Title of Invention

HEAT TRANSFER TUBE

Abstract A heat transfer tube (10) has an inner surface (12) and an outer surface, wherein the inner surface comprises a plurality of primary fins (12), a plurality of intermediate fins (26), and a plurality of grooves (24) defined by adjacent primary fins, and the intermediate fins (20) are positioned in at least some of the grooves (24).
Full Text HEAT TRANSFER TUBE
Field of the Invention
The present invention relates to heat transfer tubes that may be used in
heat exchangers and other components in air conditioners, refrigerators and
other such devices. The present invention relates more particularly to heat
transfer tubes having grooved inner surfaces that form fins along the inner
surface of the tubes for improved heat transfer performance.
Background of the Invention
Heat transfer tubes with grooved inner surfaces are used primarily as
evaporator tubes or condenser tubes in heat exchangers for air conditioning and
refrigeration. It is known to provide heat transfer tubes with grooves and
alternating "fins" on their inner surfaces. The grooves and the fins cooperate to
enhance turbulence of fluid heat transfer mediums, such as refrigerants,
delivered within the tube. This turbulence enhances heat transfer performance.
The grooves and fins also provide extra surface area and capillary effects for
additional heat exchange. This basic premise is taught in U.S. Patent No.
3,847,212 to Withers, Jr. et al.
It is further known in the art to provide internally enhanced
heat exchange tubes made by differing methods; namely - seamless
tubes and welded tubes. A seamless tube may include internal fins and
grooves produced by passing a circular grooved member through the interior of
the seamless tube to create fins on the inner surface of the tube. However, the
shape and height of the resulting fins are limited by the contour of the circular

member and method of formation. Accordingly, the heat transfer potential of
such tubes is also limited.
A welded tube, however, is made by forming a fiat workpiece into a
circular shape and men welding the edges to form a tube. Since the workpiece
may be worked before formation when flat, the potential for varying fin
height, shape and various other parameters is increased. Accordingly, the heat
transfer potential of such tubes is also increased.
This method of tube formation is disclosed in U.S. Patent No.
5,704,424 to Kohn,, et al. Kohn, et al. discloses a welded heat transfer tube
having a grooved inner surface. In the described and claimed production
method, a flat metallic board material is rounded in the lateral direction until
the side edges are brought into contact with each other. At that point, the two
edges of the board material are electrically seam welded together to form the
completed tube. As stated therein, an advantage of this method is that any
internal fins or grooves can be embossed onto one side of the tube while the
metallic board is still flat, thereby permitting increased freedom of design
attributes.
Such design freedom is a key consideration in heat transfer tube
design. It is a common goal to increase heat exchange performance by
changing the pattern, shapes and sizes of grooves and fins of a tube. To that
end, tube manufacturers have gone to great expense to experiment with
alternative designs. For example, U.S. Patent No. 5,791,405 to Takima et al.
discloses a tube having grooved inner surfaces that have fins formed
consecutively in a circumferential direction on the inner surface of the tube.
A plurality of configurations are shown in the various drawing figures. U.S.
Patent Nos. 5,332,034 and 5,458,191 to Chiang et al. and U.S Patent No.
5,975.196 to Gaffaney et al. all disclose a variation of this design referred to
in this application as a cross-cut design. Fins are formed on the inner tube
surface with a first embossing roller. A second embossing roller then makes


cuts or notches cross-wise over and through the fins. This process is costly as at least two embossing
rollers are required to form the cross-cut design. Moreover, the fins disclosed in all of the designs of
these patents are separated by empty troughs or grooves. None of the designs capitalize on this empty
area to enhance the heat transfer characteristics of the tubes.
While these inner surface tube designs aim to improve the heat transfer performance of the
tube, there remains a need in the industry to continue to improve upon tube designs by modifying
existing and creating new designs that enhance heat transfer performance. Additionally, a need also
exists to create designs and patterns that can be transferred onto the tubes more quickly and cost-
effectively. As described hereinbelow, the applicant has developed new geometries for heat transfer
tubes and, as a result, significantly improved heat transfer performance.
Summary of the Invention
Accordingly the present invention provides a heat transfer tube comprising an inner surface
and an outer surface, wherein the inner surface comprises a plurality of primary fins, a plurality of
intermediate fins, and a plurality of grooves defined by adjacent primary fins, the plurality of
intermediate fins being positioned in at least some of the plurality of grooves to form a grid like
pattern on the inner surface of the tube, at least a first portion of primary fins and intermediate fins
being separated from at least a second portion of primary fins and intermediate fins by a channel that
runs along a portion of the length of the inner surface of the tube.
