Field of the Invention
[0001] The present invention relates to a heat exchanger, and particularly, although not
exclusively to an exhaust gas recirculation heat exchanger.
Background of the Invention
[0002] Heat exchangers that cool hot gases with a coolant liquid stream (and as a specific
example an Exhaust Gas Recirculation Cooler) have a number of requirements that drive
continuing design developments, including the following:
- 1. Customers' packaging space is being reduced.
- 2. Greater heat exchange and lower pressure drops are being specified which either
requires a larger heat exchanger of traditional design or a new design.
- 3. Customers are continuously looking to reduce both weight and cost.
- 4. The delivery pressure of both fluids is increasing.
- 5. For different power ranges of the same engine, the customer specifies different
mass flow rates. To maintain performance this would require a change in the cooler
design. However, the customer wishes to restrict the cost of tooling.
- 6. Regeneration of the fouling caused by the exhaust gas back towards the clean condition
is critical to maintaining high levels of performance.
[0003] On top of these drivers there are the ongoing needs:
- 1. To ensure that the thermal loading of the heat exchanger, especially at the gas
inlet interface, is kept within safe limits. A major contributor to this is to control,
reduce and stop boiling of the liquid coolant.
- 2. To have well distributed gas flows over the width of the plate.
- 3. To have good and well controlled flow of the coolant, especially at the gas inlet
interface.
- 4. To ensure that the liquid side of the cooler does not have pockets that could trap
air.
- 5. To have a design which allows both fluid interfaces to be either in line with the
cooler or at right angles to the cooler.
[0004] To aid manufacturability and thus help reduce costs.
- 1. As many internal joints that are designed to be leak tight to be checked prior
to full assembly. This reduces the cost of scrap.
- 2. As many internal joints that are designed to carry a load can be tested prior to
full assembly. This reduces the cost of scrap.
- 3. All joints that can not be checked as sub-assemblies to be re-workable in the full
assembly.
[0005] Exhaust gas recirculation heat exchangers are used in vehicles to remove heat from
the recirculated exhaust of an internal combustion engine. Exhaust gas recirculation
is a nitrogen oxide NOx reduction technique used in petrol/gasoline or diesel engines.
EGR works by which circulating a portion of the engine's exhaust gases back to the
cylinders of the engine which reduces the percentage of oxygen and so reduces the
flame temperature of the fuel inside the engine which reduces NOx formation. The cooler
the recirculated gas the more gas can be flowed and the lower the flame temperature.
[0006] In modern diesel engines, the recirculated exhaust gas is cooled using a heat exchanger
to allow a greater mass of gas to be recirculated into the cylinders of the engine
than if the recirculated gas is uncooled.
[0007] Typically a heat exchanger for EGR use has a plurality of plates within a casing.
Exhaust gases are passed through the plates, and the casing provides a fluid tight
jacket around the plates to cool the gases in the plates.
[0008] Prior art heat exchangers for other uses comprise a series of a plurality of plates
built as a stack and brazed together. This has an advantage that there is no outer
casing, which reduces manufacturing cost. The braze holds the individual plate members
together, and seals an outer wall around the plates.
[0009] Figure 1 herein shows a prior art heat exchanger of the brazed type. This prior art
type of cooler is typically used as an oil cooler in the automotive industry, or in
the dairy industry, and are generally used for liquid to liquid heat exchange where
there is a relatively constant pressure on either side of the component. Typically
such heat exchangers are used where the temperatures are not excessively high.
[0010] A problem with the prior art low temperature heat exchanger is that it requires a
lot of brazing. The heat exchanger is built up as a series of individual flat metal
plates, each of which are coated with a braze material. The plates are stacked up
on top of each other, and the heat exchanger plates are brazed together as one assembly
in a single operation.
[0011] A problem with the brazed joint is that one cannot be certain that the joints are
correctly formed, or that there is any joint there at all. The only place where the
braze is visible and accessible for testing is around the outer edges of the device,
and around the inlet and outlet for the coolant. The whole assembly can be leak checked
to see if there is any liquid leaking from the completed heat exchanger. However,
the brazed joints inside the assembly are not accessible for inspection. Unless the
device is pressure tested to failure, then it is not certain that all the internal
brazed joints are correctly formed and are not leaking internally. The internal brazed
joints cannot be tested nondestructively or inspected to make sure that they have
the required strength to withstand the pressure pulsations to which the heat exchanger
will be subjected to in use.
[0012] In an EGR application, the temperatures of the exhaust gases is higher. To withstand
the cyclic pressures which the device is subjected to in use, it needs to be ensured
that each one of the internal brazes joins properly to give mechanical strength between
the plates. This is very difficult to ensure.
[0013] A further problem with the prior art when used for an application such as an EGR
cooler is that the cooler does not flow the gas in its optimal flow.
[0014] A second objective in an EGR heat exchanger is to obtain heat transfer between two
fluid flows as efficiently as possible.
[0015] In a known liquid to gas heat exchanger there are heat exchange plates which have
gas running through a plurality of channels through the centres of the heat exchange
plates, and liquid coolant surrounding the outside of the plates.
[0016] In the known liquid to gas heat exchangers, a flat area between the inlet and outlet
tubes does not act as a fin because the whole of the surface is driven to the coolant
temperature.
[0017] In
EP1159574 there is disclosed a plate heat exchanger for use in the food industry, for cooling
beverages such as beer, which comprises a plurality of a corrugated plates, where
pairs of adjacent plates are coated with a solder material so that corrugated projections
of each pair of plates are brazed together, and the plates are bent over at their
edges, so that when the plates are stacked one on top of the other the edges of the
plates can be brazed together to form a heat exchanger which does not need an outer
casing.
Summary of the Invention
[0018] In a known liquid to gas heat exchanger, a flat area between the inlet and outlet
tubes does not act as a fin because the whole of the surface is driven to the coolant
temperature. However, the inventors herein have realised that if the gas and liquid
flows were reversed, so that the coolant was on the inside of the plate and the gas
was on the outside of the plate, the flat areas would become a fin and would operate
to exchange heat between gas and liquid.
[0019] The known heat exchanger suffers from the problem that in the prior art seamless
plate cooler, the welded section is a secondary surface, and the gas passage primary
surface are both at coolant temperature. Therefore part of the heat exchange surface
is wasted, and not used for efficient heat exchange.
[0020] Specific embodiment heat exchangers disclosed herein preferably have a primary heat
exchange surface and a secondary heat exchange surface formed from a single sheet
of material.
[0021] However with the present heat exchanger, those surfaces are not utilised for heat
exchange.
[0022] In a specific method of construction disclosed herein, an individual cell is formed,
so that two plates are joined together to form two sides of a cell, with either a
weld or a braze extending all the way around a perimeter of the cell, and with individual
welds or brazing across a central area of the cell.
[0023] Each individual cell is pressure tested or otherwise checked for fluid leaks and
mechanical integrity, before assembly into a stack which forms the finished heat exchanger.
A plurality of cells, each of which has been tested for fluid leaks and found to be
fluid tight and have adequate mechanical integrity are joined together, and the only
places of the cells which need to be joined together are the areas around the inlet
and outlet interfaces of the cells, and around the outer perimeters of the cells,
all of which can be tested via a final pressure leak test of the finished stack.
[0024] According to a first aspect, there is provided a gas to liquid coolant heat exchanger
for transferring heat between a gas and a liquid coolant, said heat exchanger comprising:
a plurality of heat exchange cells;
each said cell comprising a liquid coolant inlet and the liquid coolant outlet;
each said cell comprising a pair of plates each said plate having a plurality of grooves
which form a plurality of liquid coolant channels between said plates, extending between
said liquid coolant inlet and liquid coolant outlet;
characterised in that
each said cell contains said liquid coolant within said cell between said pair of
plates.
[0025] According to a second aspect, there is provided a heat exchange cell for a gas to
liquid heat exchanger, said cell comprising:
a first plate and the second plate;
at least one of said plates having a plurality of grooves which form a plurality of
liquid coolant channels between said plates,
characterised in that
each said cell contains said liquid coolant within said cell between said plates.
[0026] According to a third aspect, there is provided a gas to liquid heat exchanger comprising:
a plurality of heat exchange cells, each said cell comprising a first plate and a
second plate;
wherein each said heat exchange cell comprises a liquid inlet aperture and a liquid
outlet aperture;
each said plate comprising a sealed perimeter of the coolant channels, and a plurality
of internal fluid channels;
each heat exchange cell having its coolant perimeter sealed independently of the outer
perimeter of each other said heat exchange cell;
said plurality of heat exchange cells arranged side-by-side in a stack arrangement;
wherein said plurality of heat exchange cells are sealed to each other by an outer
perimeter seal around at least part of their respective outer perimeters, to form
a plurality of gas channels extending between said plurality of cells.
[0027] According to a fourth aspect, there is provided a method of manufacture of a heat
exchanger comprising a plurality of heat exchange cells, said method comprising:
individually forming each of said plurality of heat exchange cells, each comprising
a respective first plate and a second plate, by joining said first and second plates
together with a continuous joint extending around the coolant perimeter of said second
plate to form a cavity between said second plate said first plate, through which a
liquid coolant may flow;
individually testing each said cell to check for fluid leaks in said cavity;
joining said plurality of individual heat exchange cells together by placing said
plurality of cells into an assembly of cells;
forming an outer joint around said plurality of cell perimeters;
forming an inlet joint joining together a plurality of inlets of said cells, and
forming an outlet joint by joining together a plurality of outlets of said plurality
of cells.
[0028] According to a fifth aspect, there is provided a heat exchange cell for a gas to
liquid heat exchanger, said cell comprising:
a first plate and a second plate;
at least one of said first and second plates comprising a plurality of elongate grooves,
said plurality of grooves forming a plurality of liquid coolant channels inside said
cell;
at least one of said first and/or second plates having a plurality of outwardly projecting
studs, which project in a direction outwardly from a plane which intersects an outer
surface of a said plate at the position of said plurality of grooves.
[0029] According to a sixth aspect there is provided a gas to liquid heat exchanger comprising
a plurality of heat exchange cells,
each said cell comprising an inner plate and an outer plate;
said plurality of heat exchange cells being stacked together side-by-side to form
a plurality of gas passages there between;
each said cell having an outer surface comprising a plurality of projections which
extend into said gas passages between said cells, for promoting turbulent gas flow
between said cells.
[0030] Individual embodiments may provide a stack of substantially parallel plates;
each plate having a plurality of corrugations, which form channels when placed against
an adjacent plate;
the edges of the plates being folded over to form a wall or rim, so that the edge
of one plate lies adjacent and substantially parallel to the edge of an adjacent parallel
plate;
pairs of plates are joined together around their inner coolant periphery, and between
channels in the central region of the plates;
a plurality of cells, each formed from a pair of adjacent plates (or one plate bent
over on itself) are brazed together around their outer edges, and at their inlet and
outlet ports.
