are formed integrally withlouvers 3 c by cutting and raising theflat parts 3 a. Thelouvers 3 c, when seen from the stacking direction X3 of the tubes 3 (hereinafter referred to as the “tube stacking direction X3”), are twisted from theflat parts 3 a by a predetermined angle θ1 (hereinafter referred to as the “twist angle θ1”). A plurality are provided at theflat parts 3 a along the air flow direction X2. Further,louver passages 5 are formed between theadjoining louvers 3 c. The twist direction of thelouvers 3 c positioned at the upstream side in the air flow direction X2 and the twist direction of thelouvers 3 c positioned at the downstream side in the air flow direction X2 differ. Note that the twist angle θ1 is, in the present embodiment, made 23°. - Here, when the direction along the angle θ1 is made the louver width direction X4, the intermediate part of each
louver 3 c in louver width direction X4 is provided with astep difference 3 d extending in the tube stacking direction X3 and projecting out to thelouver passage 5 side. - One
step difference 3 d is provided at eachlouver 3 c. Thestep difference 3 d is provided at thelouver passage 5 side positioned upstream in the air flow direction X2 among thelouver passages 5 positioned at the two sides of eachlouver 3 c. Further, the bending angle θ2 when viewing thestep difference 3 d from the tube stacking direction X3 is, in the present embodiment, made 90°. - Note that in the present embodiment, the
fins 3 are made of aluminum alloy, the thickness t of thefins 3 is 0.05 mm, the length L of thelouvers 3 c in the louver width direction X4 (hereinafter referred to as the “louver width L”) is 0.8 mm, and the amount of projection S of thestep differences 3 d is made 0.05 mm. - Further, the amount of projection S of the
step differences 3 d is preferably at least the thickness t of thefins 3. Further, when the length of one period of thefins 3 formed in the corrugated shape is the fin pitch FP and the dimension of the cooling water circulation direction X1 in thelouvers 3 c is the louver pitch height HLP, it is preferable that FP/HLP be 10 or less. - Next, the actions and effects of the present embodiment will be explained.
-
FIG. 4 (a) shows the change in the local heat conductivity of thefins 3 according to the present embodiment, whileFIG. 4 (b) shows the change in the local heat conductivity of the fins having configurations similar to that described in Patent Publication 1. - As shown in
FIG. 4 (a), the upstream ends of thelouvers 3 c in the air flow direction X2 become higher in local heat conductivity due to the edge effect. Next, when the cooling air flows through thelouver passages 5, the temperature boundary layers develop and the local heat conductivity gradually falls. - However, the radiator 1 of the present embodiment has
step differences 3 d projecting out to thelouver passage 5 sides. By the cooling air striking thesestep differences 3 d, the flow of the cooling air is disrupted by thestep differences 3 d and the temperature boundary layers are destroyed, so at the locations of thestep differences 3 d, the local heat conductivity again rises and the average heat conductivity is improved. Therefore, it is possible to improve the heat conductivity of thefins 3 without shortening the louver pitch. - Further, since the
step differences 3 d are provided at thelouver passage 5 side positioned at the upstream side in the air flow direction X2, compared even with the case of providing thestep differences 3 d at thelouver passage 5 side positioned at the downstream side of the air flow direction X2, the flow of the cooling air is strongly disrupted. Therefore, the heat conductivity of thefins 3 can be further improved. - Note that
FIG. 5 shows modifications of thefins 3 of the present embodiment and gives views of thestep differences 3 d seen from the tube stacking direction X3. -
FIG. 5 (a) shows astep difference 3 d with a blunted bending angle θ2.FIG. 5 (b) shows astep difference 3 d with a louver width L1 at one end and a louver width L2 at the other end made different.FIG. 5 (c) shows a plurality ofstep differences 3 d provided at alouver 3 c . - A second embodiment of the present invention will be explained next.
