[0001] The present invention relates to a heat exchanger in general, and the tubes used
in a heat exchanger in particular. A heat exchanger including cooling tubes made according
to the present invention is particularly advantageous in terms of ease of construction
and manufacturing costs.
[0002] Oil-to-air coolers are widely used in motor vehicle applications to cool engine oil,
transmission oil, power steering oil and hydraulic fluids. The cooler usually consists
of bundles of tubes, fins and two manifolds. The oil flows inside the tubes while
outside air passes through the fins. Due to the high viscosity of the oil, internal
turbulators are often disposed within oil-cooling tubes to improve heat transfer.
The turbulators are typically bonded to the internal walls of the oil-cooling tubes
to allow heat flow from the turbulators to the tube walls.
[0003] The addition of turbulators to oil-cooling tubes, however, increases the cost and'
complexity of the heat exchanger manufacturing process. Bonding turbulators with oil-cooling
tubes adds a step to the process. In addition, if the turbulator-to-tube bond is not
properly formed, the cooling capacity of the oil coolers will be diminished. Consequently,
it is desirable to eliminate and/or simplify the construction of oil-cooling tubes,
yet still have such tubes transfer heat at the same or an improved rate over known
heat exchangers.
[0004] An example of a prior art approach to eliminating turbulators is set forth in
U.S. Patent No. 5,036,911, the contents of which are hereby incorporated by reference. In the approach of this
patent, an embossed plate replaces turbulators within the oil-cooling tubes. The plate
includes uniformly spaced-apart mating projections, which, when brought together during
the assembly process, create additional surface area to enhance the transfer of heat
from the oil during operation of the heat exchanger. Although there is no turbulator
component, the plate sizes are fixed, which makes assembly of different cooler sizes
difficult. Also, there is a risk of two plates not properly bonding together, which
could result in leaks and loss of heat transfer.
[0005] A need therefore exists for a more high-performance leak proof oil-coolers that do
not include turbulators as a separate assembly. In addition, a need exists for a cost
effective and automated means to manufacture such oil-coolers. The invention is generally
directed to a heat exchanger for a motor vehicle, such as an oil-to-air heat exchanger,
a charge air heat exchanger or an exhaust gas heat exchanger, which heat exchanger
includes internal cooling tubes formed by extruding a suitable material, such as aluminum,
steel, or stainless steel. The cooling tubes include a plurality of fluid paths, which
are also extruded as part of the tube-forming process. The transverse cross-section
of the fluid paths is typically rectangular. The walls of the fluid paths may be smooth
or, alternatively, contain flanges, ribs or teeth to improve heat transfer.
[0006] All of the fluid paths within a particular tube may be identical. As an alternative,
a tube may contain a plurality of fluid paths, certain of which differ in cross-section
from others. The one-piece extruded cooling tubes are assembled into a heat exchanger,
either with other similarly extruded tubes or with cooling tubes of a more conventional
design.
[0007] Further objects, features and advantages of the invention, will become apparent from
the detailed description of the preferred embodiments that follows, when considered
in conjunction with the attached figures of drawing.
[0008] Exemplary embodiments of the invention are given below with reference to the drawing,
in which:
FIG. 1 is a drawing that schematically illustrates a heat exchanger;
FIG. 2 is a transverse cross-sectional view of a prior art tube taken along the line
2-2 in Fig. 1;
FIG. 3 is a transverse cross-sectional view of an extruded tube according to one embodiment
of the invention;
FIG. 4 is a transverse cross-sectional view of an extruded tube according to another
embodiment of the invention;
FIG. 5 is a transverse cross-sectional view of yet another possible variant of a tube
made according to the invention;
FIG. 6 is a drawing that schematically illustrates a heat exchanger that includes
a combination of different types of cooling tubes; and
FIG. 7 is a drawing that schematically illustrates a heat exchanger that includes
two separate coolant loops.