The invention further provides a tube comprising an inner surface and a longitudinal axis,
wherein the inner surface comprises :
a. a plurality of primary fins, wherein at least some of the plurality of primary fins are
oriented substantially parallel to each other and wherein at least some of the plurality of primary fins
are oriented at an angle relative to the longitudinal axis wherein the plurality of primary fins is
divided into a first portion of primary fins and a second portion of primary fins;
b. a plural ity of grooves defined by adjacent primary fins;
c. a plurality of intermediate fins, wherein the plurality of intermediate fins are
positioned in at least some of the plurality of grooves and wherein at least some of the intermediate
fins are oriented at an angle relative to at least some of the primary fins, and
d. a trenched groove that runs between the first portion of primary fins and the second
portion of primary fins.
The invention further provides a heat transfer tube comprising an inner surface and an outer
surface, wherein the inner surface comprises:
a. two sets of fins, comprising (i) a plurality of adjacent primary fins defining a groove
between adjacent primary fins; and (ii) a plurality of short, intermediate fins positioned in at least
some of the grooves between the adjacent primary fins, wherein the plurality of short intermediate
fins are provided in a number greater than the number of adjacent primary fins; and
b. a channel dividing the two set of fins providing a trench for fluid transfer mediums to
flow between the two sets of fins.
The invention further provides a tube comprising an inner surface and an outer surface
wherein the inner surface comprises:
a. a first set of a plurality of primary fins positioned substantially parallel to one another
and defining (i) a plurality of primary fin axes and (ii) a first set of grooves between each set of
adjacent primary fins;
b. a first set of plurality of intermediate fins provided in an amount greater than the
amount of the first set of primary fins, wherein the first set of a plurality of intermediate fins is
positioned substantially parallel to one another in at least some of the first set of grooves,
c. a second set of a plurality of primary fins positioned substantially parallel to one
another and spaced apart from the first set of primary fins by a channel, wherein the second set of a
plurality of primary fins define (i) a plurality of primary fin axes and (ii) a second set of grooves
between each set of adjacent primary fins;
d. a second set of a plurality of intermediate fins provided in an amount greater than the
amount of the second set of primary fins, wherein the second set of a plurality of intermediate fins is
positioned substantially parallel to one another in at least some of the second set of grooves, and
e. a channel that separates the first set of primary and intermediate fins from the second
set of primary and intermediate fins.
Generally described, the present invention comprises an improved heat transfer tube and a
method of formation thereof. The inner surface of the tube, after the design of the present invention
has been embossed on a metal board and the board formed and welded into the tube, will have a
primary set of fins and an intermediate sets of fins positioned in the areas between the primary fins
and at an angle relative to the primary fins. While intermediate fins may be used with primary fins
arranged in any pattern, in a preferred embodiment of the inner surface tube design, the intermediate
fins are positioned relative to the primary fins to result in a grid-like appearance. Tests show that the
performance of tubes having the intermediate fin designs of the present invention is significantly
enhanced.
The method of the present invention comprises rolling a flat metallic board
between a first set of rollers shaped to create the primary and intermediate fin
designs on at least one side of the board. While previous
designs with similar performance use additional roller sets, the basic designs
of the present invention may be transferred onto the board using a single roller
set, thereby reducing manufacturing costs. Subsequent sets of rollers may be
used, however, to impart additional design features to the board. After the
desired pattern has been transferred onto the board with the rollers, the board
is then formed and welded into a tube, so that, at a minimum, the inner surface
design of the resulting tube includes the intermediate fins as contemplated by
the present invention.
Thus, it is an object of the present invention to provide improved heat
transfer tubes.
It is a further object of the present invention to provide an innovative
method of forming improved heat transfer tubes.
It is a further object of the present invention to provide an improved
heat transfer tube having intermediate fins.
It is a further object of the present invention to provide a method of
forming improved heat transfer tubes having intermediate fins.
It is a further object of the present invention to provide an improved
heat transfer tube with intermediate fins that may include primary and
intermediate fins of differing heights, shapes, pitches, and angles.
It is a further object of the present invention to provide an improved
heat transfer tube with two sets of fins formed in one rolling operation.
It is further object of the present invention to provide an improved heat
transfer tube that has at least two sets of fins having cuts cut cross-wise over
and at least partially through the fins.
It is further object of the present inventions to provide an improved
heat transfer tube having chambers, formed, in part, by the walls of the
intermediate fins, for enhanced nucleate boiling.
These and other features, objects and advantages of the present
invention will become apparent by reading the following detailed description of
preferred embodiments, taken in conjunction with the accompanying drawings.
Brief Description of the Accompanying Drawings
FIG. 1 is a perspective view of the inner surface of one embodiment of a
tube of the present invention.
FIG. 2 is an enlarged section view taken at inset circle 2 in FIG. 1.
FIG. 3 is a fragmentary plan view of one embodiment of a tube of the
present invention spread open to reveal the inner surface of the tube.
FIG. 4 is a cross-sectional view taken along line 4-4 in FIG. 3, illustrating
one embodiment of the primary fins.