FIG. 6 is a perspective view offins 3 in a heat exchanger according to a second embodiment. - The present embodiment is provided with, in place of the
step differences 3 d in the first embodiment, holes 3 e in thelouvers 3 c. The other points are common with the first embodiment. - The
holes 3 e pass through thelouvers 3 c so as to communicate thelouver passages 5 positioned at the two sides. Further, theholes 3 e are oval in shape. A plurality are provided at the intermediate parts of thelouvers 3 c in the louver width direction X4 and at thelouvers 3 c along the tube stacking direction X3 (in this example, three). Note that theholes 3 e correspond to the communicating passages of the present invention. - According to this, when the cooling air flows through the
louver passages 5, part of the cooling air passes through theholes 3 e and flow to the adjoininglouver passages 5, whereby the development of temperature boundary layers is suppressed and therefore the average heat conductivity is improved. Therefore, it is possible to improve the heat conductivity of thefins 3 without shortening the louver pitch. - A third embodiment of the present invention will be explained next.
FIG. 7 is a perspective view offins 3 in a heat exchanger according to the third embodiment. - In the second embodiment, the
holes 3 e were formed by punching, but in the present embodiment, theholes 3 e are formed by cutting and raising up parts of thelouvers 3 c. Due to this, it is possible to formholes 3 e without generating waste material. Note that the 3 f is a piece which is cut and raised up. - A fourth embodiment of the present invention will be explained next.
FIG. 8 (a) is a partially cutaway perspective view of thefins 3 in a heat exchanger according to the fourth embodiment,FIG. 8 (b) is an enlarged view of the part D ofFIG. 8 (a),FIG. 9 (a) is a sectional view of thefins 3 ofFIG. 8 seen along the tube stacking direction X3, andFIG. 9 (b) is an enlarged view of the part E ofFIG. 9 (a). - In the second embodiment, each
louver 3 c was provided with a plurality ofholes 3 e to communicate thelouver passages 5 positioned at the two sides of thelouver 3 c, but the present embodiment eachlouver 3 c is provided with onelong slit 3 g extending in the tube stacking direction X3 so as to communicate thelouver passages 5 positioned at the two sides of thelouver 3 c. Note that theslits 3 g correspond to the communicating passages of the present invention. - The
slits 3 g are formed as follows: That is, a cut is made in the intermediate part of eachlouver 3 c in the louver width direction X4 along the tube stacking direction X3, then the two sides of the cut are deformed. Due to this, it is possible to form theslits 3 g without generating any waste material. - In the above embodiments, the twist direction of the
louvers 3 c positioned at the upstream side in the air flow direction X2 and the twist direction of thelouvers 3 c positioned at the downstream side in the air flow direction X2 were made different, but it is also possible to make the twist directions of all of thelouvers 3 the same. - Note that the present invention was explained in detail based on specific embodiments, but a person skilled in the art could make various changes, modifications, etc. without departing from the claims and idea of the present invention.
Claims (20)
1. A computer-implemented method for communication within a network, said method comprising the steps of:
transmitting a data packet as a broadcast signal from a first application node of a first subnetwork to a first gateway node of the first subnetwork;
transmitting the data packet as a point-to-point signal from the first gateway node to a second gateway node of a second subnetwork;
transmitting the data packet as a broadcast signal from the second gateway node of the second subnetwork to at least one application node of the second subnetwork; and
simulating war games between two remote geographic sites.
2. The computer-implemented method as set forth in claim 1 further comprising the steps of:
transmitting another data packet as a broadcast signal from the at least one application node of the second subnetwork to the second gateway node of the second subnetwork;
transmitting the other data packet as a point-to-point signal from the second gateway node to the first gateway node of the first subnetwork; and
transmitting the data packet as a broadcast signal from the first gateway node of the first subnetwork to the first application node of the first subnetwork.
3. The computer-implemented method as set forth in claim 1 wherein said transmitting the data packet as a point-to-point signal is conducted across an undedicated communication network.
4. The computer-implemented method as set forth in claim 3 wherein the undedicated communication network is the Internet.