[0009] A heat exchanger, such as that schematically illustrated in FIG. 1, typically includes
an inlet manifold
2, an outlet manifold
5, a plurality of flat cooling tubes
6a-6e disposed between the inlet and the outlet, and air-cooled fins
7 disposed between the rows of the cooling tubes. Although the type of heat exchanger
illustrated in FIG. 1 is a direct heat exchanger, i.e., air is forced or drawn across
fluid containing tubes, the invention may be used with other types of heat exchangers
known to persons of skill in the art. The invention may be applied, for example, to
indirect heat exchangers in which cooling tubes are cooled by a liquid coolant, such
as water, that is separately cooled by yet another air exchanger.
[0010] During operation of a motor vehicle, a pump forces fluid from the inlet
2 of heat exchanger
1, through the plurality of cooling tubes 6a-6e, and into the heat exchanger outlet
3. Outside air (or coolant) is forced or drawn across fins
7, which are in contact with cooling tubes
6a-6e. Heat from the fluid passing through the exchanger is transferred to the air passing
across fins
7 and, ultimately, out and away from the motor vehicle. The arrows near inlet
2 and outlet
3 illustrate the direction of fluid flow within heat exchanger
1.
[0011] FIG. 2 illustrates a transverse cross-section of a common prior art oil-cooling tube
6a taken along section
2-2 of FIG. 1. In this prior art structure, tube
6a includes a turbulator
8, which promotes heat transfer within the tube for the relatively low viscosity oil.
The turbulator is a separate component that must be properly bonded to the tube
6a. The ends of tube
6a are assembled to the inlet and outlet manifolds in a manner known to persons of skill
in the art.
[0012] The cooling tubes of one embodiment of the invention differs from the prior art as
illustrated in the transverse cross-section of FIG. 3. A flat cooling tube 10 is formed
through an extrusion process and includes a plurality of fluid-flow paths
11a-11i, which are also formed during extrusion of the tube. Each flow path typically has
a rectangular cross-section as illustrated, but persons of skill in the art will appreciate
other shapes that may be used, such as rounded or oval shapes. The separate flow paths
within each tube eliminate the need for a turbulator component, thereby resulting
in a one-piece tube that is simple to manufacture and assemble into a heat exchanger.
A one-piece tube also reduces the risk of fluid leaking from the tube due to an improper
assembly. In addition, cooling tubes formed through extrusion may be cut to an appropriate
length for a variety of sizes of heat exchangers, thereby allowing maximum flexibility
during the manufacturing and assembly processes.
[0013] Tubes, such as cooling tube 10, are assembled to the inlet and outlet manifolds of
a heat exchanger in a manner known to persons of skill in the art. For example, tube
10 may be assembled to an inlet and outlet manifold through a Nocolock controlled-atmosphere
brazing process. Tube
10 is preferably formed from metal. In highly preferred embodiments, tube
10 may be extruded from any suitable metal, such as aluminum, steel or stainless steel.
[0014] Tube
10 includes a major axis, indicated by the "H" dimension, and a minor axis, indicated
by the "W" dimension. It has been empirically determined that the preferred range
of the external cross-sectional area for an extruded one-piece oil cooler tube, which
is calculated as the product of H and W, should be between 45 and 160 mm
2 for automotive applications. If the cross-sectional area is above 160 mm
2, the heat transfer per volume of oil flow will not be sufficient. If the cross-sectional
area is below 45 mm
2, the internal oil pressure drop will be too high, which, in turn, will result in
insufficient oil flow. In addition, it has been determined that the preferred hydraulic
diameter of the tube, which is defined as four times the internal area of the tube
divided by wetted perimeter, should be between 1.2 mm to 3.5 mm.
[0015] FIG. 4 illustrates an alternative embodiment of the invention. The extruded tube
12 still includes a plurality of extruded fluid paths
13a-13e. The number of such fluid paths, however, have been reduced in comparison with the
embodiment of FIG. 3. In addition, the smooth-walled fluid paths
11a-11i of the embodiment of FIG. 3 have been replaced with fluid paths
13a-13e that have "teeth" or flanges
16 formed, by extrusion, into the side walls. The flanges
16 may be identically-patterned on all sides of the fluid path, or, as shown in FIG.