[0031] The heat exchanger may be fabricated by:
forming a heat exchange cell from two parallel plates, or a single plate bent over,
which has a plurality of corrugations so that the two plates form channels there between;
laser welding around a coolant periphery of at least one said plate;
each cell having an inlet port and outlet port;
each cell having a peripheral rim or skirt which is folded over so that when adjacent
cells are placed next to each other the rims contact each other and part of one rim
lies substantially parallel to part of an adjacent room of an adjacent cell;
stacking a plurality of cells together; and
brazing around the outer rims of the cells to form an outer seal, so that the spaces
between adjacent cells form channels for a first fluid path, whilst the interior of
each cell forms a channel for a second fluid;
the brazing operation also connects adjacent cells together at the inlet port and
the outlet ports, thereby sealing the first fluid path between aid adjacent cells,
and a second fluid path inside the cells; and
pressure testing the whole assembly after brazing.
[0032] Hence, each individual cell is pressure tested individually, and any faulty cells
can be rejected or recycled before they are incorporated into an assembly of cells,
thereby improving the reliability of the finished heat exchanger, since only cells
which have passed their individual pressure test are included in the stack of cells
from which the finished heat exchanger is constructed.
[0033] Further, by joining each cell individually prior to assembly into a stack, the joints
between individual channels in each cell are formed more reliably than in the prior
art case, where joints between individual channels are formed in a brazing operation
where the brazes cannot be individually nondestructively tested, and can only be checked
by cutting open and sacrificing a finished heat exchanger to check the internal brazes.
Hence embodiments of the present invention can be tested nondestructively by pressure
testing of each cell individually before assembly into the plate heat exchanger, and
by testing the whole plate exchanger after final assembly of the cells.
[0034] Preferably there is provided a gas to liquid heat exchanger that encloses a liquid
coolant within a cell.
[0035] Preferably each cell is designed to control and direct the flow of coolant such that
there is adequate flow of coolant across the gas inlet interface to reduce and/or
eliminate the occurrence of coolant boiling.
[0036] Preferably a said cell is designed to control and direct the flow of coolant such
that there is adequate flow of coolant in all of a plurality of longitudinal coolant
channels, so as to reduce and/or eliminate the occurrence of coolant boiling.
[0037] Preferably said cell is designed to significantly reduce the volume of coolant within
the heat exchanger such that the cooler is both smaller and lighter in its wet condition
compared to prior art coolers of similar heat exchange capacity.
[0038] Said heat exchanger may effectively 'decouple' the geometry of the coolant side and
the gas side of a heat exchanger such that the coolant performance and the gas performance
can be maximised.
[0039] Preferably, said heat exchanger has a heat exchange of > 0.25 W/m
2.K.kg at 98% effective or greater when the pressure loss times absolute inlet pressure
of the gas is <0.5 bar.bar in the range of K (gas inlet temperature - coolant inlet
temperature) of 200°C to 500°C.
[0040] Preferably, in a main part of the heat exchanger, both fluids flow in paths which
extend along a substantially longitudinal direction of said heat exchanger.
[0041] Preferably, said heat exchanger has no separate outer case, bulkhead or separate
gas header.
[0042] Preferably, said heat exchanger can interface the gas inlet and outlet either longitudinally
or perpendicularly to the cooler, or a combination of one of the gas inlet or outlet
interfacing longitudinally to the main length of the heat exchanger, and the other
of the inlet or outlet interfacing perpendicularly to the main length of the heat
exchanger.
[0043] Preferably said heat exchanger has the coolant entry within the main path of the
gas flow characterised by the coolant still being able to vent any gas within the
coolant void.
[0044] The heat exchanger may have the coolant entry outside the main path of the gas flow,
characterised by the coolant still being able to vent any gas within the coolant void.
[0045] In the embodiments described herein, each individual cell fully contains liquid coolant
within the cell.
[0046] In the embodiments described herein, there is shown a method of manufacture of a
heat exchanger, whereby two plates making up a heat exchange cell are welded together
and tested for leaks before assembly of the cells into a stack/core comprising a full
heat exchanger assembly.
[0047] In the embodiments described herein, there are disclosed a plurality of Protrusions
or studs which project into the gas passages between the cells, which introduce turbulence
into the gas flow, but without significantly affecting the flow characteristics or
the volume of the liquid coolant.
[0048] Other aspects are as set out in the claims herein.
Brief Description of the Drawings
[0049] For a better understanding of the invention and to show how the same may be carried
into effect, there will now be described by way of example only, specific embodiments,
methods and processes according to the present invention with reference to the accompanying
drawings in which:
Figure 1 shows a prior art heat exchanger which is fabricated in a single brazing
operation;
Figure 2 herein shows in perspective view from one side a first heat exchanger according
to a specific embodiment herein;
Figure 3 herein shows the first heat exchanger in view from one side;
Figure 4 herein shows the first heat exchanger of figures 2 and 3 in cutaway view
along a line A - A' in figure 3;
Figure 5 herein shows the first heat exchanger of figures 2 and 3 in cutaway view
along a line B - B' in figure 3;
Figure 6 herein shows the first heat exchanger of figures 2 and 3in cutaway view along
the line C - C' in figure 3;
Figure 7 herein shows the first heat exchanger of figures 2 and 3 in cutaway view
along the line D - D' in figure 3;
Figure 8 herein shows the first heat exchanger of figures 2 and 3 herein in cutaway
view along the line E - E' in figure 3;
Figure 9 herein shows a second heat exchanger according to a second specific embodiment
in perspective view form a first side, a first end and above;
Figure 10 herein shows the second heat exchanger according to a second specific embodiment
in perspective view from a first side;
Figure 11 herein shows a core of the second heat exchanger in view from the first
side;
Figure 12 herein shows the second heat exchanger in perspective view from the first
side, a first end and above;
Figure 13 herein shows the second heat exchanger in perspective view from a second
side, a first end, and above;
Figure 14 herein shows a core of the second heat exchanger in perspective view from
the second side, the first end, and above;
Figure 15 herein shows the core of the second heat exchanger in perspective view from
the first side, the first end and above;
Figure 16 herein, shows a first cell of the second heat exchanger, being a cell located
on a side of the core;
Figure 17 herein shows a second cell of the heat exchanger, being a cell located within
the core;
Figure 18 herein shows in perspective view from a first side, a first end and both
a first side plate of the second heat exchanger;
Figure 19 herein shows in perspective view from the second side, a first end, and
above a second side plate of the second heat exchanger;
Figure 20 herein shows a section across the line A-A' in figure 10 herein, showing
an internal structure of the second heat exchanger;
Figure 21 herein shows a section across the line B-B' in figure 10 herein, showing
an internal structure of the second heat exchanger at the ends of the second plates
therein;
Figure 22 herein shows a section across the line C-C' in figure 10 herein showing
an internal structure of the second heat exchanger;
Figure 23 herein shows a section across the line D-D' in figure 10 herein, showing
an internal structure of the second heat exchanger along the length of the heat exchange
cells;
Figure 24 herein shows a section across the line E-E' in figure 10, showing an internal
structure of the second heat exchanger;
Figure 25 herein shows a velocity contour gas flowing in a middle plane, at gas channel
7, within the second heat exchanger as gas flows from the gas inlet to the gas outlet
between adjacent cells;
Figure 26 shows a velocity vector plot of gas flowing in gas channel 1, in a middle
plane view, from the gas inlet end towards the centre of the second heat exchanger;
Figure 27 shows a velocity vector plot of gas flowing in gas channel 1, in a middle
plane view, from the centre of the second heat exchanger towards the second end, where
gas is outlet from the second heat exchanger;
Figure 28 shows a velocity vector plot at a second end of heat exchanger, viewed in
a direction perpendicular to the main planes of the heat exchange cells, showing exhaust
of gas through the outlet passage;
Figure 29 herein shows a velocity magnitude plot of gas flowing through the second
heat exchanger between a gas inlet and a gas outlet in three-dimensional view; and
Figure 30 shows a velocity vector plot of coolant flowing through a cell at the middle
plane of the cell from a coolant inlet at the second end of the second heat exchanger,
towards a coolant outlet at a first end of the second heat exchanger, and showing
mass flow fraction as a % for individual coolant channels 1 -13 across a depth of
the heat exchange cell.
Detailed Description of the Embodiments
[0050] There will now be described by way of example a specific mode contemplated by the
inventors. In the following description numerous specific details are set forth in
order to provide a thorough understanding. It will be apparent however, to one skilled
in the art, that the present invention may be practiced without limitation to these
specific details. In other instances, well known methods and structures have not been
described in detail so as not to unnecessarily obscure the description.
[0051] Referring to figure 2 herein, there is illustrated schematically in perspective view
from above and the front, a plate heat exchanger according to a specific embodiment
disclosed herein.
[0052] The plate heat exchanger 200 comprises a plurality of heat exchange cells 201; a
first fluid inlet tube 203; a first fluid outlet tube 204; a second fluid inlet tube
205; and a second fluid outlet tube 206. The first inlet tube 203 and first outlet
tube 204 are positioned on a same front face 202 of the heat exchanger. The second
fluid inlet tube 205 and the second fluid outlet tube 206 are positioned on opposite
outer faces of the heat exchanger, the second fluid inlet tube 205 being positioned
on the front face 209, and the second fluid outlet tube 206 being positioned on the
rear face of the heat exchanger. The first fluid inlet tube 203 and first fluid outlet
tube 204 form a first fluid path through the heat exchanger for carrying coolant,
such as a liquid coolant. The second fluid inlet tube 205 and the second fluid outlet
tube 206 form a second fluid path through the heat exchanger for the second fluid,
being an internal combustion engine exhaust gas to be cooled prior to being mixed
with an inlet air to the engine.
[0053] The plate heat exchanger comprises a plurality of substantially identical cells,
each cell constructed from a pair of plates. The plurality of cells are positioned
side by side to form a stack of said cells. The outer most cells are slightly different
to the inner cells such that the void for the gas inlet and outlet is closed and there
are interfaces for the coolant inlet and outlet and the gas inlet and outlet if flowed
perpendicular to the main cooler. The first and second outermost cells are slightly
different to each other, because the first outer cell has a pair of apertures positioned
for location of the first inlet tube 203 and the first outlet tube 204, whereas the
second outer most plate does not have such apertures.
[0054] Outside of the outer cells a protective plate may be used. This gives strength to
the fluid inlet and outlet interfaces, adds stiffness to the outer skin of the cooler
for clamping and may cover the heat exchange section of the cooler to give a lower
surface temperature.
