TECHNICAL FIELD
[0001] This invention relates to automotive heat exchangers in general, and specifically
to a liquid flow heat exchanger, such as a radiator, with a novel in tank structure
for reducing the pressure drop caused by flow turning losses.
BACKGROUND OF THE INVENTION
[0002] Automotive heat exchangers that use a pumped, liquid heat exchange medium, as opposed
to a compressed gaseous/liquid heat exchange medium, include radiators and heaters.
Typically, these include two elongated manifolds or header tanks, one on each side
of the heat exchanger, with a central core consisting of a plurality of evenly spaced,
flattened flow tubes and interleaved corrugated air fins running between the two tanks.
Each tank is generally box shaped, with parallel side walls, a back wall joining the
side walls, two axially opposed ends, and an open area opposite the back wall, which
is eventually closed off when it is fixed leak tight to one side of the core. Each
header tank distributes pumped liquid to or from the flow tubes in the core, and is
in turn filled or drained by an inlet or outlet pipe opening into the header tank
at a discrete location. In typical radiators, the inlet or outlet pipe to the header
tank is oriented both transversely to the length of the tank and to the flow tubes.
Coolant flow entering the inlet pipe must, therefore, turn through a substantial angle
toward the two ends of the tank before as well as turning substantially again to flow
out of the tank interior and into the flow tubes. The converse is true for coolant
exiting the return tank through the outlet pipe. An example of a recent radiator with
molded plastic, box shaped header tanks may be seen in
U.S. Pat. No. 5,762,130, which is fairly typical in its basic flow configuration, apart from being a U flow
design, with the inlet and outlet pipe located on one tank. The orientation of the
pipes relative to the tank walls and flow tubes is as described above, however. A
metal design is shown in
U.S. Patent No. 6,283,200 wherein the end of the inlet pipe is flared outwardly to reduce the pressure loss.
[0003] The design of a radiator or any cross flow heat exchanger with a liquid medium flowing
in one direction through flow tubes, and with air blown perpendicularly across the
flow tubes, is a compromise between heat exchange efficiency between the two flowing
media, and the pressure or pumping losses of the two media. For example, it is well
known that decreasing the flow passage cross sectional area will present relatively
more surface area of the fluid medium within the flow passage to the air blowing over
the flow tube, increasing the heat transfer efficiency from fluid to air. A tube that
is smaller on the inside is also thinner on the outside, and so presents less obstruction
the air blown over the outside of it, decreasing the air side pressure loss through
the core. However, a thinner flow tube creates more fluid pressure loss through the
tube, end to end. Some compromise can generally be found between airside pressure
drop, tube thickness, and liquid (coolant) pressure drop. However, the ability to
reduce total coolant pressure loss (pumping loss) elsewhere in the heat exchanger
would allow the use of thinner tubes in general, which would be very positive, considering
that thinner tubes also decrease air side pressure loss.
[0004] One source of coolant pressure drop through the heat exchanger that has not received
a great deal of attention in the prior art is turbulence or "turning" losses that
occur at the transition between the pipe opening and the enclosed interior of the
header tank. That is, since the inlet pipe typically enters through a tank side wall,
and not the tank back wall, it is oriented transversely to the flow tubes, as well,
and must change direction both to reach the opposite ends of the tank and in order
to flow into the tubes. The turning transition is not a great source of pressure loss
when the interior volume of the tanks is large, since a large interior volume can
act as a large pressure reservoir to "absorb" and distribute coolant to the flow tubes.
As available underhood space shrinks, however, radiator header tanks become smaller,
and the parallel sidewalls become closer. Flow exiting the opening of the inlet pipe
(through the first side wall) impinges on the proximate, opposed second side wall,
creating turbulence and pressure loss before it can be distributed toward the opposite
ends of the tank and into the flow tubes.
[0005] The other liquid medium heat exchanger typically found in an automobile, the heater
core, has a similar cross flow configuration, but faces a different problem. There,
the inlet pipe generally opens through the back wall of the header tank, in line with,
rather than perpendicular to, the flow tubes. The flow thus impinges directly onto
the ends of the nearest aligned flow tubes, rather than against a sidewall of the
tank, which would theoretically be positive, in terms of direct flow into the tubes
with minimal pressure loss. However, the fact that the ends of the nearest tubes are
in line with the inlet pipe is a detriment, because the force of the impinging flow
against the near tube ends causes erosion and damage. Therefore, it has been proposed
in several heater core designs to place a protective tent or baffle like structure
between the inlet pipe opening and the ends of the nearest aligned flow tubes. These
act as a road block, in effect, interrupting the flow at that point, rather than smoothing
it out, and would actually increase total coolant pressure drop across the core. This
is an acceptable price in that context, however, since it is considered necessary
to protect the otherwise eroded tubes. Another solution is shown in U. S. Patent
6,116,335 to Beamer et al wherein a flow turning structure is molded into the inlet header tank opposite to
the inlet pipe.