3, may include a first pattern
16 along a wall or walls and a second pattern
17 along a different wall or walls. Protrusions, such as flanges
16 and
17, into the fluid paths
13a-13e promote the additional transfer of heat.
[0016] The number of fluid paths within an extruded tube, such as fluid paths
11a-11i or
13a-13e, may be selected to obtain the desired pressure drop and/or amount of heat transfer
for a particular application. In addition, the fluid paths within a particular tube
may differ from one another. FIG. 5 illustrates an example embodiment in which different
types of fluid paths are incorporated into a single tube. Fluid path
15a includes flanges
16 and
17, whereas fluid path
15b is smooth-walled. In addition, fluid path
15c includes flanges of one type
17 along two walls, whereas fluid path
15d includes flanges of a different type 16 along a different wall.
[0017] The dimensions of the flanges, teeth or other protrusions are selected to optimize
the heat transfer characteristics of the heat exchanger. In a preferred embodiment,
such protrusions have a feature size that relates to the size of the fluid path. The
dimension of flanges
16 along the "W" axis, for example, is preferably between 10-30% of the opening of the
fluid path along the same axis.
[0018] The dimension of these same flanges along the "H" axis, as another example, is preferably
between 50-75% of the opening of the fluid path along the same axis, with individual
flanges having dimensions ranging between 6-15% of the opening. Flanges
17 will have similar general dimensions, but such dimensions will be transposed along
the "W" and "H" axes when compared with flanges
16.
[0019] The number and types of fluid paths described above and in FIGS. 3-5 may be varied
according to the desired performance characteristics of the heat exchanger. In addition,
as illustrated in FIG. 6, a heat exchanger may be assembled with different types of
tubes. A first type of cooling tube, such as prior art tube
6a with a turbulator component
8, may be assembled along with a second type of cooling tube, such as extruded metal
tube
10, and a third type of cooling tube, such as extruded metal tube 12. Metal tubes
10 and
12 may be extruded from any suitable metal, such as aluminum, steel or stainless steel.
[0020] Additionally, because of superior heat transfer characteristics, the tubes made according
to the invention also can be used for cooling applications such as hybrid vehicle
electronics. Usually such electronics are cooled by a separate coolant loop due to
their relatively lower temperature operating characteristics (below 70C). Due to limited
pump power in this second loop, however, the coolant flow is relatively lower when
compared with the main radiator. Prior art radiator tubes, such as those illustrated
in Fig. 2, are not well suited for this kind of application because there is not sufficient
internal surface within such tubes to transfer heat. Tubes made according to the invention,
as describe above, typically will have more surface area to transfer heat. FIG. 7
illustrates an exemplary arrangement of tubes within a combination heat exchanger
that includes a first coolant loop or circuit for fluid cooling, schematically indicated
by a first inlet manifold
4 and a first outlet manifold
5 and first bundle of tubes
10a-10c, and a second coolant loop or circuit for coolant cooling, schematically indicated
schematically indicated by a second inlet manifold
20 and a second outlet manifold
21 and second bundle of tubes
10d-10e. In this arrangement, the first bundle of tubes
10a-10c is of the same type as the second bundle of tubes
10d-10e. The benefit of such an arrangement is that a single tube type can be disposed within
a single heat exchanger, but between separate inlet and outlet chambers for different
cooling applications.
[0021] While this invention has been described with an emphasis upon particular embodiments,
it should be understood that the foregoing description has been limited to the presently
contemplated best modes for practicing the invention. For example, the precise form
of the flat tubes may be modified in accordance with the invention. It will be apparent
that further modifications may be made to the invention, and that some or all of the
advantages of the invention may be obtained. Also, the invention is not intended to
require each of the abovedescribed features and aspects or combinations thereof. In
many instances, certain features and aspects are not essential for practicing other
features and aspects. The invention should only be limited by the appended claims
and equivalents thereof, since the claims are intended to cover other variations and
modifications even though not within their literal scope.