5. (canceled)
6. The computer-implemented method as set forth in claim 1 wherein the broadcast signals each comprise an Ethernet Protocol Data Unit.
7. The computer-implemented method as set forth in claim 1 wherein the point-to-point signal includes an IP address.
8. The computer-implemented method as set forth in claim 1 further including the step of transmitting the data packet as a broadcast signal to a second application node of the first subnetwork.
9. A system comprising:
a first device for transmitting a data packet as a broadcast signal from a first application node of a first subnetwork to a first gateway node of the first subnetwork;
a second device for transmitting the data packet as a point-to-point signal from the first gateway node to a second gateway node of a second subnetwork; and
a third device for transmitting the data packet as a broadcast signal from the second gateway node of the second subnetwork to at least one application node of the second subnetwork,
the broadcast signals each comprising an Ethernet Protocol Data Unit.
10. The system as set forth in claim 9 wherein said third device transmits another data packet as a broadcast signal from the at least one application node of the second subnetwork to the second gateway node of the second subnetwork; said second device transmits the. other data packet as a point-to-point signal from the second gateway node to the first gateway node of the first subnetwork; and said third device transmits the data packet as a broadcast signal from the first gateway node of the first subnetwork to the first application node of the first subnetwork.
11. The system as set forth in claim 9 wherein said first device is a computer.
12. The system as set forth in claim 11 wherein the first gateway node converts the data packet from the broadcast signal to the point-to-point signal by adding an IP address to the broadcast signal.
13. The system as set forth in claim 9 wherein said third means is a computer.
14. The system as set forth in claim 9 wherein said second means is an undedicated intranet.
15. The system as set forth in claim 9 wherein said first device transmits the data packet as a broadcast signal form the first application node to a second application node of the first subnetwork.
16. An apparatus for simulating a war game, said apparatus comprising:
a first means for transmitting a data packet as a broadcast signal from a first application node of a first subnetwork to a first gateway node of the first subnetwork;
a second means for transmitting the data packet as .a point-to-point signal from the first gateway node to a second gateway node of a second subnetwork; and
a third means for transmitting the data packet as a broadcast signal from the second gateway node of the second subnetwork to at least one application node of the second subnetwork,
said first, second, and third transmitting means simulating the war game between two remote geographic sites.
17. The apparatus as set forth in claim 16 wherein said third means transmits another data packet as a broadcast signal from the at least one application node of the second subnetwork to the second gateway node of the second subnetwork; said second means transmits the other data packet as a point-to-point signal from the second gateway node to the first gateway node of the first subnetwork; and said third means transmits the data packet as a broadcast signal from the first gateway node of the first subnetwork to the first application node of the first subnetwork.
18. A computer program product containing executable instructions for communicating within a network, said product comprising:
a first subnetwork having a first application node and a first gateway node; and
a second subnetwork having a second application node and a second gateway node,
said first application node transmitting a data packet as a broadcast signal to said first gateway node of said first subnetwork;
said first gateway node transmitting said data packet as a point-to-point signal from said first gateway node to said second gateway node of said second subnetwork,
said second gateway node transmitting said data packet as a broadcast signal from said second gateway node of said second subnetwork to said second application node of said second subnetwork,
the broadcast signals each comprising an Ethernet Protocol Data Unit.
19. The computer program product as set forth in claim 18 wherein said second application node transmits another data packet as a broadcast,signal to said second gateway node, said second gateway node transmits said other data packet as a point-to-point signal to said first gateway node, and said first gateway node transmits said other data packet as a broadcast signal to said first and second application nodes.