[0006] Design of tanks and manifolds in automotive heat exchangers such as radiators involves
tradeoffs between the conflicting requirements of minimizing coolant pressure drop
and packaging space. Market trends are simultaneously driving down the allowable tank
size and pressure drop. This problem is further compounded when internal oil coolers
or baffles are required that partially block the inlet/outlet pipes.
[0007] Plate type oil coolers are frequently incorporated in radiator tanks to provide engine
and transmission oil cooling. Due to packaging constraints, it is common for oil coolers
to straddle the coolant inlet/outlet pipes. This flow blockage increases coolant pressure
drop and creates local regions of high coolant velocity that can cause erosion corrosion
of the oil cooler. In a typical cross flow radiator, the tanks and oil cooler represent
50% of the total coolant pressure drop. The penalty due to the oil cooler blockage
is 35-40% of the tank pressure drop (~20% of total pressure drop).
[0008] Since the pipe diameters are specified by the vehicle manufacture, the most common
method used to limit the oil cooler coolant pressure drop penalty is the spacing (stand
off height) of the oil cooler from the inside tank wall. Typically it is not practical
to reduce the pressure drop penalty below the levels described above because the increased
stand off height required will reduce the size of oil cooler that can be installed
in the tank, or a larger tank must be used with increased packaging space, mass, and
cost penalties.
[0009] For sheet metal tanks and pipes, the internal juncture between the pipe and tank
is typically sharp edged. Due to the joint design, the pipe is frequently extended
into the tank to allow secure clinching of the pipe to the tank. Both the sharp edge
and pipe extension act to increase coolant pressure drop.
SUMMARY OF THE INVENTION
[0010] The subject invention provides a radiator header tank to pipe joint that reduces
coolant pressure drop by reducing turning losses at the transition between the pipe
and the header tank wall.
[0011] The heat exchanger assembly of the subject invention is distinguished by a transition
between the header wall and the pipe extending transition completely around the opening
to present an expanding flow control surface between from the header wall to the pipe
for conveying the heat exchange medium closely over the control surface between the
tank interior and the pipe to reduce turbulence and pressure loss at the transition
between the tank interior the said pipe.
[0012] This invention provides a transition to significantly reduce the oil cooler pressure
drop penalty and/or reduce the size of the tank. A method of determining the required
feature size and practical designs are provided for integrally molded or fabricated
sheet metal tanks. Several configurations are shown that incorporate an internal radius
or chamfer to eliminate the pipe extension inside the tank.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Other advantages of the present invention will be readily appreciated as the same
becomes better understood by reference to the following detailed description when
considered in connection with the accompanying drawings wherein:
Figure 1 is a fragmentary view of a heat exchanger showing a header tank and heat
exchanger core;
Figure 2 is an interior perspective view of the heat exchanger header tank of Figure
1;
Figure 3 is schematic showing the flow pattern for a sharp edged pipe to header joint
of the prior art;
Figure 4 is schematic showing the flow pattern for a chamfered header to pipe transition
of the subject invention;
Figure 5 is a schematic view comparing the radius and chamfered joints of the subject
invention; and
Figure 6 is a perspective view of a header tank incorporating an oil cooler facing
an inlet configured in accordance with Figure 4;
Figure 7 is a plot of the chamfer/radius size versus the pressure drop for a given
inlet diameter;
Figure 8 is a plot of the taper angle versus pressure drop with a given chamber angle
and pipe size;
Figure 9 is a plot of chamfer versus pressure drop for various pipe diameters and
stand off heights;
Figure 10 is a plot of radius versus pressure drop for a given pipe size and various
stand-off heights;
Figures 11 through 16 show various pipe to header joints constructed in accordance
with the subject invention.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0014] A heat exchanger assembly constructed in accordance with the subject invention is
generally shown at
20 in Figures 1 and 2. The assembly
20 includes a core comprising a plurality of flow tubes
22 having heat exchange fins
24 extending therebetween. A header tank
26 distributes a flowing liquid heat exchange medium to and from the flow tubes
22 and presents a header wall
28 with an interior surface. A pipe
30 is disposed in an opening through the header wall
28.
[0015] A joint extends between the pipe
30 and the header wall
28 to define an endless transition completely around the opening to present an expanding
flow control surface between the pipe
30 and the interior surface
32 of the header wall
28 for conveying the heat exchange medium closely over the control surface between the
interior surface and the pipe
30 to reduce turbulence and pressure loss at the transition between the interior surface
and the pipe
30.
[0016] A typical pipe to header wall joint is shown in Figure 3 wherein a sharp edged corner
is presented annularly about the opening into the header wall
28. The pipe is formed in a cylindrical shape to define entry flow into the header as
cylindrical. However, it is to be understood that the cylindrical pipe could be flattened
into an oval, elliptical, or other shape at the joint. The joint of the subject invention
presents an expanding flow control surface with a rounded radius
32 or a straight or conical shaped chamfer
34 as illustrated in Figure 4. The use of a chamfer
34 is slightly more effective than the radius
32 due to increased entrance flow area for the same size pipe flow area as shown in
Figure 5.
[0017] The typical pipe/tank juncture is a sharp edged corner as illustrated in Figure 3.
The limiting entrance flow area into the pipe is a cylinder. This invention replaces
the sharp corner with a radius or chamfer to increase entrance flow area and facilitate
turning of the flow into the pipe. Flow streamlines for both sharp and chamfered geometry's
are shown in figures 3 and 4. Use of a chamfer is slightly more effective than a radius
due to increased entrance flow area for the same size feature as shown in Figures
5 and 7. The optimum chamfer angle was found to be 45° as shown in Figure 8.
[0018] Based on CFD simulation and prototype testing it was found that the effect of radius/chamfer
size is similar through out the practical range of pipe and standoff sizes. A radius/chamfer
of 2.0 mm yields approximately 50% of the total savings possible as shown in Figures
9 and 10. Therefore this invention claims the use of a radius or 30/60° chamfer equal
to or greater than 2.0 mm.
[0019] Accordingly, the pipe
30 is cylindrical about an axis and the flow control surface expands radially as it
opens axially into the interior surface
32 of the header wall
28, it expanding through a radius or through a cone shaped chamfer. The header wall
28 presents a planar disk-like portion immediately adjacent to and extending radially
from the opening in the header wall
28 to define the interior surface
32 in a radial plane. In all cases, the control surface blends into the planar disk-like
portion to present a smooth transition of the control surface from the pipe
30 into the interior surface
32 of the header wall
28. It is important that the control surface blend into the planar interior surface 32
to present a smooth transition of the control surface from the pipe
30 into the interior surface
32 of the header wall
28. As alluded to above, the control surface may extend through a radius
32 or through a cone to define a chamfer
34. Referring to Figure 6, the pipe
30 is integrally formed of plastic material with the header wall
28 define the chamfered control surface
34 that expands to the radial plane of the interior surface
32 of the header wall
28. An oil cooler
36 is disposed opposite to the pipe
30. The chamfer
34 significantly reduces the pressure drop caused by the imposition of the oil cooler
36.
[0020] Referring to Figures 11-16, the header wall
28 defines the control surface and the control surface expands from a cylindrical collar
40 to the radial plane of the interior surface
32. Said another way, the header wall
28 extends through a transition control surface into a cylindrical collar
40, which receives the pipe
30.
[0021] In the Figures 11 and 12, the pipe
30 extends within the opening of the collar
40 and terminates in an annular edge
38. The header wall
28 extends into the axially extending collar
40 to surround and engage the pipe
30. The pipe
30 includes a bead
42 abutting the open end of the collar
40.
[0022] Accordance with the invention, the pipe
30 has an end which terminates in spaced relationship to the radial plane in the header
wall
28.
[0023] In Figures 13-16, the pipe
30 is disposed about the exterior of the collar
40.
[0024] In Figure 13, the pipe
30 is flared
48 outwardly into a flare to engage the exterior of the collar
40 defining the control surface.
[0025] In Figures 14 and 15, the pipe
30 includes an enlarged end
50 defining a shoulder
52 for surrounding and engaging the exterior of the collar
40 with the shoulder
52 abutting the collar
40. The only difference in Figure 15 is that the pipe
30 and the collar
40 are forced radially into one another to create a mechanically overlapping connection
in the axial direction.
[0026] In Figure 16, the pipe
30 and the collar
40 include mating undulations
54 extending annularly thereabout for locking the pipe
30 to the collar
40 to create a mechanically overlapping connection in the axial direction.
[0027] It is to be understood that the various embodiments may employ the radius
32 shown in Figures 12-14 and 16 or the chamfer
34 shown in Figures 11 and 15 and that either may be used with the various species of
Figures 11-16. The joint may be formed with a radiused or chamfered flange and may
be secured by fixturing, staking, tack weld, or spin welding, prior to final bonding.
The pipe
30 end may be expanded to engage the outside surface of the collar or flange
40 as illustrated in Figures 11-12. A feature can be added to the end of the pipe
30 to provide lead in.
[0028] The pipe
30 and the header wall
28 may be molded of an organic polymeric material (plastic) or formed of sheet metal,
when of metal, the pipe
30 may be secured to the tank
26 prior to brazing by expanding the collar
40 into the pipe
30. Alternately, as illustrated in Figures 13-16, the pipe
30 can be a press fit on to the collar
40, or can be shrunk onto the collar
40. Either the collar
40 or the pipe
30 can be tapered to control the press fit characteristics. The collar
40 can be expanded into the pipe
30 or the pipe
30 shrunk on to the collar
40. The bead
42 may be formed into the pipe
30 and the collar expanded into the bead
42. All configurations allow the use of an unclad pipe
30 and externally clad tank
26. All configurations are designed to allow brazing of the pipe
30 and collar. Typically clad material is used for the tank
26 body and bare material for the pipe
30, but either or both parts can be clad. Alternately, a separate source of braze material
can be used such as a braze ring or braze paste. Some of the configurations could
also be spin welded. In the case of plastics, the pipe
30 may be mechanically attached or bonded to the collar
40, as by an adhesive, fusion or spin welding or integrally molded.
[0029] The collar
40 and the pipe
30 may be bonded together by brazing, soldering, welding or an adhesive, depending upon
the composition of the components. In addition, the pipe
30 may be secured prior to bonding to the collar
40 by fixturing, a press fit, e.g., expanding or shrinking, staking, forming undulations,
etc. In order to facilitate assembly, the pipe
30 and/or collar
40 may include a lead-in such as a taper, or the locating bead
42 or shoulder
52.
[0030] Obviously, many modifications and variations of the present invention are possible
in light of the above teachings. The invention may be practiced otherwise than as
specifically described within the scope of the appended claims.
1. A heat exchanger assembly comprising;
a plurality of flow tubes (22),
a header tank (26) for distributing a flowing liquid heat exchange medium to and from said flow tubes
(22) and presenting a header wall (28) with an interior surface (32),
a pipe (30) disposed in an opening through said header wall (28), and
a transition by extending said header wall (28) into said pipe (30) around said opening to present an expanding flow control surface between said pipe
(30) and said interior surface (32) of said header wall (28) for conveying the heat exchange medium closely over said control surface between
said interior surface and said pipe (30) to reduce turbulence and pressure loss at said transition between said interior surface
and said pipe (30).
2. An assembly as set forth in claim 1 wherein said flow control surface is internal
with said header wall (28) and expands radially as it opens axially into said interior surface (32) of said header wall (28).
3. An assembly as set forth in claim 2 wherein said flow control surface extends in a
circle about an axis for defining a collar (40) for receiving said pipe (30).
4. An assembly as set forth in claim 2 wherein said control surface extends through a
radius (32).
5. An assembly as set forth in claim 2 wherein said control surface extends through a
cone to define a chamfer (34).
6. An assembly as set forth in claim 2 wherein said pipe (30) and said header wall (28) comprise an organic polymeric material.
7. An assembly as set forth in claim 2 wherein said pipe (30) and said header wall (28) comprise metal.
8. An assembly as set forth in claim 3 wherein said pipe (30) terminates in spaced relationship to the plane of said header wall (28).
9. An assembly as set forth in claim 3 wherein said pipe (30) includes a bead (42) abutting said collar (40).
10. An assembly as set forth in claim 3 wherein said collar (40) and said pipe (30) are bonded together.
11. An assembly as set forth in claim 10 wherein said pipe (30) is secured prior to bonding to said collar (46).
12. An assembly as set forth in claim 3 wherein said pipe (30) is flared (48) outwardly and engages the exterior of said collar (46) defining said control surface.
13. An assembly as set forth in claim 12 wherein said pipe (30) includes an enlarged end (50) defining a shoulder (52) for surrounding and engaging the exterior of said collar (46) with said shoulder (52) abutting said collar (46).
14. An assembly as set forth in claim 12 wherein said pipe (30) and said collar (46) include mating undulations (54) extending annularly thereabout for locking said pipe (30) to said collar (46).
15. An assembly as set forth in claim 4 wherein said control surface presents a smooth
transition from said pipe (30) into said interior surface (32) of said header wall (28) with a radius or a 30°to 60° chamfer equal to or greater than 2.0mm
16. An assembly as set forth in claim 5 wherein said control surface presents a smooth
transition from said pipe (30) into said interior surface (32) of said header wall (28) with a radius or a 30 to 60 chamfer equal to or greater than 2.0 mm.