1. An heat exchanger for use in a motor vehicle, the heat exchanger comprising a inlet
chamber, an outlet chamber, a plurality of extruded metal flat tubes arranged in rows
and connected between the inlet and outlet chambers, a plurality of fins disposed
between the rows of tubes, and wherein each of the tubes includes a plurality of extruded
fluid paths.
2. The heat exchanger of claim 1, wherein the flat tubes are oil cooling tubes.
3. The heat exchanger of claim 1, wherein the flat tubes are charge air cooling tubes.
4. The heat exchanger of claim 1, wherein the flat tubes are exhaust gas tubes.
5. The heat exchanger of claim 1, wherein the flat tubes are aluminum.
6. The heat exchanger of claim 1, wherein the transverse cross-section of each extruded
fluid path within a tube is identical.
7. The heat exchanger of claim 1, wherein the transverse cross-section of at least one
of the extruded fluid paths within a tube is different than the transverse cross-section
of at least one of the other extruded fluid paths.
8. The heat exchanger of claim 1, wherein the transverse cross-section of at least one
of the extruded fluid paths is rectangular.
9. The heat exchanger of claim 8, wherein the transverse cross-section of at least one
of the extruded fluid paths includes a plurality of flanges along at least one side.
10. The heat exchanger of claim 9, wherein the transverse cross-section of at least one
of the extruded fluid paths includes a plurality of flanges along a first side and
a plurality of flanges along a second side.
11. The heat exchanger of claim 10, wherein the plurality of flanges along the first side
have the identical pattern to the plurality of flanges along the second side.
12. The heat exchanger of claim 8, wherein the transverse cross-section of at least one
of the extruded fluid paths includes a plurality of flanges along four sides.
13. The heat exchanger of claim 9, wherein the dimension of the flanges along a first
axis is in the range of about 10 percent to about 30 percent of the dimension of the
at least one fluid path along the first axis.
14. The heat exchanger of claim 9, wherein the dimension of the flanges along a second
axis is in the range of about 50 percent to about 75 percent of the dimension of the
at least one fluid path along the second axis.
15. The oil-to-air heat exchanger of claim 1, wherein the transverse cross-section of
at least one of the extruded aluminum fluid paths is oval.
16. A heat exchanger for transferring heat, the heat exchanger comprising: a fluid inlet,
a fluid outlet and a plurality of fluid flow paths extending between the fluid inlet
and the fluid outlet, wherein each flow path is defined by an extruded tube that includes
a plurality of extruded fluid sub-paths.
17. An heat exchanger for use in a motor vehicle, the heat exchanger comprising:
a first coolant loop comprising a first inlet, a first outlet, a first bundle of extruded
flat tubes arranged in rows and connected between the first inlet and first outlet
chambers, and a plurality of fins disposed between the rows of tubes, wherein each
of the flat tubes in the first bundle include a plurality of extruded fluid paths;
a second coolant loop comprising a second inlet, a second outlet, a second bundle
of extruded flat tubes arranged in rows and connected between the second inlet and
second outlet chambers, and a plurality of fins disposed between the rows of tubes,
wherein each of the flat tubes in the second bundle include a plurality of extruded
fluid paths;
18. The heat exchanger of claim 17, wherein the fluid paths in the first bundle are aluminum
oil-cooling tubes.
19. The heat exchanger of claim 17, wherein the fluid paths in the first bundle are air
cooling fluid paths.
20. The heat exchanger of claim 17, wherein the fluid paths in the first bundle are exhaust
gas fluid paths.
21. The heat exchanger of claim 17, wherein the fluid paths in the second bundle are aluminum
coolant-cooling tubes.
22. The heat exchanger of claim 17, wherein the transverse cross-section of each extruded
fluid paths within a tube in the first and second bundle of tubes is identical.
23. The heat exchanger of claim 17, wherein the transverse cross-section of at least one
of the extruded fluid paths is rectangular.
24. The heat exchanger of claim 23, wherein the transverse cross-section of at least one
of the extruded fluid paths includes a plurality of flanges along at least one side.