FIG. 5 is a cross-sectional view taken along line 5-5 in FIG. 3, illustrating
one embodiment of the intermediate fins.
FIG. 6 is a cross-sectional view similar to FIGS. 4 and 5 showing an
alternative embodiment of the shape of the primary and/or intermediate fins.
FIG. 7 is a cross-sectional view similar to FIGS. 4 and 5 showing another
alternative embodiment of the shape of the primary and/or intermediate fins.
FIG. 8 is a cross-sectional view similar to FIGS. 4 and 5 showing another
alternative embodiment of the shape of the primary and/or intermediate fins.
FIG. 9 is a cross-sectional view similar to FIGS. 4 and 5 showing another
alternative embodiment of the shape of the primary and/or intermediate fins.
FIG. 10 is a cross-sectional view similar to FIGS. 4 and 5 showing another
alternative embodiment of the shape of the primary and/or intermediate fins.
FIG. 11 is a cross-sectional view similar to FIGS. 4 and 5 showing
another alternative embodiment of the shape of the primary and/or
intermediate fins.
FIG. 12 is a cross-sectional view similar to FIG. 5 showing another
alternative embodiment of the intermediate fins.
FIG. 13 is a fragmentary plan view of an alternative embodiment of a
tube of the present invention spread open to reveal the inner surface of the
tube.
FIG. 14 is a fragmentary plan view of an alternative embodiment of a
tube of the present invention spread open to reveal the inner surface of the
tube.
FIG. 15 is a fragmentary plan view of an alternative embodiment of a
tube of the present invention spread open to reveal the inner surface of the
tube.
FIG. 16 is a fragmentary plan view of an alternative embodiment of a
tube of the present invention spread open to reveal the inner surface of the
tube.
FIG. 17 is a fragmentary perspective view of the inner surface of an
alternative embodiment of a tube of the present invention.
FIG. 18 is a fragmentary perspective view of the inner surface of an
alternative embodiment of a tube of the present invention.
FIG. 19 is a perspective view of the fin-forming rollers used to produce
one embodiment of the tube of the present invention.
FIG. 20 illustrates a cross-sectional shape of a tube of the present
invention.
FIG. 21 illustrates an alternative cross-sectional shape of a tube of the
present invention.
FIG. 22 illustrates an alternative cross-sectional shape of a tube of the
present invention.
FIG. 23 illustrates an alternative cross-sectional shape of a tube of the
present invention.
FIG. 24 illustrates an alternative cross-sectional shape of a tube of the
present invention.
FIG. 25 illustrates an alternative cross-sectional shape of a tube of the
present invention.
FIG. 26 is a graph illustrating condensation heat transfer using an
embodiment of the tube of the present invention with R-22 refrigerant.
FIG. 27 is a graph illustrating condensation pressure drop using an
embodiment of the tube of the present invention with R-22 refrigerant.
FIG. 28 is a graph illustrating condensation heat transfer using an
embodiment of the tube of the present invention with R-407c refrigerant.
FIG. 29 is a graph illustrating condensation pressure drop using an
embodiment of the tube of the present invention with R-407c refrigerant.
FIG. 30 is a graph illustrating the efficiency of one embodiment of the
tube of the present invention with R-407c refrigerant.
FIG. 31 is a graph illustrating the efficiency of an alternative
embodiment of the tube of the present invention with R-22 refrigerant.
FIG. 32 is a graph illustrating condensation heat transfer using
embodiments of the tube of the present invention with R-22 refrigerant
FIG. 33 is a graph illustrating condensation pressure drop using
embodiments of the tube of the present invention with R-22 refrigerant.
Detailed Description of the Drawings
Like existing designs, the inner surface design of the tube 10 of the
present invention, one embodiment of which is illustrated in FIGS. 1-3,
includes a set of primary fins 12 that run parallel to each other along the inner
surface 20 of the tube 10. The cross-sectional shape of the primary fins 12
may assume any shape, such as those disclosed in FIGS. 6-11, but preferably
is triangular-shaped, having angled, straight sides 14, a rounded tip 16, and
rounded edges 18 at the interface of the sides 14 and inner surface 20 of the
tube 10 (see FIG. 4). The height of the primary fins HP may vary depending
on the diameter of the tube 10 and the particular application, but is preferably
between .004 - .02 inches. As shown in FIG. 3, the primary fins 12 may be
positioned at a primary fin angle 0 between 0°-90° relative to the longitudinal
axis 22 of the tube 10. Angle 9 is preferably between 5°-50° and more
preferably between 5°-30°. Finally, the number of primary fins 12 positioned
along the inner surface 20 of a tube 10, and thus the primary fin pitch PP
(defined as the distance between the tip or centerpoint of two adjacent primary
fins measured along a line drawn perpendicular to the primary fins), may vary,
depending on the height HP and shape of the primary fins 12, the primary fin
angle 0, and the diameter of the tube 10. Moreover, the primary fin shape,
height HP, angle 9, and pitch PP may vary within a single tube 10, depending
on the application.