20. The computer program product as set forth in claim 18 wherein said first application node transmits said data packet as a broadcast signal to another application node of said first subnetwork simultaneously to the transmission of said data packet to said first gateway node.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2005011466A JP2006200788A (en) | 2005-01-19 | 2005-01-19 | Heat exchanger |
| JP2005-011466 | 2005-01-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20060157233A1 true US20060157233A1 (en) | 2006-07-20 |
Family
ID=36682686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/331,439 Abandoned US20060157233A1 (en) | 2005-01-19 | 2006-01-12 | Heat exchanger |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20060157233A1 (en) |
| JP (1) | JP2006200788A (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070137840A1 (en) * | 2005-12-16 | 2007-06-21 | Denso Corporation | Corrugated fin and heat exchanger using the same |
| US20070246202A1 (en) * | 2006-04-25 | 2007-10-25 | Yu Wen F | Louvered fin for heat exchanger |
| EP2068106A1 (en) | 2007-12-04 | 2009-06-10 | Valeo Systèmes Thermiques | Corrugated fin with louvers for a heat exchanger |
| US20100123877A1 (en) * | 2008-11-20 | 2010-05-20 | Fujibayashi Hiroko | Projection display apparatus |
| US20110108260A1 (en) * | 2008-08-15 | 2011-05-12 | Alahyari Abbas A | Heat exchanger fin including louvers |
| US20130199760A1 (en) * | 2008-08-06 | 2013-08-08 | Delphi Technologies, Inc. | Heat exchanger assembly having split mini-louvered fins |
| DE102015205902A1 (en) | 2015-04-01 | 2016-10-06 | Mahle International Gmbh | Rib for a heat exchanger |
| US20170198984A1 (en) * | 2014-07-18 | 2017-07-13 | Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. | Fin for heat exchanger and heat exchanger having fin |
| EP3255369A1 (en) * | 2016-06-08 | 2017-12-13 | Mahle International GmbH | Fin element for a heat transferer |
| US10436156B2 (en) * | 2016-12-01 | 2019-10-08 | Modine Manufacturing Company | Air fin for a heat exchanger, and method of making the same |
| CN111912279A (en) * | 2020-08-13 | 2020-11-10 | 西安交通大学 | A twisted and zigzag shutter fin |
| EP4023994A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
| EP4023995A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
| EP4023996A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
| USD967361S1 (en) * | 2020-08-17 | 2022-10-18 | Mercracing, Llc | Heat exchanger |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| KR101100114B1 (en) * | 2009-11-27 | 2011-12-29 | 한국델파이주식회사 | Fin for heat exchanger |
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| US20070137840A1 (en) * | 2005-12-16 | 2007-06-21 | Denso Corporation | Corrugated fin and heat exchanger using the same |
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| EP2778592A1 (en) * | 2013-03-15 | 2014-09-17 | Delphi Technologies, Inc. | Heat exchanger assembly having split mini-louvered fins |
| US20170198984A1 (en) * | 2014-07-18 | 2017-07-13 | Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. | Fin for heat exchanger and heat exchanger having fin |
| US10082343B2 (en) * | 2014-07-18 | 2018-09-25 | Danfoss Micro Channel Heat Exchanger (Jiaxing) Co., Ltd. | Fin for heat exchanger and heat exchanger having fin |
| DE102015205902A1 (en) | 2015-04-01 | 2016-10-06 | Mahle International Gmbh | Rib for a heat exchanger |
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| US10436156B2 (en) * | 2016-12-01 | 2019-10-08 | Modine Manufacturing Company | Air fin for a heat exchanger, and method of making the same |
| US11162742B2 (en) * | 2016-12-01 | 2021-11-02 | Modine Manufacturing Company | Air fin for a heat exchanger |
| CN111912279A (en) * | 2020-08-13 | 2020-11-10 | 西安交通大学 | A twisted and zigzag shutter fin |
| USD967361S1 (en) * | 2020-08-17 | 2022-10-18 | Mercracing, Llc | Heat exchanger |
| EP4023994A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
| EP4023995A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
| EP4023996A1 (en) * | 2020-12-29 | 2022-07-06 | Valeo Autosystemy SP. Z.O.O. | Heat exchanger |
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|---|---|
| JP2006200788A (en) | 2006-08-03 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: DENSO CORPORATION, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:OZAKI, TATSUO;OKOCHI, TAKAKI;REEL/FRAME:017688/0247 Effective date: 20060106 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |