FIELD OF THE INVENTION
[0001] The invention relates to a heat exchanger. In particular, the invention relates to
the heat exchanger for a motor vehicle.
BACKGROUND OF THE INVENTION
[0002] Evaporators look like, and in fact are, similar to radiators, only thicker and smaller
in overall size. Like radiators, evaporators consist of a series of internal tubes
or flow paths with fins attached to them. Air can pass freely through the fins, just
like a radiator. But unlike a radiator, where the internal tubes carry moving engine
coolant, the passages in the evaporator carry moving refrigerant.
[0003] In an automotive air conditioning system (further referred to as A/C system), cold,
low-pressure liquid refrigerant enters the evaporator. Warm air from the interior
of the vehicle passes through the evaporator by action of the blower fan. Since it's
a fact of nature that heat always travels from a warmer area to a cooler area, the
cooler refrigerant flowing inside the evaporator's absorbs heat from the warm air.
At the same time, humidity in the air condenses on the cool evaporator's surface,
then eventually drips out of a drain tube to the outside. After the initially warmed
refrigerant has completed its path through the evaporator, it moves on to the compressor.
[0004] In order to improve the heat exchange between the media, so-called fins are implemented
in-between the tubes of the evaporator. The fins are interlaced to form a sandwich
with adjacent tubes. The fins allow to increase the heat exchange area while still
allowing the air to flow in-between the tubes. However, during the heat exchange the
ambient air may condensate. The water condensed during evaporation is hot and may
contain a small amount of the debris. This 'carry over' in the vapour is due to air
impurities creating a mist of tiny particles which can be carried over into the condensate
along with the water. For this reason the evaporator condensate, although relatively
pure can contain enough organic material to support bacterial growth when cool. This
makes the condensate unacceptable for re-use in any environment. The condensate accumulated
on the surface of the evaporator may create the environment which may be harmful for
the passengers. It may also lead to decreased service life of the whole heat exchanger
due to deterioration or corrosion of different sub- components.
[0005] Thus, it is desirable to provide an efficient way to evacuate condensate form the
surface of the heat exchanger.
SUMMARY OF THE INVENTION
[0006] The object of the invention is, among others, a heat exchanger for heat exchange
between a first fluid and a second fluid comprising: a first header- tank assembly;
a second header- tank assembly wherein the heat exchanger is intended for operation
in orientation in which the first header- tank assembly is substantially higher with
respect to a ground level than the second header- tank assembly; plurality of tubes
arranged in a first stack and in a second stack, wherein the stacks are arranged between
the first header- tank assembly and the second header- tank assembly, wherein the
second stack is arranged downstream to the first stack with respect to the intended
first fluid flow path; at least one fin interlaced between two adjacent tubes of each
stack, wherein the fin further comprises a first section configured to deflect the
first fluid substantially obliquely-upwardly, and a second section configured to deflect
the first fluid towards the second header- assembly, wherein the second section is
arranged downstream to the first section with respect to the intended first fluid
flow path, characterised in that the fin further comprises a third section arranged
downstream to the first section and the second section so that the second section
is located substantially between the first stack and the second stack.
[0007] Preferably, the third section deflects the first fluid substantially in the same
direction as the first section.
[0008] Preferably, the third section deflects the first fluid in different direction than
the first section.
[0009] Preferably, the first stack comprises a first thickness measured perpendicularly
to a stacking direction and a second stack comprises a second thickness also measured
perpendicularly to a stacking direction, wherein the stacks are arranged between the
first header- tank assembly, so that the gap is formed between the stacks.
[0010] Preferably, the third section at least partially overlaps the second thickness and
the first section at least partially overlaps the first thickness.
[0011] Preferably, the heat exchanger comprises a gap between the first stack and the second
stack, wherein the gap is smaller than any of the thickness.
[0012] Preferably, the second section at least partially overlaps the gap.
[0013] Preferably, the first header-tank assembly comprises two fluidly isolated channels
for the first fluid, and wherein the first header-tank assembly further comprises
an inlet and an outlet for connecting the heat exchanger into first fluid loop.