Unlike previous designs, the designs of the present invention capitalize
on the empty areas or grooves 24 between the primary fins 12 to the enhance
heat transfer characteristics of the tubes. Intermediate fins 26 are formed in
the grooves 24 defined by the primary fins 12 to give the inner surface tube
design a grid-like appearance. The intermediate fins increase the turbulence
of the fluid and the inside surface area, and thereby the heat transfer
performance of the tube 10. Additionally, the intermediate fin designs
contemplated by the present invention may be incorporated onto the same
roller as the primary fin design, thereby reducing the manufacturing costs of
the tube 10.
The intermediate fins 26 preferably extend the width of the groove 24
to connect adjacent primary fins 12 (as shown in FIG. 3). Just as with the
primary fins 12, the intermediate fins 26 may assume a variety of shapes,
including but not limited to those shown in FIGS. 5-11. The intermediate fins
26 may be, but do not have to be, shaped similar to the primary fins 12, as
shown in FIG. 5. As with the primary fins 12, the number of intermediate fins
26 positioned between the primary fins 12 (and therefore the intermediate fin
pitch P1, defined as the distance between the tip or centerpoint of two adjacent
intermediate fins measured along a line drawn perpendicular to the
intermediate fins) and the height of the intermediate fins HI may be adjusted
depending on the particular application. The height of the intermediate fins HI
may, but do not have to, extend beyond the height of the primary fins HP. As
shown in FIG. 3, the intermediate fins 26 are positioned at an intermediate fin
angle ß measured from the counter-clockwise direction relative to the primary
fins 12. Intermediate fin angle ß may be any angle more than 0°, but is
preferably between 45°-135°.
As with the primary fins, the intermediate fin shape, height HI, pitch PI,
and angle ß need not be constant for all intermediate fins 26 in a tube 10, but
rather all or some of these features may vary in a tube 10 depending on the
application. For example, FIG. 12 illustrates a cross-section of a spread out
tube 10 having an inner surface tube design with a variety of intermediate fin
shapes, heights (HI-I, HI-2, and HI-3), and pitches (PI-I and PI-2).
As shown in FIGS. 13-16, intermediate fins 26 may be used in
conjunction with primary fins 12 arranged in any pattern, including, but not
limited to, all of the patterns disclosed in U.S. Patent No. 5,791,405 to Takima
et al., the entirety of which being herein incorporated by reference. For
example, FIGS. 13-16 illustrate embodiments where some of the primary fins
12 are arranged at an angle relative to other of the primary fins 12. In FIGS.
13 and 14, the primary fins 12 intersect Similarly, in FIG. 16, portions of
primary and intermediate fins run along the length of tube 10 while adjacent
portions of primary and intermediate fins are arranged at angles thereto. In
FIG. 15, the primary fins 12 do not intersect, but rather are separated by a
channel 50 that runs along the length of the inner surface 20 of tube 10. More
than one channel 50 may be provided along the inner surface 20 of tube 10.
The depth of channel 50 into tube 10 can be varied depending on the
application. Moreover, the surface of channel 50 can be, but does not have to
be, smooth. Rather, grooves, ridges, and/or other features to roughen the
surface of channel 50 can be provided.
Additionally, instead of connecting adjacent primary fins 12, the
intermediate fins 26 may be free-standing geometrical shapes, such as cones,
pyramids, cylinders, etc. (as shown in FIG. 18).
One skilled in the art would understand how to manipulate inner
surface tube design variables of the primary and intermediate fins, including
fin arrangement, shape, height HP and HI, angles 0 and ß and pitches PP and
PI to tailor the inner surface tube design to a particular application in order to
obtain the desired heat transfer characteristics.
The tubes having patterns in accordance with the present invention
may be manufactured using production methods and apparatuses well known
in the art, such as those disclosed in U.S. Patent No. 5.704.424 to Kohn, et al.,
the entirety of which is herein incorporated by reference. As explained in
Kohn, et al., a flat board, generally of metal, is passed between sets of rollers
which emboss the upper and lower surface of the board. The board is then
gradually shaped in subsequent processing steps until its edges meet and are
welded to form a tube 10. The tube may be formed into any shape, including
those illustrated in FIGS. 20-25. While round tubes have traditionally been
used and are well-suited for purposes of the present invention, enhanced heat
transfer properties have been realized using tubes 10 having a cross-sectional
shape flatter than traditional round tubes, such as those illustrated in FIGS. 22,
23, and 25. Consequently, it may be preferable during the shaping stage of
production, but before the welding stage, to form tubes 10 having a flatter
shape. Alternatively. the_tubes 10 may be formed into the traditinoal round
shape and subsequently compressed to flatten the cross-sectional shape of the
tube 10. One of ordinary skill in the art would understand that the tube 10
may be formed into any shape, including but not limited to those illustrated in
FIGS. 20-25, depending on the application.
The tube 10 (and therefore the board) may be made from a variety of
materials possessing suitable physical properties including structural integrity,
malleability, and plasticity, such as copper and copper alloys and aluminum
and aluminum alloys. A preferred material is deoxidized copper. While the
width of the flat board will vary according to the desired tube diameter, a flat
board having a width of approximately 1.25 inches to form a standard 3/8"
tube outside diameter is a common size for the present application.
To form the desired pattern on the board, the board is passed through a
first set of deforming or embossing rollers 28, which consists of an upper
roller 30 and a lower roller 32 (see FIG. 19). The pattern on the upper roller
30 is an interlocking image of the desired primary and intermediate fin pattern
for the inner surface of the tube 10 (i.e. the pattern on the upper roller
interlocks with the embossed pattern on the tube). Similarly, the pattern of the
lower roller 32 is an interlocking image of the desired pattern (if any) of the
outer surface of the tube 10. FIG. 19 illustrates one set of rollers 28, the upper
roller 30 having a pattern that includes an intermediate fin design as
contemplated by the present invention.
Note, however, that to manufacture a tube in accordance with the
embodiment shown in FIG. 15, one or more longitudinal channels 50 are
preferably first embossed along at least a portion of the length of the board
with an embossing roller having ridges around the circumference of the roller.
These ridges form the channels in the smooth board. The number of ridges
provided on the roller coincides with the number of channels embossed on the
board. After channel formation, the board is then subjected to the rollers 28 as
described above. In this way, the pattern on the upper roller 30 is not
embossed onto the depressed channels 50 in the board.
The patterns on the rollers may be made by machining grooves on the
roller surface. As will be apparent to one of ordinary skill in the art, because
of the interlocking-image relationship between the rollers and the board, when
the board is passed through the rollers, the grooves on the rollers form fins on
the board and the portions of the roller surface not machined form grooves on
the board. When the board is subsequently rolled and welded, the desired
inner and outer patterns are thereby located on the tube.
An advantage of the tubes formed in accordance with the present
invention is that the primary and intermediate fin designs of the tubes may be
machined on the roller and formed on the board with a single roller set, as
opposed to the two sets of rollers (and consequently two embossing steps) that
have traditionally been necessary to create existing inner surface tube designs,
such as the cross-cut design, that enhance tube performance. Elimination of a
roller set and embossing stage from the manufacturing process can reduce the
manufacturing time and cost of the tube.
However, while only one roller set is necessary to create the primary
and intermediate fin designs of the present invention, subsequent and
additional rollers may be used impart additional design features to the board.
For example, a second set of rollers may be used to make cuts 38 cross-wise
over and at least partially through the fins to result in a cross-cut design, as
shown in FIG. 17.
In an alternative design, the primary and intermediate fins form the
sidewalls of a chamber. The tops of the primary fins may be formed, such as,
for example, by pressing them with a second roller, to extend or flare laterally
to partially, but not entirely, close the chamber. Rather, a small opening
through which fluid is able to flow into the chamber remains at the top of the
chamber. Such chambers enhance nucleate boiling of the fluid and thereby
improve evaporation heat transfer.
In addition to potentially reducing manufacturing costs, tubes having
designs in accordance with the present invention also outperform existing
tubes. FIGS. 26-29 graphically illustrate the enhanced performance of such
tubes in condensation obtainable by incorporating intermediate fins into the
inner surface tube design. Performance tests were conducted on four
condenser tubes for two separate refrigerants (R-407c and R-22). The
following copper tubes, each of which had a different inner surface design,
were tested:
(1) "Turbo-A®," a seamless or welded tube made by Wolverine
Tube for evaporator and condenser coils in air conditioning and refrigeration
with internal fins that run parallel to each other at an angle to the longitudinal
axis of the tube along the inner surface thereof (designated "Turbo-A®");
(2) a cross-cut tube made by Wolverine Tube for evaporator and
condenser coils (designated "Cross-Cut");
(3) a tube with an intermediate fin design in accordance with the
present invention (designated "New Design"); and
(4) a tube with an intermediate fin design in accordance with the
present invention whereby the primary and intermediate fins have been cross-
cut with a second roller (designated "New Design X").
Figs. 26 and 27 reflect data obtained using R-22 refrigerant. Figs. 28
and 29 reflect data obtained using R-407 refrigerant. The general testing
conditions represented by these graphs are as follows:
Evaporation Condensation
Saturation Temperature 35° (1.67° C) 105°F(40.6°C)
Tube Length 12 ft (3.66 m) 12 ft (3.66 m)
Inlet Vapor Quality 10% 80%
Outlet Vapor Quality 80% 10%
The data was obtained for flowing refrigerant at different flow rates.
Accordingly, the "x" plane of all the graphs is expressed in terms of mass flux
(lb./hr. ft2). Figs. 26 and 28 show heat transfer performance. Accordingly, the
"y" plane of these two graphs is expressed in terms of heat transfer co-
efficient (Btu/hr. fit2). Figs. 27 and 29 show pressure drop information.
Accordingly, the "y" plane of these two graphs is expressed in terms of
pressure per square inch (PSI).
The data for the R-407c refrigerant (Figs. 28 and 29), which is a
zeotropic mixture, indicates that the condensation heat transfer perfonnance of
the New Design is approximately 35% improved over the Turbo-A® design.
Further, the New Design provides increased performance (by approximately
15%) over the standard Cross-Cut design, which is currently regarded as the
leading performer in condensation performance among widely
commercialized tubes. In terms of pressure drop performance, the New
Design performs as well as the Turbo-A® design and approximately 10%
lower than the standard Cross-Cut design. The pressure drop is a very
important design parameter in heat exchanger design. With the current
technology in heat exchangers, a 5% decrease in pressure drop can sometimes
provide as much benefit as a 10% increase in heat transfer performance.
The new design makes use of an interesting phenomenon in two-phase
heat transfer. In a tube embodiment of the present invention, where a fluid is
condensing on the inside of the tube, the pressure drop is mainly regulated by
the liquid-vapor interface. The heat transfer is controlled by the liquid-solid
interface. The intermediate fins affect the liquid layer, thereby increasing the
heat transfer, but do not impact the pressure drop. The relationship between
the heat transfer and pressure drop is captured by the efficiency factor.
With use of the R-22 refrigerant (Figs. 26 and 27), the New Design X
outperformed the Turbo-A® and Cross-Cut designs with respect to heat
transfer by nearly the same percentages as the New Design did in the R-407c
tests. The inventor has no reason to believe that similar performance
improvement will not be obtained using other refrigerants such as R-410(a) or
R-134(a), and other similar fluids.
FIGS. 30 and 31 compare the efficiency factors of the Cross-Cut
design with the efficiency factors of the New Design (FIG. 30) and the New
Design X (FIG. 31). The efficiency factor is a good indicator of the actual
performance benefits associated with a tube inner surface because it reflects
both the benefit of additional heat transfer and the drawback of additional
pressure drop. In general, the efficiency factor of a tube is defined as the
increase in heat transfer of that tube over a standard tube (in this case, the
Turbo-A®) divided by the increase in pressure drop of that tube over the
standard tube. The efficiency factors plotted in FIGS. 30 and 31 for the
Cross-Cut were calculated as follows:
The efficiency factors of the New Design and the New Design X, plotted in
FIGS. 30 and 31, respectively, were similarly calculated.
As can be seen in FIGS. 30 and 31, the efficiency factors for the New
Design and the New Design X are all (with the exception of one) above "1",
which indicates that the efficiency of both of these new designs is better than
that of the standard Turbo-A® by as much as 40% in R-22 condensation (FIG.
31) and by up to 35% in R-407c condensation (FIG. 30). Moreover, by
comparing the efficiency factors of the Cross-Cut (FIGS. 30 and 31) plotted
against the New Design (FIG. 30) and New Design X (FIG. 31), it is apparent
that the efficiencies of the new designs are consistently better than the Cross-
Cut tube by 20% in R-22 condensation (FIG. 31) and 10% in R-407c
condensation (FIG. 30).
Additionally, tests also demonstrate mat tubes having inner surfaces
similar to those shown in Figs. 13 and 15 also outperform Turbo-A® tubes.
The results of such tests are shown in Figs. 32 and 33, wherein a tube having
an inner surface in accordance with Fig. 13 is designated "New Design 2" and
a tube having an inner surface in accordance with Fig. 15 is designated "New
Design 3." Figs. 32 and 33 reflect data obtained using R-22 refrigerant under
the same condensation testing conditions described above.
Figs. 32 and 33 show heat transfer performance and pressure drop,
respectively. The data, as reflected in Figs. 32 and 33, indicates that the
condensation heat transfer performance of the New Design 2 and New Design
3 is approximately 80% and 40% improved, respectively, over the Turbo-A®
design. Further, while the pressure drop for the New Design 2 increased over
Turbo-A®, the New Design 3 exhibited pressure drop comparable to Turbo-
A®. This data suggests that significant heat transfer benefits can be realized
by incorporating the New Design 3 into existing systems to replace Turbo-A®
tubes. In addition, by preventing the pattern from forming on a portion of the
tube (i.e., in the channels 50), the amount of material in a unit length of tube is
reduced. This results in significant cost savings to customers.
Moreover, the New Design 2 may be particularly beneficial
incorporated into redesigned systems. This is particularly significant in light
of recent measures to increase efficiencies of air-conditioning equipment. By
using the New Design 2 surface, one can attain increased performance in the
same size of equipment or reduce the size of equipment Thus, it would be
possible to reduce or eliminate expensive redesign efforts. In addition, by
reducing the size of the system, one also reduces the amount of other
components, like metal for the base, aluminum for the fins and tubing lines,
that can result in considerable savings to the customer.
Thus it is seen that a tube providing intermediate fins represents a
significant improvement over cross-cut and single helical ridge designs. This
new design thus advances the state of the art. It will be understood by those
of ordinary skill in the art that various modifications may be made to the
preferred embodiments within the spirit and scope of the invention as defined
by the appended claims.
WE CLAIM :
1. A heat transfer tube comprising an inner surface and an outer surface, wherein the inner
surface comprises a plurality of primary fins, a plurality of intermediate fins, and a plurality of
grooves defined by adjacent primary fins, the plurality of intermediate fins being positioned in at
least some of the plurality of grooves to form a grid like pattern on the inner surface of the tube, at
least a first portion of primary fins and intermediate fins being separated from at least a second
portion of primary fins and intermediate fins by a channel that runs along a portion of the length of
the inner surface of the tube.
2. The tube as claimed in claim 1, which is made of a metal.
3. The tube as claimed in claim 1, which is made of a non-metallic material.
4. The tube as claimed in claim 1, which is of a circular cross-sectional shape.
5. The tube as claimed in claim 1, the outer surface whereof is smooth.
6. The tube as claimed in claim 1, the outer surface whereof is contoured.
7. The tube as claimed in claim 1, wherein at least some of the plurality of primary fins are
oriented parallel to each other.
8. The tube as claimed in claim 1, wherein the plurality of primary fins comprises a first set of
adjacent primary fins having a first primary fin pitch and a second set of adjacent primary fins having
a second primary fin pitch, wherein the first primary fin pitch is not equal to the second primary fin
pitch.
9. The tube as claimed in claim 1, wherein at least some of the plurality of primary fins have a
cross-sectional shape of substantially a triangle with rounded tip.
10. The tube as claimed in claim 1, wherein at least some of the plurality of primary fins have a
substantially rectilinear cross-sectional shape.
11. The tube as claimed in claim 1, wherein at least some of the plurality of primary fins have a
generally curved cross-sectional shape.
12. The tube as claimed in claim 1, having a longitudinal axis, wherein at least some of the
plurality of primary fins are oriented at an angle relative to the longitudinal axis.
13. The tube as claimed in claim 12, wherein at least some of the plurality of primary fins are
oriented at an angle between 5° to 50° relative to the longitudinal axis.
14. The tube as claimed in claim 13, wherein at least some of the plurality of primary fins are
oriented at an angle between 5° to 30° relative to the longitudinal axis.
15. The tube as claimed in claim 1, wherein at least some of the plurality of primary fins have
cuts that traverse the width of the primary fins.
16. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
contact adjacent primary fins.
17. The tube as claimed in claim 1, wherein the plurality of intermediate fins comprise a first set
of adjacent intermediate fins having a first intermediate fin pitch and a second set of adjacent
intermediate fins having a second intermediate fin pitch, wherein the first intermediate fin pitch is not
equal to the second intermediate fin pitch.
18. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins are
oriented at an angle relative to at least some of the primary fins.
19. The tube as claimed in claim 18, wherein at least some of the plurality of intermediate fins
are oriented at an angle between 45° to 135° relative to at least some of the primary fins.
20. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
comprise a free-standing geometrical shape positioned in the groove.
21. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
have a cross-sectional shape of substantially a triangle with a rounded tip.
22. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
have a substantially rectilinear cross-sectional shape.
23. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
have a generally curved cross-sectional shape.
24. The tube as claimed in claim 1, wherein at least some of the plurality of intermediate fins
have cuts that traverse the width of the intermediate fins.
25. A heat transfer tube comprising an inner surface and a longitudinal axis, wherein the inner
surface comprises :
a. a plurality of primary fins, wherein at least some of the plurality of primary fins are
oriented substantially parallel to each other and wherein at least some of the plurality of primary fins
are oriented at an angle relative to the longitudinal axis wherein the plurality of primary fins are
divided into a first portion of primary fins and a second portion of primary fins;
b. a plurality of grooves defined by adjacent primary fins;
c. a plurality of intermediate fins, wherein the plurality of intermediate fins are
positioned in at least some of the plurality of grooves and wherein at least some of the intermediate
fins are oriented at an angle relative to at least some of the primary fins, and
d. a trenched groove that runs between the first portion of primary fins and the second
portion of primary fins.
26. The tube as claimed in claim 1, which is of a substantially oval cross-sectional shape.
27. The tube as claimed in claim 1, which has a cross-sectional shape comprising two
substantially parallel lines connected by arcs.
28. The tube as claimed in claim 1, wherein the plurality of primary fins comprise a first set and
a second set of primary fins, the plurality of grooves comprise a first set of grooves defined by the
first set of primary fins and a second set of grooves defined by the second set of primary fins, and the
plurality of intermediate fins comprise a first set of intermediate fins positioned in at least some of
the first set of grooves and a second set of intermediate fins positioned in at least some of the second
set of grooves, wherein the first set of primary fins is oriented at an angle with respect to the second
set of primary fins.
29. The tube as claimed in claim 28, wherein the first set of primary fins and the second set of
primary fins intersect.
30. The tube as claimed in claim 28, wherein the first set of primary fins and the second set of
primary fins are separated by at least one channel that runs along a portion of the length of the inner
surface of the tube.
31. A heat transfer tube comprising an inner surface and an outer surface, wherein the inner
surface comprises:
a. two sets of fins, comprising (i) a plurality of adjacent primary fins defining a groove
between adjacent primary fins; and (ii) a plurality of short, intermediate fins positioned in at least
some of the grooves between the adjacent primary fins, wherein the plurality of short intermediate
fins are provided in a number greater than the number of adjacent primary fins; and
b. a channel dividing the two set of fins providing a trench for fluid transfer mediums to
flow between the two sets of fins.
32. The tube as claimed in claim 31, wherein at least some of the plurality of short, intermediate
fins are oriented at an angle relative to at least some of the adjacent primary fins.
33. The tube as claimed in claim 32, wherein at least some of the plurality of short, intermediate
fins are oriented at an angle between 45° to 135° relative to at least some of the adjacent primary fins.
34. A heat transfer tube comprising an inner surface and an outer surface wherein the inner
surface comprises:
a. a first set of a plurality of primary fins positioned substantially parallel to one another
and defining (i) a plurality of primary fin axes and (ii) a first set of grooves between each set of
adjacent primary fins;
b. a first set of plurality of intermediate fins provided in an amount greater than the
amount of the first set of primary fins, wherein the first set of a plurality of intermediate fins is
positioned substantially parallel to one another in at least some of the first set of grooves,
c. a second set of a plurality of primary fins positioned substantially parallel to one
another and spaced apart from the first set of primary fins by a channel, wherein the second set of a
plurality of primary fins define (i) a plurality of primary fin axes and (ii) a second set of grooves
between each set of adjacent primary fins;
d. a second set of a plurality of intermediate fins provided in an amount greater than the
amount of the second set of primary fins, wherein the second set of a plurality of intermediate fins is
positioned substantially parallel to one another in at least some of the second set of grooves, and
e. a channel that separates the first set of primary and intermediate fins from the second
set of primary and intermediate fins.
35. The tube as claimed in claim 34, wherein at least some of the plurality of intermediate fins are
oriented at an angle relative to at least some of the adjacent primary fins.
36. The tube as claimed in claim 35, wherein at least some of the plurality of intermediate fins are
oriented at an angle between 45° to 135° relative to at least some of the adjacent primary fins.
37. The tube as claimed in claim 1, having a plurality of first portions of primary fins and
intermediate fins separated from a plurality of section portions of primary fins and intermediate fins
by a plurality of channels.
38. The tube as claimed in claim 25, having more than one trenched groove dividing more than
one first and second portions of primary fins.
39. The tube as claimed in claim 31, having more than two sets of fins, wherein each set of fins
are divided by a channel.
40. The tube as claimed in claim 34, having a plurality of first and second sets of fins separated
by a plurality of channels.
A heat transfer tube (10) has an inner surface (12) and an outer surface,
wherein the inner surface comprises a plurality of primary fins (12), a plurality of
intermediate fins (26), and a plurality of grooves (24) defined by adjacent primary
fins, and the intermediate fins (20) are positioned in at least some of the
grooves (24).

Documents:


Patent Number 223783
Indian Patent Application Number 01356/KOLNP/2003
PG Journal Number 39/2008
Publication Date 26-Sep-2008
Grant Date 23-Sep-2008
Date of Filing 21-Oct-2003
Name of Patentee WOLVERINE TUBE INC.
Applicant Address 200 CLINTON AVENUE, SUITE 1000, HUNTSVILLE, AL
Inventors:
# Inventor's Name Inventor's Address
1 CLEVINGER NORMAN R 517 FERRY STREET, N.E., DECATUR, AL 35601
2 THORS PETUR 4222 WILLOW BEND ROAD, S.E., DECATUR, AL 35603
3 NARAYANMURTHY RAMACHANDRAN 1075 DOCKSIDE DRIVE, #914, HUNTSVILLE, AL 35824
PCT International Classification Number F28F 1/40
PCT International Application Number PCT/US02/12296
PCT International Filing date 2002-04-17
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 09/836,808 2001-04-17 U.S.A.