[0055] The heat exchanger may be attached to a surface, for example a vehicle engine block
by a pair of brackets 206, 207 respectively which extend around a main body of the
plate heat exchanger, and which has a plurality of tabs having apertures through which
bolts or other fixing means can be passed to attach the brackets to a surface. Alternatively
the heat exchanger may be attached to a surface by the outer protective plates if
used.
[0056] In the heat exchanger of figure 2, at the position at which the gas is inlet and
outlet from the heat exchanger, there is an uncooled section which allows the gas
to spread out across the whole of the face of the cell at the coolant perimeter.
[0057] Referring to figure 3 herein, there is illustrated in view from the front, the heat
exchanger of figure 2 herein. As viewed from the front, the heat exchanger has a substantially
rectangular shape with rounded corners, with the first fluid inlet tube 203 and the
first fluid outlet tube 204 being located adjacent a same first side 303 of the rectangle,
and inwardly from a respective first end 300 and second end 301. The second fluid
outlet tube 206 is located adjacent the first end 300 and adjacent the same side as
the first fluid inlet tube 203 and the first fluid outlet tube 204, whilst the second
fluid inlet tube 205 is located adjacent the second end 301, and adjacent an opposite
second side 304, the second fluid inlet 205 and second fluid outlet 206 being mounted
on opposite faces of the heat exchanger to each other. The first end 300 and the second
end 301 up to the welded joint of the cell 305 and 305 forms a void where the second
fluid can distribute and flow over the full width of the cell.
[0058] Referring to figure 4 herein, there is shown in cutaway view along the section A
- A', the heat exchanger of figure 2 herein. The main body of the heat exchanger is
constructed from a plurality of cells 400 - 409, stacked side-by-side. Each cell is
substantially identical to each other cell, within manufacturing tolerances in the
heat exchange section. Each cell comprises a first plate and a second plate.
[0059] Each first plate comprises a substantially flat sheet having a first (inner facing)
face facing inside the cell, and a first (outer facing) face facing outside the cell,
each said first inner facing face extending in a respective first inner plane and
each said first outer facing face extending in a first outer plane, there being a
plurality of first ridges in the sheet, wherein outer extremities of the first ridges
lie in a first ridge plane, said first ridge plane extending substantially parallel
to said first inner plane and first outer plane. An outer rim portion of said first
plate is formed into a skirt portion which extends around an outer perimeter of said
first plate, to form a substantially frusto pyramid shaped skirt having skirt walls
which extend in planes transverse to the first inner plane, first outer plane and
the ridge plane.
[0060] Each second plate comprises a substantially flat sheet having a second (inner facing)
face, facing inside the cell, and a second (outer facing) face facing outside the
cell, each said second inner facing face extending in a respective second inner plane,
and each said second outer facing face extending in a second outer plane, there being
a plurality of ridges in the sheet, wherein outer extremities of the second set of
ridges lie in a second ridge plane, said second inner plane, second outer plane and
second ridge plane extending parallel to each other, and parallel to the first inner
plane, first outer plane and first ridge plane. Like the first plate, the second plate
does have a peripheral skirt portion.
[0061] The first and second plates are joined together such that the plurality of ridges
of the first plate lie opposite the plurality of ridges of the second plate, so that
between the first and second plates there are formed one or a plurality of internal
cell channels 419 - 431 defined by the ridges.
[0062] The one or a plurality of internal cell channels of the first cell and the one or
plurality of internal cell channels of one or more adjacent cells in the stack collectively
form a first fluid channel through the heat exchanger, for carrying the first fluid.
In the best mode embodiment, the plurality of internal cell channels of each cell
extend in a direction along a length of the heat exchanger between the first fluid
inlet aperture and the first fluid outlet aperture of said cell.
[0063] Between adjacent cells, where a second cell is stacked on top of or adjacent a first
cell, a space between a second (upper) plate of the first cell and a first (lower)
plate of the second cell forms a second plurality of fluid channels, 432 - 444 which
extend between the second fluid inlet apertures and the second fluid outlet apertures
of the cells. Preferably, the second fluid channels also extend in a direction along
a length of the heat exchanger.
[0064] In use, a first fluid passing through the first fluid channels 419 - 431 travels
in a first direction along a length of the heat exchanger, whilst a second fluid passing
through the second fluid channels 432 - 444 travels in a second direction along a
length of the heat exchanger, where the first and second directions are generally
opposite to each other, and thereby achieving a contraflow of the fluids within the
heat exchanger.
[0065] This means that a hot exhaust gas passing through the second fluid inlet apertures
and travelling externally outside the cells transfers heat through the plate walls
to a second fluid (coolant fluid) which is about to exit the heat exchanger through
the first fluid outlet aperture. Similarly, the first fluid (coolant) at its coolest
point on entering the heat exchanger draws heat through the plate walls from the exhaust
gas which is about to leave the heat exchanger through the second fluid outlet, and
which has already experienced a degree of cooling during its passage through the heat
exchanger, to cool the exhaust gas at its coolest point as it leaves the heat exchanger.
The coolant acquires heat during its passage through the heat exchanger, whereas the
exhaust gas loses heat during its passage through the heat exchanger.
Individual Cell Construction
[0066] Each plate is constructed from a single sheet of metal, which is stamped out. Pairs
of plates, each having a set of ridges, and a respective plate inlet aperture and
plate outlet aperture, and forming for skirt portion which extends around the first
plate.
[0067] The first and second plates are welded to each other, preferably using a laser welding
machine, introducing a series of welds between the adjacent channels formed by the
opposite ridges on the first and second plates, and by laser welding around a coolant
perimeter region of the plates so that the set of first channels 419 - 431 are sealed
and fluid tight from channels 432 - 444. Further the laser weld joins each pair of
plates either side of first channels 419 - 431 such that the cell is able to constrain
the internal pressure of fluid 1.
Stack Construction
[0068] As shown in figure 4, the stack of cells is constructed by laying one cell on top
of the other, so that the plurality of cells lie side-by-side. Between pairs of adjacent
cells, there is created a void, so that a plurality of voids 410 - 418 are created
between the cells, which in totality form a second fluid passage through the heat
exchanger, between the second fluid inlet and the second fluid outlet.
[0069] Referring to figure 5 herein, there is shown in cutaway view along the section B
- B', the heat exchanger of figures 2 and 3 herein. In figure 5 the outwardly projecting
studs in the plates are shown sectioned, and the bracket is not shown. These studs
cause turbulence of the gas. Some of the studs may be used to space one cell from
another adjacent cell.
[0070] Referring to figure 6 herein, there is shown in cutaway view along the section C
- C', the heat exchanger of figures 2 and 3 herein. There is shown the first fluid
inlet 203 in cross-sectional view. The first fluid inlet 203 comprises a tubular cylindrical
portion 600 which is a fixed around a perimeter of an inlet aperture of an outermost
facing plate 208. The tubular cylindrical portion is a fixed to the region around
the aperture by brazing or soldering. A collection tube having one end which fits
inside the cylindrical stub tube 600, is held in place by solder or brazing.
[0071] The plurality of perimeter regions 602 - 611 around the individual first inlet apertures
of the individual cells are open, so that the first fluid can permeate into the first
channels inside the individual cells.
[0072] Referring to figure 7 herein, there is shown in cutaway view along the section D
- D', the heat exchanger of figures 2 and 3 herein. Shown in figure 7 is the second
fluid outlet 206. The second fluid outlet comprises a cylindrical tube 700; a cylindrical
stub ring or tube 701 which is soldered to an outermost facing perimeter region of
a second inlet aperture of the plate on the rear face of the heat exchanger; and the
collective plurality of second fluid outlet apertures of the individual cells.
[0073] Around their second outlet apertures, each individual cell has its first and second
plates are laser welded together, so that fluid passing into the spaces between adjacent
cells cannot leak into the inside of the cells themselves.
[0074] Referring to figure 8 herein, there is shown in cutaway view along the section E
- E', the heat exchanger of figures 2 and 3 herein. Shown in figure 8 in cross-sectional
view are the first fluid inlet 203 and the second fluid outlet 206, the second fluid
outlet being of larger diameter than the first fluid inlet. The first fluid inlet
comprises a cylindrical spigot, or tube 600, which is brazed or soldered to an outermost
facing plate of the heat exchanger, and a substantially cylindrical outer tube 601
which is suitable for connecting to an external hose.
[0075] The second fluid outlet 206 comprises an annular spigot or tube 802, which is soldered
or brazed to an outer surface of a plate at the rear of the heat exchanger around
the second inlet apertures of the cells, and a tubular substantially cylindrical pipe
803 which can be connected into an exhaust gas circuit.
[0076] The first fluid inlet connects with a plurality of first fluid inlets of the individual
cells, which collectively form a first fluid inlet passage 804 in the heat exchanger,
and the second fluid outlet 206 forms a channel with a passage formed by the plurality
of individual second fluid outlets, which collectively form a second fluid outlet
channel 805 to allow the second fluid to pass from the channels between individual
cells in the heat exchanger.
Overview of Method of Manufacture
[0077] An overall method of manufacture is as follows. Each individual cell is formed from
a pair of plates.
[0078] Each pair of plates is joined around their coolant perimeter, and in a region within
the outer perimeter. Joining can be either by brazing, or by laser welding.
[0079] Each cell is pressure tested to check for leaks and mechanical integrity around the
cell perimeter, and in the region bounded by the coolant perimeter.
[0080] A plurality of cells are laid side-by-side and formed into a stack. The plurality
of cells are joined together around the outer edges of the cells, and around the regions
which border the inlet apertures and outlet apertures of the cells. Joining together
of the cells to form the stack is by brazing or soldering.
[0081] The internal regions where adjacent cells are soldered or welded to each other inside
the inlet passages and outlet passages can be inspected visually, and the joining
around the outer perimeter of the cells can also be inspected visually.
[0082] Spigots are attached at the first inlet, second inlet, first outlet and second outlet.
[0083] The stack is then pressure tested by attaching tubes to the inlet and outlet spigots,
and pressurising fluid through the first fluid channel and second fluid channel, and
by measurement of the stack for leaks.
Cell Manufacture Method
[0084] Each plate is formed from a single sheet of metal material. A pair of plates is stamped
out from a single sheet of metal material using a stamping machine. The stamping operation
cuts a perimeter around a piece of initially flat metal material, and at the same
time stamps a first plurality of ridges and troughs in a first area of the sheet of
material to form a first plate, and a second plurality of ridges and troughs in a
second area of material, to form a second plate.
[0085] An upper plate is positioned on top of a lower plate such that the plates lie parallel
to each other and opposite each other side-by-side. The plurality of ridges and troughs
on the respective first and second plates lie opposite each other, with ridges on
the first plate lying opposite ridges on the second plate, and troughs on the first
plate lying opposite troughs on the second plate, so that the adjacent opposite ridges
can contact each other, and the adjacent opposite troughs between the ridges form
a plurality of channels through the cell.
[0086] First and second plates are then joined together around a coolant perimeter, and
along areas of the plates which contact each other, For example along regions between
the channels. Joining can either be by welding, for example laser welding or brazing.
[0087] Once joined, each cell is individually tested for leaks and for robustness of the
joints. Each cell can be visually inspected, or non-destructively pressure tested
by injecting fluid under pressure into the cell and testing for leaks and excessive
deformation, which may indicate weak welds or joins in the central area of the plates.
Stack Method of Manufacture
[0088] A plurality of cells, each of which has been previously leak tested, are assembled
into a stack by laying the cells one on top of each other. The cells self - align
with each other due to the skirt regions on each cell, which are angled in a substantially
frusto pyramid shape which allows the cells to be stacked one on top of each other,
with a lower outer surface of the first cell facing an upper outer surface of an adjacent
second cell. The plurality of cells may be held together by clamping. The outwardly
projecting studs may also set the spacing between cells.
[0089] The plurality of cells forming the stack are joined together in a single brazing
or soldering operation. The plurality of skirt regions are joined, by brazing each
skirt to one or more adjacent skirts.
[0090] Outer surfaces of the cells adjacent cell first fluid inlet passages are joined together
by brazing or soldering, forming a plurality of circular or annular seals between
adjacent cells. The plurality of adjacent seals around the first inlet's, and the
circular first inlet apertures in the cells form the first inlet passage extending
through the stack.
[0091] Similarly, the surface areas of adjacent cells which touch each other around the
first fluid outlet passages are each sealed by welding or brazing to form a plurality
of circular or annular seals, which together with the plurality of first outlet apertures
form the first outlet passage extending through the stack.
[0092] Similarly, the outer perimeter edges of the cells are joined together by brazing
or soldering, forming a plurality of perimeter seals between adjacent cells.
[0093] Having joined a plurality of cells together to form the stack, the completed stack
may be visually inspected to make sure that there are no visually identifiable defects
in the solders or brazes around the outer skirts, and in the regions around the first
fluid inlet passage, first fluid outlet passage, second fluid inlet passage and second
fluid outlet passage.
[0094] The first fluid inlet spigot, the first fluid outlet spigot, the second fluid inlet
spigot, and the second fluid outlet spigot are located in the corresponding respective
first fluid inlet aperture, first fluid outlet aperture, second fluid inlet aperture
and second fluid outlet apertures, of the outermost plates on of the stack, and are
joined to the material around those apertures by welding or brazing.
[0095] The completed stack with connected spigots may be pressure tested by connecting a
fluid supply and drain tubes to form a first fluid circuit through the first inlet
of the first outlet, and a second fluid circuit through the second inlet and second
outlet and passing fluid through the first and second fluid channels. The stack can
be pressure tested as a whole, with the first and second fluid channels being under
pressure at the same time, or the first fluid channel can be pressure tested independently
of the second fluid channel.
[0096] The heat exchanger disclosed herein is constructed of a series of cells which are
joined together. Hence, rather than braze a series of plates together, as in the prior
art heat exchanger, in the present heat exchanger there are individual cells, each
of which can be checked for leaks before being joined together to make a complete
heat exchanger.
[0097] The heat exchanger forms a cell from two plates, and encapsulates a liquid coolant
within the cell. The primary and secondary heat exchange surfaces are formed from
a single cell.
[0098] Gas flow occurs from one end of the plate to the other, across the full width of
the face of the plate.
[0099] Coolant, via the channels in the cell, flows from near one end of the cell to near
the other end, in an opposite direction to the other liquid, so there is contraflow
between the cooling liquid and the liquid being called.
[0100] The cell has a sealed coolant channel across the gas inlet passage.
[0101] The heat exchanger does not have a bulkhead. Hence there is lower weight, bulk and
cost, compared to the prior art exhaust gas recirculation heat exchanger. Specific
embodiments disclosed herein may provide a heat exchanger without a bulkhead. The
absence of a bulkhead lowers weight and reduced cost. It also avoids the problem of
thermal loading at the bulkhead.
[0102] The heat exchanger does not need a separate case, because the casing is formed by
the sides of the heat exchange plates themselves and the outermost plates.
[0103] The heat exchanger disclosed herein may provide a more compact EGR heat exchanger.
[0104] The heat exchanger disclosed herein may have a plate profile which is easier to manufacture
than prior art plate profiles.
[0105] The individual cells may be laser welded, and hermetically sealed before being assembled
into a full heat exchanger device.
[0106] The specific embodiments herein also have an advantage that there is no heat exchanger
outer case, which reduces manufacturing cost, component weight and component bulk.
[0107] The heat exchanger herein forms gas inlet and outlet headers from the same plates
which form the heat exchange surfaces. This reduces weight, bulk and cost.
[0108] A reduction in overall weight can being achieved, firstly because there is no thick
wall casing, and secondly because there is significantly less coolant in the heat
exchanger.
[0109] In the present embodiments, since the cells are hermetically sealed and are able
to be leak tested as a single cell when sealed at the coolant inlet and outlet interfaces,
this reduces the amount of rejects of full heat exchanger assemblies at the point
of manufacture.
[0110] The heat exchangers disclosed herein have designed flexibility of the cell which
allows some limited deformation under pressure and aids fouling regeneration.
[0111] In a conventional heat exchanger, there is a bulkhead and a reducer and an interface
from the reducer so that heat exchange is not obtained straightaway right across the
plates. In the embodiments herein, the plates themselves create a cavity which act
as a reducer, thereby eliminating the need for a separate reducer section. There is
created a cavity which acts as a reducer, within the cell itself.
[0112] The gas heat exchanger forms the gas inlet and outlet headers from the same plates
as only used for heat exchange. The inlet and outlet ports are outboard of the main
heat exchange area.
[0113] There is a cost saving in manufacture, because the only components used are a series
of plates, and there are no other expensive components which do not actually aid heat
exchange.
[0114] Although there is no outer casing, in the embodiment shown in figures 2 and 3, the
reinforcement plate is added on the front and the back to surfaces of the heat exchanger.
[0115] Referring to figures 9 to 30 herein, there is illustrated a second heat exchanger
according to a second specific embodiment. The second heat exchanger is designed for
cooling a gas, using a liquid coolant.
[0116] Referring to figure 9 herein there is shown the second heat exchanger in perspective
view from above , a first side and a first end;
[0117] Referring to figure 10 herein, there is illustrated schematically the second heat
exchanger in view from a first side.
[0118] Referring to figure 11 herein, there is illustrated schematically the second heat
exchanger in view from the first side, showing an outer most plate as transparent,
so as to view a plurality of liquid coolant channels of an interior core part of the
second heat exchanger, and outwardly protruding studs in the gas channels.
[0119] Referring to figure 12 herein, there is illustrated in perspective view from above
and a first side, the second heat exchanger showing impartial cutaway view and interior
of a central core of the heat exchanger.
[0120] Referring to figure 13 herein, there is illustrated in perspective view from above
and a second side, the second heat exchanger showing impartial cutaway view and interior
of a central core of the heat exchanger.
[0121] Referring to figures 14 and 15 herein, there is illustrated in perspective view from
above and the second side, a central core of the second heat exchanger.
[0122] The second heat exchanger 900 comprises a plurality of heat exchange cells 901; a
gas inlet manifold 902 cavity; a gas outlet tube 903; a liquid coolant inlet tube
904; a liquid coolant outlet tube 905, and an end flange 930. Each cell comprises
a pair of heat exchange plates which are welded together, and a plurality of cells
comprises a heat exchanger body. On the respective first and second outer sides of
the heat exchanger body, there are two outer plates (shown as semi - transparent in
figures 14 and 15) which protect the core of the heat exchanger body, and which provide
a plurality of anchorage points for attaching the heat exchanger to a supporting component,
for example an engine block or a vehicle bulkhead.
[0123] A main body of the heat exchanger comprises a plurality of individual plates which
are stacked side-by-side to form the plurality of individual heat exchange cells.
Each cell is sealed so as to contain a plurality of longitudinally extending liquid
coolant channels which run inside the cell. Adjacent cells are sealed together at
their outer perimeters to form a plurality of gas flow channels which extend longitudinally
along a main length direction of the heat exchanger. A first end of the heat exchanger
is substantially rectangular, where the second end of the heat exchanger has a pointed
or angled shape.
[0124] In use, the liquid may flow through the cells in a direction opposite to the direction
in which the gas flows through the cells, so that contra flow between the liquid coolant
and the gas to be cooled occurs, with the liquid and gas being isolated from each
other. Heat transfers from the gas to the liquid through the thin plate walls.
[0125] However, in the general case, liquid may be passed in either direction along the
length of the cells by reversing the coolant flow direction, although the heat exchanger
may be marginally more efficient with the coolant flowing in the opposite direction
to the gas flow direction (contraflow) than with the gas flow and coolant flow running
along the length of the heat exchanger in the same direction.
[0126] In use, the second heat exchanger is placed in an exhaust gas circuit of an internal
combustion engine so that the gas flow comprises recirculated exhaust gas, and the
liquid coolant flow cools the exhaust gas.
[0127] In the second embodiment heat exchanger, the gas inlet manifold 902 is designed to
accept gas from a direction along a main length axis of the heat exchanger, and gas
is outlet from the heat exchanger via the outlet tube 903 in a direction perpendicular
to a main length axis of the heat exchanger. The gas inlet manifold 902 transfers
gas directly into a plurality of gas passages which extend between adjacent cells
along a main length of the heat exchanger to the outlet end, at which the gas flows
into an outlet passage 923 within the heat exchanger, the outlet passage extending
in a direction transverse to the main planes of the heat exchange plates. Hence, the
gas is inlet in a direction along a main length direction of the heat exchanger, and
is outlet in a direction perpendicular to a main length of the body of the heat exchanger
(although as stated above, the device will also operate with good efficiency with
the gas flowing in the opposite direction). Preferably, a width of the each gas passage
along its main gas flow region between adjacent cells is a distance of no less than
3mm.
[0128] The liquid coolant is connected to the heat exchanger by a substantially "L" shaped
liquid inlet tube 904 so that a connecting fluid pipe (not shown) can run in a plane
parallel to a set of planes which intersect the heat exchange plates, with the liquid
entering the heat exchanger in a direction transverse or perpendicular to the planes
which intersect the heat exchange plates. A liquid inlet passage is formed within
the body of the heat exchanger by the plurality of heat exchange plates, each of which
has its own liquid inlet aperture, the plurality of liquid inlet apertures forming
the inlet passage within the main body of the heat exchanger.
[0129] Similarly, the liquid coolant exits from the heat exchanger through a liquid outlet
passage extending in a direction transverse or perpendicular to the planes which intersect
the heat exchange plates, passing into the liquid outlet tube 905, which is also substantially
"L" shaped, and which connects to a fluid pipe (not shown) which may extend in a plane
parallel to the planes which intersect the heat exchange plates. Each individual heat
exchange plate has a liquid outlet aperture, whereby the plurality of liquid outlet
apertures together form the internal liquid outlet passage within the main body of
the heat exchanger. The liquid outlet tube 905 is connected to the internal outlet
passage. Hence, the heat exchanger can form a compact unit with the liquid being supplied
by a pair of connecting pipes which lay compactly adjacent the heat exchanger.
[0130] For additional mechanical strength, the stack of heat exchange plates may be secured
together by a plurality of externally located connecting members 906 - 909, which
also provide a means of connecting the second heat exchanger to a support. The two
outermost heat exchange plates each have a set of peripheral protruding anchor points
910 - 913 respectively on a second outer plate 927; and 914 - 917 respectively on
a first outer most plate 926, each connecting member 906 - 909 being attached to a
pair of opposite said anchor points, one of which is on the first outer most plate,
and the other one of which is on the second outer most plate, so that the connecting
members connect the outermost plates together, bridging across the stack of plates
in a direction transverse to the planes which intersect the individual heat exchange
plates.
[0131] The connecting members 906 - 909 each comprise a cylindrical tube, the ends of which
are brazed to the anchor plates 910 - 913. In use, the connecting members provide
a fitting points for fitting the second heat exchanger to an engine block or other
vehicle mounting point, by passing bolts through the hollow tubes to attach them to
the engine block or other mounting surface.
[0132] On the second side of the heat exchanger opposite to the liquid coolant inlet 904,
there is provided a first bleed valve 924, which allows any gas in the liquid circuit
to be bled from the liquid coolant path. At a position on the second side of the heat
exchanger opposite to the liquid coolant outlet tube 905 there is provided a second
bleed valve 925, which connects with the liquid outlet passage in the core, and which
can also be used to remove air or gas from the liquid coolant path of the heat exchanger.
Each bleed valve is attached to the heat exchanger along a direction of an internal
inlet or outlet liquid passage.
[0133] Each internal inlet or outlet coolant passage has a teardrop shaped or cam shaped
cross-section, arranged such that a protruding part of the aperture is located at
a highest point of the passage, so as to allow gas to flow to the top of the passage,
and to stop gas becoming trapped in the core. As mentioned elsewhere in this description,
the coolant flow can be reversed, so the inlets and apertures may become swapped over
in function.
[0134] Referring to figure 15 herein, there is shown schematically a core of the second
heat exchanger in view from the first side, being the side to which the coolant inlet
tube 904 and coolant outlet tube 905 are attached. And outermost cover plate is not
shown, except for the anchorage points 914 - 917.
Cell Types
[0135] The second heat exchanger comprises three types of cells as follows:
an inner cell, comprising a first plate and the second plate;
an outer left hand cell, on a first side of the heat exchanger comprising a third
plate and a second plate; and
an outer right hand cell, on a second side of the heat exchanger, comprising a fourth
plate and a second plate.
[0136] Each cell type comprises two separate plates. Overall, there are six different plate
types which can be divided into plates having a first formed shape including coolant
channel indentations which all use the same forming tool, and differ only by virtue
of the regions where apertures are pierced through the basic formed shape; and plates
of a second formed shape, which are formed by a second forming tool, having a plurality
of coolant channel indentations and which differ only by virtue of which regions have
apertures pierced or material removed from the basic second formed shape; and plates
of a third formed shape, being the outer plates which do not have any coolant channel
indentations.
[0137] Referring to figure 16 herein there is shown in view from one side a first type of
cell 1600, comprising a first plate 1601 and a second plate 1602 joined together by
a leak tight weld 1603 extending around a coolant periphery of the second plate, and
joining the second plate to the first plate.
[0138] The first plate 1601 comprises an elongate substantially flat plate which intersects
with a plane, the first plate having a central region containing a plurality of elongate
indentations which extend along a main longitudinal axis of the plate. The plurality
of indentations are separated from each other by a plurality of flat fin portions
extending along a main longitudinal axis of the plate, alternating between adjacent
elongate indentations.
[0139] An outer perimeter of the first plate is formed into a flange or skirt 1604 which
extends around the outside of the first plate in a direction transverse to a main
plane of the first plate. At the first end of the plate, being the gas inlet end,
the skirt is absent, to allow gas flow into the cell.
[0140] At a first end 1605 of the first plate, there extends a flat portion of the plate
1606, which in use forms part of the side of the heat exchanger. At a second end 1607
of the first plate there is a further flat portion 1508 which forms part of the side
of the heat exchanger and seals off one end of the gas outlet passage of the central
core of the heat exchanger. The second end of the first plate comprises a substantially
triangular shaped portion having a rounded corner.
[0141] At the first end of the cell the first and second plates form a first aperture 1610
to allow coolant to flow between the first and second plates and into the plurality
of longitudinal passages extending inside the cell, and at the second end of the cell,
the first and second plates form a second aperture 1609 for exiting liquid coolant
from the inside of the cell. In use, the first aperture 1610 forms a liquid coolant
inlet to the cell, and a second aperture 1609 forms a liquid coolant outlet (although,
the heat exchanger can be connected with direction of flow of the liquid coolant reversed,
making the second aperture 1609 an inlet aperture, and the first aperture 1610 an
outlet aperture). The second aperture 1610 is teardrop or cam shaped, comprising a
circular aperture with a peripheral extending part in the plane of the circle, so
that in use, the extending parts is at a highest point, and any gas forming in the
liquid coolant rises into the void formed by the extending part, from where it can
be bled from the heat exchanger. Similarly, the first aperture 1609 has a similar
teardrop or cam shape, but with the pointed part of the teardrop extending downwardly,
so that if the heat exchangers fitted the other way up, the pointy part of the aperture
will be uppermost, and any gas in the coolant liquid will collect in the pointed part
of the second+ aperture.
[0142] The second plate 1602 is formed from a second sheet of material, and is welded to
the first plate 1601. The second plate comprises a plurality of elongate indentations
1612 which extend longitudinally along a main length of the second plate, and which
are positioned opposite the plurality of indentations in the first plate, to form
a plurality of longitudinal internal channels through which a liquid flows. The second
indentations protrude out of a main plane which is coincident with the main metal
sheet of the second plate.
[0143] With the plurality of longitudinal liquid carrying channels are formed by the plurality
of indentations on the first plate, which lie opposite and extend in an opposite direction
transverse to a main central plane of the cell to the first indentations of the first
plate. Hence, a main central plane of the cell extends at the interface where the
first and second plates touch each other, there being a parallel first outer plane
which intersects with the outer extremity of the first set of longitudinal channels,
and a second outer plane which intersects the main outer extremities of the second
set of longitudinal channels of the second plate. A first plurality of flat fin portions
extend between the first set of indentations on the first plate, and a second's plurality
of flat fin portions extend between the second set of indentations on the second plate.
The first and second flat fin portions lie opposite each other and touch each other
as the two plates are mated together, and the two plates are welded together along
each fin portion between the channels, and around the coolant periphery of the second
plate, so that the liquid coolant channel is contained within the second plate, and
a plurality of individual longitudinal channels within the cell are isolated from
each other by the intervening fin portions. The welds along the fins do not need to
be leak tight, since their primary purpose is to give mechanical strength to the cell,
and the coolant is contained within the leak tight weld which extends around an outer
perimeter of the second plate, joining to the first plate.
[0144] At a first end of the second plate, there is provided a substantially flat portion
1613 which forms a distribution chamber or manifold for channeling liquid between
first aperture 1509 and the first ends of the plurality of internal fluid channels
1612. Similarly, at a second end of the second plate there is provided a second substantially
flat portion 1614 which forms a distribution manifold or chamber for transferring
fluid from the second ends of the plurality of internal channels and a second aperture
1610. The shape of the distribution chambers 1613,1614 is designed so as to create
a flow of coolant all the way across the gas flow, to minimise dwell of liquid in
the distribution chambers, and thereby minimise the risk of the liquid boiling, and
to ensure a relatively even distribution of liquid coolant across all of the plurality
of liquid channels. In the embodiment shown, each distribution chamber in plan view
has a substantially triangular shape, with a bulbous round portion at a lower corner
of the triangle, in which an aperture is positioned. Internally, the distribution
chamber is a substantially constant width, with one or a plurality of projecting indentations
which extend into the distribution chamber there within. In plan view, the area is
substantially tapered or wedge shaped, with a circular region at one end, approximately
in the form of an acute angled triangle. This shape helps prevent "dead zones" where
the liquid flows more slowly and therefore is more vulnerable to boiling.
[0145] As shown in figure 16 on the surface of the second plate, both the first and second
plates each comprise a plurality of studs or indents 1611 distributed over the plates
in the region of the plurality of longitudinal channels. These indents are distributed
evenly in rows and columns, and when the first cell is placed adjacent to another
cell, the indents project into a gas channel formed between the cells.
[0146] Each elongate indentation is periodically modified along its length by a plurality
of discrete indentations which form projecting stud portions 1611 which project outwardly
beyond a plane joining the outermost surfaces of the longitudinal indentations on
the outside of the plate. These projecting studs have a primary function of projecting
into a passage or channel between adjacent cells through which there is a gas flow,
in order to introduce turbulence into the gas flow. The depths of the indentations
may be varied as a design parameter, to vary the amount of protrusion into the gas
channel flowing on the outside of the cell between adjacent cells. Different patterns
of studs may be provided, but in a best mode embodiment, as shown on the surface of
the second plate 1602 in figure 16, and arrangements of studs in rows and columns,
in which the studs lie on corners of a parallelogram gives an optimised turbulent
gas mixing.
[0147] In the region of the first distribution region 1613, there are a pair of indents,
which extend into the coolant flow, and similarly, in the region of the second distribution
area 1614 there are provided a pair of indents extending into the coolant flow.
[0148] The projecting or protruding studs 1611 may also have a secondary purpose of acting
as spacers between adjacent cells. However their function as spacers is not essential
for the operation of the heat exchanger, because the spacing between adjacent cells
is determined by the peripheral flange 1603 which extends around the outside of the
first plate 1601.
[0149] Referring to figure 17 herein, there is illustrated schematically a second type of
cell, which is used sandwiched between two of the first type of cells of figure 16
to make a stack of cells comprising the main body of the heat exchanger. The second
cell comprises a third plate 1700 and a second plate 1602.
[0150] Third plate 1700 is substantially similar to the first plate, but with the following
exceptions. A first end 1701 of the third plate has a hollow cutout between the laterally
extending flange portions 1702, 1703 extending either side of the first end, which,
in a stack of plates in the assembled heat exchanger forms an inlet chamber for the
gas, prior to entering between the region of the cells which contain the laterally
extending liquid coolant channels. Further, at the second end of the third plate,
there is a cutout aperture region 1704, which in the first plate is a solid sheet
of metal, but in a third plate forms an outlet passage for gas leaving the heat exchanger.
At the second end, the gas outlet aperture 1705 is bounded by a second end of the
second plate, and a peripheral skirt or flange portion 1706 which extends along an
upper and lower periphery of the second end of the third plate.
[0151] Similarly to the first cell, the third cell comprises a plurality of longitudinally
extending fluid channels 1707 formed by opposing elongate indentations in the third
plate and the second plate, alternating with a plurality of flat fin portions of the
second and third plates which are welded, and thereby separating the plurality of
adjacent elongate liquid channels inside the cell. The plurality of liquid channels
extend between a first end and a second end of the second plate, and between a first
aperture 1708 and a second aperture 1709. In the second cell, the third plate has
a first aperture 1710 and a second aperture 1711, which lineup with the first aperture
1708 of the second plate and the second aperture 1709 of the second plate respectively,
so that in the assembled heat exchanger, the first aperture is form a first liquid
coolant passage of the second aperture is form a second liquid coolant passage through
the core of the heat exchanger.
[0152] At the first end of the second plate, there is a first liquid distribution manifold
1712, formed between the material of the second plate and the third plate for channeling
liquid between the first aperture is and the first ends of the internal liquid channels;
at a second end of the second plate, there is formed a second liquid distribution
manifold 1713, which channels liquid between the second ends of the liquid carrying
channels and the second apertures. Each liquid distribution manifold comprises a substantially
flat volume, substantially triangular in plan view and having a rounded corner which
accommodates the apertures.
[0153] All other features of the second cell are identical to the corresponding features
of the first cell.
[0154] Referring to figure 18 herein, there is shown schematically in perspective view from
one side, a first outer plate 1800 of the heat exchanger for fitting to the first
side, and which forms an outer facing surface of the assembled heat exchanger. The
first outer plate comprises a substantially elongate plate of sheet metal material,
stamped out and pressed into a shape which comprises an elongate rectangle, having
at a first end a waist portion 1801 having a depth approximately 80% of a full depth
of the plate; at a second end, a rounded triangular nose section 1802; a first aperture
1803 for attachment of a second liquid carrying tube 905; a second aperture at the
second end, for attachment of a first liquid carrying tube 904; and first to fourth
anchorage points 914 -917 as previously described.
[0155] Referring to figure 19 herein, there is illustrated schematically in perspective
view, a second outer plate 1900 of the heat exchanger, which is fitted to a second
side of the heat exchanger, protecting the core cell assembly, and providing an outer
facing surface of the assembled heat exchanger. The second outer plate comprises a
substantially elongate plate of sheet metal material, stamped out pressed into a shape
consisting of an elongate rectangle having a first end 1901 and a second end 1902;
said first and comprising a narrow waist portion 1903 having a depth of around 80%
of the depth of the main central portion of the second outer plate; at a first end,
a first drain aperture 1904 which aligns with the first liquid channel inside the
core of the heat exchanger, and which is used to bleed off any gas formed in the first
liquid channel; at the second end, a second drain aperture 1905 which is used to bleed
gas from the first liquid channel if installed the other way up, and a gas outlet
aperture 1906 to which is connected to the gas outlet 923; and a second plurality
of anchor points 910 - 913, each of the second anchor points being formed in a bent
"dog leg" so that they lie in a plane parallel to and adjacent the main plane passing
through the main body of the second outer plate.
[0156] The sheet material of the first and second outer plates is preferably of thicker
but lower grade material than the sheet material of the metal used to make the heat
exchange plates inside the core of the heat exchanger.
[0157] Referring to figure 20 herein, but the shown schematically a cutaway view along the
line B - B' shown in figure 11 herein. This section shows a second end of the heat
exchanger in which a plurality of cells 2000 - 2007 are assembled into a stack to
form the main body of the heat exchanger. At the second end, the internal longitudinal
passages which carry liquid coolant flow into a liquid coolant inlet manifold section
1600 within the cell comprising a substantially flat portion of the first, second
and third plates which make up the cells. This manifold inlet section channels liquid
from the coolant inlet passage 1601 into the plurality of longitudinally extending
coolant passages extending through the main body of each cell.
[0158] As shown in cutaway view, and taking a first cell 2000 as an example, the first cell
comprises a plurality of first to thirteenth liquid carrying channels 2008 - 2020
inside the cell, arranged side by side, and separated by a plurality of fin portions
2021 - 2033. The first, fourth, seventh, tenth and thirteenth channels shown in cutaway
view in figure 20 are cut at a location where the channel is expanded to accommodate
the indents or studs. In the embodiment shown in figure 20, the studs contact each
other, but in the general case, the spacing between adjacent cells is determined by
the outer flange portions of each cell 2034 - 2041.
[0159] The two plates of each cell are welded along each fin, and around a coolant perimeter
of the second plate, so that the internal liquid carrying channels of the cell are
leak tight. Laser welding along the fins, and around the periphery of the cell gives
mechanical strength to the cell and allows the cell to operate under a high liquid
pressure.
[0160] Between adjacent cells, there are provided a plurality of gas conducting channels
2042 - 2048, through which gas flows through the heat exchanger core.
[0161] Figure 21 herein shows a section across the line B - B' in figure 11 herein, showing
an internal structure of the heat exchanger through the liquid distribution manifolds
of the cells at the second end of the heat exchanger. Preferably a width
w1 of the gas passage between adjacent cells is no less than 3mm in the main region
of the gas passage, and at the regions where the coolant inlet manifolds are present,
the width
w2 of the gas passage is no less than 2mm. This helps with the regeneration of the gas
passages, by removal of any soot or carbon deposit which might be deposited within
the gas passage.
[0162] Figure 22 herein shows a section across the line C-C' in figure 11 herein showing
an internal structure of the second heat exchanger.
[0163] Figure 23 herein shows a section across the line D-D' in figure 11 herein, showing
an internal structure of the second heat exchanger along the length of the heat exchange
cells.
[0164] Figure 24 herein shows a section across the line E-E' in figure 11, showing an internal
structure of the second heat exchanger.
Heat Transfer and Fluid Flow
[0165] An advantage of arranging the fluid flow was so that the liquid flows through the
centre of the heat exchange cells with the gas flowing between adjacent heat exchange
cells is that a full surface area of the cells which is in contact with the gas act
as heat exchange surfaces. This means that the material comprising the fins, as well
as the part of the material comprising the longitudinal coolant channels act as heat
exchange surfaces having substantially similar heat transfer characteristics. In the
case of the material comprising the indent forming the longitudinal liquid channels,
heat is transferred directly from the gas on one side of the metal, through the metal,
to the liquid coolant on the inside of the coolant channel. For gas which contacts
the fins, heat is conducted from the gas to the metal of the fins, and then transfers
by conduction laterally to the metal walls of the coolant channels, and to the coolant
flowing in those channels. The metal walls comprising the fin portions of therefore
not significantly hotter than the metal walls comprising the coolant channels.
[0166] Figure 25 herein shows a velocity contour gas flowing in a middle plane, at gas channel
7, within the second heat exchanger as gas flows from the gas inlet to the gas outlet
between adjacent cells. As shown in figure 25, each protrusion which extends into
the gas flow causes in its wake a substantially teardrop shape eddy, which promotes
turbulent mixing of the gas behind the protrusion, in the direction of main gas flow.
[0167] Figure 26 shows a velocity vector plot of gas flowing in gas channel 1, in a middle
plane view, from the gas inlet end towards the centre of the second heat exchanger.
In figure 26, gas is shown flowing from the first end of the cell to the second end.
At the first end of the gas channel on the left-hand side in figure 26, gas enters
the channel with substantially laminar flow. The gas expands laterally across a depth
of the cell, around the coolant outlet channels shown as a circle, and over the liquid
distribution manifold, into the main heat exchange area of the cell, where the plurality
of studs project into the gas channel. The plurality of studs disrupt the gas flow,
to cause turbulence, which promotes greater heat exchange between the gas and the
metal surface of the plates compared to laminar flow. Each stud creates eddies in
the gas flow which disrupt the gas flow both in the lateral direction across a depth
of the adjacent cells, and in a direction across a width of the gas channel between
cells. The coolant outlet channel also causes turbulence in its wake. Once the gas
flow is past the coolant outlet and into the main body of the core, the gas flow is
very homogeneous, having even turbulence across the whole depth of the cells.
[0168] Whilst the stud arrangement causes significant increase in turbulence in the gas
flow, and thereby increases the rate of heat transfer between the gas and the liquid
coolant, the existence of the studs in the liquid channels does not cause significant
increase in turbulence to the liquid coolant flow. Hence this means that the gas flow
has been affected, without significantly affecting the liquid coolant flow. This is
not achievable in prior art coolers having channels which have a serpentine liquid
coolant path, where introduction of turbulence creating indents into the gas channel
also introduce coolant path also introduce turbulence into the coolant channel.
[0169] Figure 27 shows a velocity vector plot of gas flowing in gas channel 1, in a middle
plane view, from the centre of the second heat exchanger towards the second end. In
figure 27, the gas flow is reversed from that shown in figure 26 (heat exchanger connected
the gas flow in the opposite direction), for the purposes of illustration. The gas
flows through the second gas passage at the second end of the cell and through the
gas passage between cells. The plurality of studs create turbulence and the gas flow,
which applies irrespective of which direction the gas flow is connected through the
heat exchanger.
[0170] Figure 28 shows a velocity vector plot at a second end of heat exchanger, viewed
in a direction perpendicular to the main planes of the heat exchange cells, showing
gas flow towards the second end of the heat exchanger, and exhaust of gas through
the gas outlet passage. At a position where adjacent cells have their coolant distribution
chambers, the gas flow is locally restricted, over part of the depth of each cell
as shown in figure 28. In figure 28, the gas is shown flowing from the first end to
the second end of the heat exchanger.
[0171] Figure 29 herein shows flow lines of gas flowing through the second heat exchanger
from the gas inlet to the gas outlet in three-dimensional view; and
[0172] Figure 30 shows a velocity vector plot of coolant flowing through a cell at the middle
plane of the cell from a coolant inlet at the second end of the second heat exchanger,
towards a coolant outlet at a first end of the second heat exchanger, and showing
mass flow fraction as a % for individual coolant channels 1 -13 across a depth of
the heat exchange cell. In figure 30, the flow of liquid passes from left to right,
but since the second plate is symmetrical, a flow in the opposite direction would
give a corresponding opposite distribution of liquid flow.