[0014] Preferably, the second header-tank assembly comprises two fluidly isolated channels
for the first fluid, and wherein the second header-tank assembly further comprises
an inlet and an outlet for connecting the heat exchanger into first fluid loop.
[0015] Preferably, the first section comprises at least one first louver aligned at a first
louver angle measured with respect to the intended first fluid flow direction.
[0016] Preferably, the second section comprises at least one second lover aligned at a second
louver angle measured with respect to the intended first fluid flow direction.
[0017] Preferably, the second louver angle is equal to (α1)+90 degrees.
[0018] Preferably, the third section comprises at least one third lover aligned at a third
louver angle measured with respect to the intended first fluid flow direction.
[0019] Preferably, the third louver angle is substantially equal to the first louver angle.
[0020] Preferably, the third louver angle is different than the first louver angle and the
second louver angle.
[0021] Preferably, at least one of the louver angles in the range from 30 to 40 degrees.
[0022] Preferably, at least one of the louver angles is in particular 35 degrees.
[0023] Preferably, the first thickness is substantially equal to the second thickness.
[0024] Preferably, the first thickness is different than the second thickness.
[0025] Preferably, the heat exchanger is evaporator.
[0026] Another object of the invention is a motor vehicle comprising such heat exchanger.
BRIEF DESCRITPTION OF DRAWINGS
[0027] Examples of the invention will be apparent from and described in detail with reference
to the accompanying drawings, in which:
Fig. 1 shows a perspective view of the heat exchanger.
Fig. 2 shows detailed, cross- sectional view of the fin according to prior art.
Fig. 3 shows detailed, cross- sectional view of the fin according to embodiment of
an invention.
DETAILED DESCRIPTION OF EMBODIMENTS
[0028] The invention refers to a heat exchanger for a motor vehicle such as evaporator.
The main sub-components of the evaporator are depicted by Fig. 1 and briefly described
by further paragraphs.
[0029] A heat exchanger 1 enables the heat exchange between two fluids, wherein one fluid
(e.g. refrigerant) is encapsulated and circulates within the heat exchanger 1 and
the other (e.g. air) flows across the sub-components of the heat exchanger 1.
[0030] Fig. 1 shows the perspective view of the heat exchanger 1 comprising main sub-components,
i.e. plurality of tubes 40 comprising open ends. The tubes 40 may be in form of elongated,
flattened channels stacked between two header- tank assemblies 20, 30, wherein all
tubes 40 are oriented in the same direction, so that the fluid (e.g. air) may flow
through the stack. The tubes 40 may provide a fluidal communication between the header-
tank assemblies 20, 30. The tubes 40 actively participate in the heat transfer process,
so the flattened shape of the tubes 40 not only enables the fluid to flow through
the stack, but also increases the heat transfer surface. However, the specific dimensions
of the tubes 40 should be calculated respecting the characteristics of other sub-components.
The tubes 40 may be arranged in a first stack 41 comprising a first thickness T1 measured
perpendicularly to a stacking direction S1 and in a second stack 42 comprising a second
thickness T2 also measured perpendicularly to a stacking direction S1. In order to
show how the thickness T1, T2 and stacking direction S1 are supposed to me measured,
they have been indicated in the figures. The header- tank assemblies 20, 30 may comprise
minor differences, depending on what role may each one of them play for the heat exchanger
1.
[0031] The tubes 40 may be formed, for example, in the process of extrusion. This process
enables to create the tubes 40 comprising one, or many channels within the single
tube. Alternatively, the tubes 40 may be made of out of single, folded sheet of metal.
Fig. 1 further shows the architecture of the heat exchanger, in which the first header-tank
assembly 20 comprises both inlet and outlet, so it is configured to deliver and collect
the fluid from the heat exchanger 1. The first header and the first cover may form
continuous channels for the for the fluid. In other words, there may be no baffles
located within the channels formed by the first header- tank assembly 20 so that the
fluid is delivered along the main axis of elongation of the channels up to the end
portion of the first header- tank assembly 20. Similarly, the second header and the
first cover may form continuous channels for the for the fluid. This allows to form
two passes for the fluid, wherein one channel of the first header- tank assembly 20
is fluidly connected with one channel of the second header-tank assembly 30 via one
stack of tubes 40, and the other channel of the first header- tank assembly 20 is
fluidly connected with the other channel of the second header-tank assembly 30 via
the other stack of tubes 40. The U-turn of the fluid is formed between the adjacent
channels of the second header- tank assembly 30.
[0032] Further, the header- tank assemblies 20, 30 may comprise at least one baffle configured
to redirect flow of the fluid within the channel. This allows to arrange more than
two passes within the heat exchanger 1.
[0033] The heat exchanger 1 is intended for operation in orientation in which the first
header-tank assembly 20 is substantially higher with respect to a ground level than
the second header- tank assembly 30.
[0034] Term "ground level" may be understood as the plane P1 being perpendicular with respect
to gravitational force Fg. The heat exchanger 1 may however be inclined relatively
to ground level, depending on the position of the vehicle. Preferably, the heat exchanger
is oriented vertically, i.e. the tubes 40 are arranged in perpendicular to the plane
P1 whereas the axes of elongation of header-tank assemblies 20, 30 may be parallel
to the plane P1.
[0035] The alternative architecture of the heat exchanger 1 may include the second header-tank
assembly 30 comprising both inlet and outlet, so that it is configured to deliver
and collect the fluid from the heat exchanger 1. In other words, the alternative design
may include the heat exchanger 1 which is oriented upside-down to one depicted in
Fig.1. However, this embodiment is not preferred in view of overall performance of
the heat exchanger 1, due to e.g. grater pressure drop associated with the location
of the inlet and the outlet on the second header-tank assembly 30.
[0036] Fig. 2 shows a detailed view of the heat exchanger with a header- tank assembly 20,
30 and the tubes 40 according to the preamble of claim 1. The tubes 40 may be arranged
in a first stack 41 comprising a first thickness T1 measured perpendicularly to a
stacking direction S1 (not shown) and in a second stack 42 comprising a second thickness
T2 also measured perpendicularly to a stacking direction S1. Again, the stacks 41,
42 may be arranged between the first header- tank assembly 20 and the second header-
tank assembly 30, wherein the second stack 42 is arranged downstream to the first
stack 41 with respect to the intended first fluid flow path depicted by arrows. The
first thickness T1 may be substantially equal to the second thickness T2. Alternatively,
the first thickness T1 may be different than the second thickness T2.
[0037] In order to further facilitate the heat transfer process, the tubes 40 may be interlaced
with so-called fins 50. The fins 50 may be in a form of corrugated sheet of material
of relatively high thermal conductivity, e.g. aluminum. The corrugations form ridges
which may be in contact with the surface of two adjacent tubes 40. Usually, the fins
50 are initially squeezed to increase the number of possible corrugations and then
brazed to the surface of the tubes 40, so that the fins 50 are immobilized with respect
to the tubes 40.
[0038] The heat exchanger 1 may thus comprise at least one fin 50 interlaced between two
adjacent tubes 40, wherein said fin 50 may extend beyond the perimeter delimited by
the stacks 41, 42 in a direction parallel to intended first fluid flow direction.
Further, the fins 50 may also be delimited perpendicularly to the stacking direction
S1 by inner faces of the header-tank assemblies 20, 30. The fin 50 may be configured
to at least partially deflect the first fluid flow path. The term "deflect" should
be understood as to cause (the air) to change its direction with respect to its intended
fluid flow path.
[0039] The fin 50 may further comprise a first section 100 extending by at least half of
the first thickness T1, and the second section 200 arranged downstream to the first
section 100 with respect to the intended first fluid flow path.
[0040] As further shown in Fig. 2, the first stack 41 may comprise the first thickness T1.
The first thickness T1 may be measured perpendicularly to a stacking direction S1.
The second stack 42 may comprise the second thickness T2 also measured perpendicularly
to a stacking direction S1. The stacks 41, 42 may be arranged between the first header-
tank assembly 20 and the second header-tank assembly 30, so that a gap T3 may be formed
between said stacks 41, 42.
[0041] Fig. 3 shows the detailed view of the heat exchanger 1 according to the embodiment
of the invention.
[0042] The first section 100 receives first fluid in a gaseous form, so the molecules are
energetic, fast moving and far apart from each other. As the air encounters cooler
surface of the heat exchanger 1, the molecules become slower, less energetic and closes
together. Then they reach a threshold energy level, the gaseous air changes to liquid.
Therefore, in terms of physical phenomena, the first section 100 may also be called
a condensation section.
[0043] The second section 200 receives the first fluid both in gaseous and liquid form.
The second section 200 is configured to separate two phases of the first fluid, so
that the liquid is evacuated from the vicinity of the tubes as quickly, as possible.
Therefore, the second section 200 may also be called evacuation section.
[0044] The heat exchanger 1 may further comprise a third section 300 arranged downstream
to the first section 100 and the second section 200 so that the second section 200
is located substantially between the first stack 41 and the second stack 42. The term
"arranged downstream" means that the third section 300 may be arranged subsequently
to the first section 100 and the second section 200 in relation to the intended first
fluid flow direction. The third section 300 may be configured to deflect the first
fluid substantially in the same direction as the first section 100. Alternatively,
the third section 300 may be configured to deflect the first fluid in different direction
than the first section 100, for example, in a direction parallel to intended first
fluid flow direction.
[0045] As further shown in Fig. 3, the third section 300 may at least partially overlap
the second thickness T2. Similarly, the first section 100 may at least partially overlap
the first thickness T1. Preferably, at least 50% the second thickness T2 is overlapped
by third section 300. Similarly, at least 50% the first thickness T1 is overlapped
by the first section 100. This allows to provide sufficient condensation area for
the first section 100.
[0046] Alternatively, the overlap between the first section 100 and the third section 30
may be asymmetric. In other words, one section may overlap a greater part of corresponding
thickness than the other. This allows to optimize the flow of the first fluid through
the sections 100, 200, 300.
[0047] As further shown in Fig.3, the heat exchanger 1 may comprise a gap T3 located between
the first stack 41 and the second stack 42. It is evident from Fig.3 that the gap
T3 is smaller than any of the thickness T1 or T2, however, an embodiments in which
the gap T3 is greater than the first thickness, second thickness T2 or both first
and second thickness T1, T2 is also envisaged.
[0048] The second section 200 may at least partially overlap the gap T3. In particular,
the third section 300 may entirely overlap the gap T3, as shown in Fig. 3. This allows
to facilitate extraction of the condensate from the heat exchanger 1.
[0049] In order to provide the proper functionality of the sections 100, 200. 300, the fins
50 may comprise additional features which enhance the heat exchange between the first
fluid and the second fluid.
[0050] As shown in Figs 1 and 2, the first section 100 may comprise at least one first louver
aligned at a first louver angle α1 measured with respect to the intended first fluid
flow direction. The second section 200 may comprise at least one second lover aligned
at a second louver angle α2 measured with respect to the intended first fluid flow
direction. The second louver angle α2 may be equal to (α1) +90 degrees.
[0051] Referring to Fig. 3, the third section 300 may comprise at least one third lover
aligned at a third louver angle α3 measured with respect to the intended first fluid
flow direction. The third louver angle α3 may be substantially equal to the first
louver angle α1. However, an embodiment in which the third louver angle α3 is different
than the first louver angle α1 and the second louver angle α2 is also envisaged.
[0052] In order to maximize the efficiency of the heat exchanger, at least one of the louver
angles α1, α2, α3 may be the range from 30 to 40 degrees. For example, the first louver
angle α1 and the third louver angle α3 may be the same, whereas the second louver
angle α2 may be (α1) +90 degrees. In other words, the second louver angle α2 is a
mirror image of the first louver angle, relatively to the intended first fluid flow
direction. As shown in Fig.3, the second louver of the second section 200 is pointing
substantially obliquely- downwardly, whereas the first louver of the first section
100 is pointing substantially obliquely- upwardly.
[0053] In particular, 17 at least one of the louver angles may be in particular 35 degrees.
[0054] The orientation and the location of the second section allow to facilitate evacuation
of liquid first fluid form the heat exchanger, so that the efficiency of the second
stack 42 is improved.
[0055] This also allows to reduce the bad odor which may be formed during non-operational
mode of the heat exchanger 1.
[0056] Other variations to the disclosed embodiments can be understood and effected by those
skilled in the art in practicing the claimed invention, from a study of drawings,
the disclosure, and the appended claims. The mere fact that certain measures are recited
in mutually different dependent claims does not indicate that a combination of these
measures cannot be used to the advantage.
1. A heat exchanger (1) for heat exchange between a first fluid and a second fluid comprising:
a first header- tank assembly (20); a second header- tank assembly (30) wherein the
heat exchanger (1) is intended for operation in orientation in which the first header-
tank assembly (20) is substantially higher with respect to a ground level than the
second header- tank assembly (30); plurality of tubes (3) arranged in a first stack
(41) and in a second stack (42), wherein the stacks (41, 42) are arranged between
the first header- tank assembly (20) and the second header- tank assembly (30), wherein
the second stack (42) is arranged downstream to the first stack (41) with respect
to the intended first fluid flow path;
at least one fin (50) interlaced between two adjacent tubes (40) of each stack (41,
42), wherein the fin (50) further comprises a first section (100) configured to deflect
the first fluid substantially obliquely-upwardly, and a second section (200) configured
to deflect the first fluid towards the second header- assembly (30), wherein the second
section (200) is arranged downstream to the first section (100) with respect to the
intended first fluid flow path,
characterised in that the fin (50) further comprises a third section (300) arranged downstream to the first
section (100) and the second section (200) so that the second section (200) is located
substantially between the first stack (41) and the second stack (42).
2. The heat exchanger (1) according to claim 1, wherein the third section (300) deflects
the first fluid substantially in the same direction as the first section (100).
3. The heat exchanger (1) according to claim 1, wherein the third section (300) deflects
the first fluid in different direction than the first section (100).
4. The heat exchanger (1) according to any of the preceding claims, wherein the first
stack (41) comprises a first thickness (T1) measured perpendicularly to a stacking
direction (S1) and a second stack (42) comprises a second thickness (T2) also measured
perpendicularly to a stacking direction (S1), wherein the stacks (41, 42) are arranged
between the first header- tank assembly (20), so that the gap (T3) is formed between
the stacks (41, 42).
5. The heat exchanger (1) according to preceding claim, wherein the third section (300)
at least partially overlaps the second thickness (T2) and the first section (100)
at least partially overlaps the first thickness (T1).
6. The heat exchanger (1) according to claims 4 or 5 comprising a gap (T3) between the
first stack (41) and the second stack (42), wherein the gap (T3) is smaller than any
of the thickness (T1) or (T2).
7. The heat exchanger (1) according to claim 6, wherein the second section (200) at least
partially overlaps the gap (T2).
8. The heat exchanger (1) according to any of the preceding claims, wherein the first
header-tank assembly (20) comprises two fluidly isolated channels for the first fluid,
and wherein the first header-tank assembly (20) further comprises an inlet and an
outlet for connecting the heat exchanger (1) into first fluid loop.
9. The heat exchanger (1) according to claims 1-7, wherein the second header-tank assembly
(30) comprises two fluidly isolated channels for the first fluid, and wherein the
second header-tank assembly (30) further comprises an inlet and an outlet for connecting
the heat exchanger (1) into first fluid loop.
10. The heat exchanger (1) according to any of the preceding claims, wherein the first
section (100) comprises at least one first louver aligned at a first louver angle
(α1) measured with respect to the intended first fluid flow direction.
11. The heat exchanger (1) according to any of the preceding claims, wherein the second
section (200) comprises at least one second lover aligned at a second louver angle
(α2) measured with respect to the intended first fluid flow direction.
12. The heat exchanger (1) according to claims 10 and 11, wherein the second louver angle
α2 is equal to (α1)+90 degrees.
13. The heat exchanger (1) according to any of the preceding claims, wherein the third
section (300) comprises at least one third lover aligned at a third louver angle (α3)
measured with respect to the intended first fluid flow direction.
14. The heat exchanger (1) according to claim 13, wherein the third louver angle (α3)
is substantially equal to the first louver angle (α1).
15. A motor vehicle comprising a heat exchanger (1) according to any of the preceding
claims.