[0173] As seen in figure 30, all liquid channels have a mass flow fraction in the range
of 6.24% to 9.28% of the total liquid mass flow, the average mass flow being 7.69%
for a cell having 13 liquid channels. Hence, a maximum deviation from the average
mass flow of liquid through the channels, of the total mass flow of 7.69% is 1.59%,
or 20.7% of the average mass flow.
Gas Path
[0174] The layout of the gas path has the following features:
- 1. The height of the gas path is set by the outer joint and the cell pad heights.
The height of the gas path does not affect the coolant path other than the cell studs
cause a widening of the coolant path in a very local area.
- 2. The gas path uses a series of 'pins' or studs formed into the plate of the coolant
cell to disrupt and mix the gas flow. The positioning of these pins relative to each
other and the gas inlet and outlet is closely control to maximise heat exchange and
minimise gas pressure drop.
- 3. The geometry of the gas channels is designed to maximise the heat transfer for
a given plate unit area ie W/m2.K.kg For a given customer specification the K differential temperature of the two
fluids and the kg mass flow of the gas is set and the W is the requirement the m2 of the plate needs to be minimised to reduce weight, size and cost.
- 4. The low coolant channels and the pin alignments cause the gas to flow in substantially
a direct path from the gas inlet header to the gas outlet header.
- 5. The height of the gas path and the pins are designed to maximise the regeneration
of the engine deposits on the gas side of the cooler. This is crucial in maintaining
performance as close as possible to the original clean condition.
- a. The height of the gas path in the main flow path is at least 2mm this ensures that
there is not a small annulus that can become fully clogged from the engine deposits.
- b. The design and spacing of the pins whilst giving good gas flow disruption and gas
mixing does not have too large eddies. This allows the gas flow to effectively scavenge
the engine deposits from the plates.
- 6. The gas pressure contained within the void formed by one cell to the next exerts
a force trying to push the cells apart. This will result in the two outermost cells
having a force caused by the gas pressure trying to move the cells apart. The cells
react some of this pressure around their outer edges where each cell is joined to
the next cell. The two outer most cells react not only around the outer edge but also
in theirs centres on the two clamping plates. This arrangement allows a small amount
of relative movement between cells to take place without exceeding a safe level of
stress. This movement helps with the regeneration of the engine deposits on the gas
side of the plates.
Gas Inlet Interface
[0175] The gas inlet interface has the following features:
- 1. The gas inlet interface at the start of the coolant channels is over at least 80%
of the width of the plate.
- 2. By having at least 80% of the width of the plate the gas distribution is sufficiently
even to ensure high levels of heat exchange and low gas pressure drop.
- 3. To save on plate material scrap when forming and cutting out the plates from strip
the coolant interfaces can be placed inside the 'normal' width of the plate.
- 4. The ends of the cells form a chamber to allow the gas to flow into and from the
cooled section of the cell without restricting or channelling the gas flow. This is
important for both good gas distribution across the width of the cell and reduced
gas pressure drop.
[0176] By using the cells to form the gas headers there is a cost saving over the traditional
prior art bulkhead and over prior art formed, fabricated or cast headers welded to
the stack.
[0177] Also by replacing the prior art relatively thick walled bulkhead and gas header with
the relatively thin walled cell edge, the stresses due to differential thermal expansion
across components at or near gas temperature and components at or near coolant temperature
are much reduced.
Fabrication - External Joints
[0178] Fabrication of the second heat exchanger follows an equivalent method to the first
heat exchanger described hereinabove. Individual plates are formed by pressing. As
mentioned above, there are two basic plate shapes, being the first plate and the second
plate for construction of the cells, and to further basic plate types being the first
outer plate and the second outer plate which are of thicker material.
[0179] Taking as an example and internal cell having a first plate and the second plate
as is hereinbefore described, the second plate is positioned opposite the first plate,
touching the first plate and laser welding around a periphery of the second plate,
to weld the perimeter of the second plate to the first plate, producing a leak tight
weld. The portions of flat metal forming the fins between adjacent coolant channels
are also laser welded, but these laser welds do not need to be leak tight, since coolant
cannot escape from the coolant channels between the first and second plates due to
the peripheral weld around the second plate. The formation of the first and second
outer cells is similarly made, the only difference between the outer cells and the
inner cells in the core of the heat exchanger being the cut out areas at the locations
of the coolant inlet's and outlets, and the gas channel at the second end of the cell.
[0180] Each cell is pressure tested and visually inspected to make sure that it is robustly
welded without any leaks.
[0181] The cells are spaced apart by the peripheral skirts which extend around the outside
of the cells. When pressed together, the regions of metal around the coolant apertures
between adjacent cells touch each other, and the skirts touch each other. In some
embodiments the studs which project into the gas passages may have been designed so
as to touch each other in the finished heat exchanger also. The first and second outer
plates are fitted by pressing them to the core of the heat exchanger. Further, the
connecting members between the anchor points on the first and second plates are inserted.
The flange at the inlet end of the heat exchanger is located around the open ends
of the cells. The outer flange helps to locate the first ends of the cells together.
The assembled heat exchanger can be held together in a clamp, or under a press or
mass for the next operation of brazing or soldering.
[0182] The whole assembly is brazed or soldered by soldering around the outer flanges connecting
them together, and soldering inside the coolant passages, soldering the coolant apertures
of adjacent cells to each other, brazing or soldering the peripheral flanges or skirts
to each other, and brazing or soldering the end flange at the first end of the heat
exchanger. At the same time, the outer plates are brazed or soldered to the core,
by brazing or soldering the flanges and, where present, around a perimeter of any
coolant apertures and gas apertures.
[0183] The coolant inlet and outlet tubes are fitted and brazed or soldered to the coolant
inlet and outlet passages.
[0184] After assembly, the whole heat exchanger is visually inspected for defects in brazing
or soldering, and if any are found, those defects areas can be rectified by further
brazing or soldering. The whole assembled heat exchanger may be gas pressure tested.
[0185] There are two types of cell to cell joint:
a. A round joint joining one coolant interface to the next coolant interface.
b. An edge or skirt joint sealing one cell to the next cell and enclosing the gas
path.
[0186] The round cell to cell joint is visible and accessible from the coolant inlet/outlet
hole on the outer most cell. Thus it can be reworked as a final assembly.
[0187] The edge joint of the skirt is an external joint and is both easily visible and re-workable.
[0188] By this design all joints that are not checked and inspected as subassemblies can
be reworked as a final assembly.
The Case and Bulkhead.
[0189] Prior art coolers have a case that encloses the coolant that flows around tubes or
plates that carry the gas.
[0190] Coolant pressure on the case applies a force on the case trying to expand the case.
This force is to some extent transferred to the prior art traditional coolers bulkhead.
The coolant is also applying a force to the bulkhead of a traditional prior art cooler
pushing the bulkheads out of the cooler.
[0191] A prior art cooler with a case and either tubes or plates has a temperature differential
between the case and the tubes or plates. The case temperature will be slightly lower
than coolant temperature due to heat loss to the ambient. The tubes or plates will
be above coolant temperature due to the heat transferred from the gas. A traditional
prior art cooler will have forces on the bulkhead caused by the differential expansion
of the tubes or plates and the case.
[0192] The stresses due to coolant pressure and differential expansion combine with the
thermal stresses at the gas inlet bulkhead to cause potentially damaging levels of
stress. This is an area of failure typically seen on a prior art traditional cooler.
[0193] The novel design disclosed herein, having no case or bulkhead, and as discussed earlier
lowers thermal stress at the gas inlet, removes this typical cause of failure.
[0194] The above embodiment heat exchangers may provide an improved heat exchanger compared
to prior art types, and which have a relatively lower gas pressure drop compared to
conventional gas to liquid heat exchangers, which have reduced volume for a specified
amount of cooling capacity, and which have lower weight, for a specified amount of
cooling capacity due to the reduced amount of liquid coolant within the heat exchanger.
[0195] The above embodiment heat exchangers effectively provide a decoupling of gas flow
design from liquid flow, so that the liquid flow direction can be reversed through
the heat exchanger without significantly affecting the rate of heat transfer from
the gas to liquid. This means that both the liquid and the gas can be fed through
the heat exchanger in the same direction, or in opposite directions in any combination
without significantly affecting the heat transfer performance of the heat exchanger.
The features which give rise to this versatility include the studs which project into
the gas channel, containment of the liquid coolant within the cells, and the symmetry
of the second plates which allow passage of coolant from either end with no significant
difference in coolant flow characteristics. The presence of the stud features, which
are formed as part of the indentations which form the liquid coolant channels, does
not significantly affect the flow of coolant in the liquid coolant channels. The studs
produce a disproportionate amount of turbulence in the gas flow, compared to the amount
of turbulence that they produce and the liquid flow. Turbulence the liquid flow is
of no particular advantage since it does not materially affect heat transfer rate,
whereas turbulent and the gas flow significantly increase its heat transfer rate.
Therefore, the studs improve heat transfer rate from the gas to liquid, without introducing
significant turbulence and pressure drop into the liquid flow, and additional wasted
coolant volume
[0196] Further, the heat exchangers are of a modular design, which can include a lesser
or greater number of cells in the core to provide a reduced or increased heat transfer
capacity as required, without significant changes to manufacturing process.
1. A gas to liquid coolant heat exchanger for transferring heat between a gas and a liquid
coolant, said heat exchanger comprising:
a plurality of heat exchange cells;
each said cell comprising a liquid coolant inlet and a liquid coolant outlet;
each said cell comprising a pair of plates each said plate having a plurality of grooves
which form a plurality of liquid coolant channels between said plates, extending between
said liquid coolant inlet and liquid coolant outlet;
characterised in that
each said cell contains said liquid coolant within said cell between said pair of
plates.
2. The heat exchanger as claimed in claim 1, wherein said plurality of liquid coolant
channels extend substantially parallel to a main length of said cell.
3. The heat exchanger as claimed in any one of the preceding claims, wherein an inner
perimeter of one of said plates is joined to the other one of said plates, to form
a liquid tight seal for containing liquid within said cell, and wherein said liquid
coolant can enter or exit said heat exchange cell only through said liquid inlet and
outlet.
4. A heat exchanger as claimed in any one of the preceding claims, wherein:
a said heat exchange cell comprises a distribution manifold for distributing said
coolant between a said coolant inlet, and a said plurality of liquid coolant channels
within said cell,
characterised in that said distribution manifold is arranged to control and direct the flow of said liquid
coolant such that there is adequate flow of said coolant across a gas inlet interface
to reduce and/or eliminate the occurrence of said coolant boiling.
5. A heat exchanger as claimed in any one of the preceding claims, wherein said cells
are designed to control and direct the flow of coolant such that there is adequate
flow of coolant in all the longitudinal coolant channels to reduce and eliminate the
occurrence of coolant boiling.
6. A heat exchanger as claimed in any one of the preceding claims, wherein said cells
are designed to minimise a volume of coolant within the heat exchanger, relative to
a gas flow capacity of said heat exchanger.
7. A heat exchanger as claimed in any one of the preceding claims, which 'decouples'
the geometry of the coolant side and the gas side of a heat exchanger such that the
coolant performance and the gas performance can be maximised substantially independently
of each other.
8. A heat exchanger as claimed in any one of the preceding claims which has a heat exchange
capacity of >0.25 W/m2.K.kg, at 98% effective or greater, whilst having low pressure drop.
9. A heat exchanger as claimed in any one of the preceding claims wherein in a main part
of the heat exchanger, both said gas and said liquid each flow in paths which follow
a substantially longitudinal direction along a main length of said heat exchanger.
10. A heat exchanger as claimed in any one of the preceding claims which has no outer
casing, no bulkhead, and no separate gas header.
11. A heat exchanger as claimed in any one of the preceding claims, comprising a gas inlet
and a gas outlet, wherein each one of said gas inlet and said gas outlet is capable
of interfacing in either a longitudinal direction relative to a main length direction
of said heat exchanger, or perpendicularly relative to said main length direction.
12. A heat exchanger as claimed in any one of the preceding claims, comprising a coolant
passage which can be used as a coolant inlet or outlet passage,
characterised in that the coolant is able to vent any gas formed within said coolant within said coolant
passage.
13. A heat exchange cell for a gas to liquid heat exchanger as claimed in any one of the
preceding claims, said cell comprising:
a first plate and a second plate;
at least one of said plates having a plurality of grooves which form a plurality of
liquid coolant channels between said plates,
characterised in that
each said cell contains said liquid coolant within said cell between said plates.
14. The heat exchange cell as claimed in claim 13, wherein an outer perimeter of said
second plate fits within an outer perimeter of said first plate, and said outer perimeter
of said second plate is sealed to said first plate by a continuous weld extending
around said outer perimeter of said second plate.
15. The heat exchange cell as claimed in claim 13 or 14, comprising a plurality of fin
regions located between said plurality of grooves, wherein said pair of plates are
welded to each other along said fin regions.
16. The heat exchange cell as claimed in any one of claims 13 to 15, comprising a liquid
inlet and a liquid outlet, for allowing liquid into and out of a cavity between said
first and second plates, said liquid inlet and outlet being located within an area
bounded by an outer perimeter of said second plate.
17. The heat exchanger as claimed into any one of claims 13 to 16, comprising a liquid
distribution chamber for distributing liquid from or to a liquid inlet or outlet and
said plurality of liquid coolant channels inside said cell, wherein said liquid distribution
chamber distributes liquid between said plurality of coolant channels such that difference
in mass flow of liquid between a liquid coolant channel having a lowest mass flow
and a liquid channel having a highest mass flow is no more than 23% of the mass flow
of the average channel mass flow.
18. A gas to liquid heat exchanger as claimed in any one of the preceding claims comprising:
a plurality of heat exchange cells, each said cell comprising a first plate and a
second plate;
wherein each said heat exchange cell comprises a liquid inlet aperture and a liquid
outlet aperture;
each said plate comprising a sealed outer perimeter, and a plurality of internal fluid
channels;
each heat exchange cell having its coolant perimeter sealed independently of the coolant
perimeter of each other said heat exchange cell;
said plurality of heat exchange cells arranged side-by-side in a stack arrangement;
wherein said plurality of heat exchange cells are sealed to each other by an outer
perimeter seal around their respective outer perimeters, to form a plurality of gas
channels extending between said plurality of cells.
19. The heat exchanger as claimed in claim 18, wherein said plurality of heat exchange
cells are sealed to each other by a liquid inlet seal, which joins the respective
inlets of the heat exchange plates together to form a liquid inlet passage.
20. The heat exchanger as claimed in claim 18 or 19, wherein said plurality of heat exchange
cells are sealed to each other by a liquid outlet seal, which joins the respective
outlets of said heat exchange plates together. To form a liquid outlet passage.
21. The heat exchanger as claimed in claim 18, wherein each said cell comprises an inlet
aperture and an outlet aperture; and
said plurality of heat exchange cells are sealed to each other by an inlet seal, which
joins the respective inlets of the plurality of heat exchange plates together to form
a common inlet passage; and
said plurality of heat exchange cells are sealed each other by an outlet seal, which
joins the respective outlets of said heat exchange plates together to form a common
outlet passage; and
said plurality of cells are joined together and said inlet seals, said outlet seals
and said outer perimeter seal formed in a single sealing operation.
22. The heat exchanger as claimed in any one of claims 18 to 21, wherein a fluid connector
for connecting said heat exchanger to a fluid circuit comprises a tubular collar brazed
or soldered to a region around a perimeter of an aperture in a said plate, said region
presented on an outer plate of said heat exchanger.
23. A method of manufacture of a gas to liquid coolant heat exchanger as claimed in claim
1, said method comprising:
individually forming each of said plurality of heat exchange cells, each comprising
a respective first plate and a second plate, by joining said first and second plates
together with a continuous joint extending around a perimeter of said second plate
to form a cavity between said second plate and said first plate, through which a liquid
coolant may flow;
individually testing each said cell to check for fluid leaks in said cavity;
joining said plurality of individual heat exchange cells together by placing said
plurality of cells into an assembly of cells;
forming an outer joint around said plurality of cell perimeters;
forming an inlet joint joining together a plurality of inlets of said cells, and
forming an outlet joint by joining together a plurality of outlets of said plurality
of cells.
24. The method as claimed in claim 23, further comprising leak testing said assembly of
cells.
25. The method as claimed in claim 23 or 24, wherein said process of individually forming
said cell comprises performing a plurality of second joints between said first and
second cells, said second joints located between a plurality of grooves in said first
and second plates, which form a plurality of liquid channels in said cavity, and within
an area bounded by said continuous joint.
26. The method as claimed in any one of claims 23 to 25, wherein each said heat exchange
cell is formed by:
forming a said first plate and a said second plate;
arranging said first and second plates so as to lie opposite each other;
joining said second plate to said first plate by forming a continuous joint around
a perimeter of said second plate; and
joining said first and second plates at a plurality of locations over a region extending
within said perimeter of said second plate.
27. The method as claimed in any one of claims 23 to 26, wherein said plurality of cells
are joined together by brazing or soldering.
28. The method as claimed in any one of claims 23 to 27, wherein said first and second
plates are joined together by laser welding or by resistance welding.
29. The method as claimed in any one of claims 22 to 27, further comprising pressure testing
each said cell to check for leaks in said perimeter joints, prior to assembling said
plurality of heat exchange cells together.
30. The method as claimed in any one of claims 23 to 29 further comprising pressure testing
the complete heat exchanger assembly after the formation of said outer perimeter joint
around said plurality of cells and after the formation of said inlet joint and said
outlet joint.
31. The method as claimed in any one of claims 23 to 30, further comprising:
locating a tubular collar at a region around a perimeter of an aperture in a said
plate, said region presented on an outer face of said heat exchanger;
brazing or soldering said collar to said plate to form an attachment point for attaching
a coolant inlet or outlet tube.
32. A heat exchange cell for a gas to liquid heat exchanger as claimed in claim 1, said
cell comprising:
a first plate and a second plate;
at least one of said first and second plates comprising a plurality of elongate grooves,
said plurality of grooves forming a plurality of liquid coolant channels inside said
cell;
at least one of said first and/or second plates having a plurality of outwardly projecting
studs, which project in a direction outwardly from a plane which intersects an outer
surface of a said plate at the position of said plurality of grooves.
33. The heat exchange cell as claimed in claim 32, wherein each said groove is formed
in a plate wall of a said first and/or second plate, and said plurality of projecting
studs comprise indents within a said groove.
34. The heat exchange cell as claimed in claim 32 or 33, wherein said studs comprise substantially
circular indents.
35. The heat exchange cell as claimed in any one of claims 32 to 34, wherein said studs
have a substantially mesa shape.
36. The heat exchange cell as claimed in any one of claims 32 to 35, wherein said plurality
of studs are arranged in a regular two-dimensional grid pattern in a plurality of
rows and columns.
37. The heat exchange cell as claimed in any one of claims 32 to 36, wherein said plurality
studs are arranged in a substantially rhomboid pattern.
38. The heat exchange cell as claimed in any one of claims 32 to 37, wherein said second
plate is welded to said first plate around a perimeter of said second plate, to form
a leak tight fluid containing chamber between said first and second plates.
39. The heat exchange cell as claimed in any one of claims 32 to 38, wherein said plurality
of grooves extend approximately parallel to each other, and said first and second
plates are joined together by welding between said grooves.
40. The heat exchange cell as claimed in any one of claims 32 to 39, comprising first
and second liquid distribution regions located respective first and second ends of
said cell, for channelling liquid from a liquid inlet or to a liquid outlet and to
a plurality of liquid channels extending along said heat exchange cell, wherein a
said liquid distribution region is designed to extend across a full depth of said
cell so as to distribute liquid volume substantially evenly across said plurality
of liquid channels.
41. The heat exchange cell as claimed in any one of claims 32 to 40, comprising one or
more liquid distribution regions located at one or both ends of said cell, said liquid
distribution regions each comprising a volume having a substantially constant internal
width, between said first and second plates, and a substantially wedge or tapered
area.
42. A gas to liquid heat exchanger as claimed in claim 1, comprising a plurality of heat
exchange cells,
each said cell comprising an inner plate and an outer plate;
said plurality of heat exchange cells being stacked together side-by-side to form
a plurality of gas passages there between;
each said cell having an outer surface comprising a plurality of protrusions which
extend into said gas passages between said cells, for promoting turbulent gas flow
between said cells.
43. The gas to liquid heat exchanger as claimed in claim 42, wherein said plurality of
protrusions are arranged in a regular two-dimensional grid pattern in a plurality
of rows and columns.
44. The gas to liquid heat exchanger as claimed in claim 42 or 43, wherein said plurality
protrusions are arranged in a rhomboid pattern.
45. The gas to liquid heat exchanger as claimed in any one of claims 42 to 44, wherein
said gas passages are bounded by first and second planes, each of which intersect
respective outer walls of adjacent said cells at the position of a plurality of elongate
liquid coolant channels, and wherein a distance between said first and second planes
is no less than 2mm, except in regions where one or a plurality of studs are present.
46. The gas to liquid heat exchanger as claimed in any one of claims 42 to 45, characterised in that a liquid flow pattern of liquid flowing through the centres of said cells is independent
of and decoupled from a gas flow pattern of gas flowing between said cells.
47. The gas to liquid heat exchanger as claimed in any one of claims 42 to 46, wherein
said plurality of protrusions cause substantially teardrop shaped eddies in said gas
flow.