BACKGROUND OF THE DISCLOSURE
[0001] This disclosure relates to heat exchangers and, more particularly, to tube heat exchangers
and configurations of tubes of tube heat exchangers.
[0002] Tube heat exchangers typically have a bundle of tubes which can include many rows
of tubes in a cross-flow setup. The tubes carry one heat exchange medium and the other
flows across the tubes.
[0003] Tube bundle heat exchangers are effective at heat exchange, but can encounter challenges
in resonance driven by wakes being shed from the tubes due to flow past the tubes.
[0004] In some flow regimes, the wake can oscillate and the oscillating wake can generate
a force function on the tubes generating the wake as well as tubes downstream being
hit with the incident wake.
[0005] In some instances, wake frequency can be similar to the natural frequency of the
tube, and resonance can occur which negatively impacts the high cycle fatigue (HCF)
life.
[0006] In addition, certain conditions of oscillation as well as resonance can lead to noise
at potentially undesirable levels, for example for humans working and/or otherwise
in the vicinity of the heat exchanger.
[0007] Also, when the heat exchanger is used, for example for heat exchange in an engine,
the environment generally is a highly vibratory environment and, therefore taking
steps to mitigate additional vibration or resonance is of interest.
SUMMARY OF THE DISCLOSURE
[0008] In accordance with one non-limiting embodiment, a tube bundle heat exchanger comprises
a flow space for a first heat exchange medium; and a plurality of heat exchange tubes
for a second heat exchange medium, wherein the plurality of heat exchange tubes extends
at least partially across the flow space, wherein the plurality of heat exchange tubes
comprises at least a first plurality of tubes having a first diameter and a second
plurality of tubes having a second diameter different from the first diameter.
[0009] In a non-limiting configuration, the second plurality of tubes are positioned relative
to the first plurality of tubes such that, during expected flow conditions through
the flow space, wake shedding frequency exhibited by the plurality of heat exchange
tubes does not match natural frequency of the plurality of heat exchange tubes.
[0010] In another non-limiting configuration, the second diameter is larger than the first
diameter.
[0011] In still another non-limiting configuration, the second plurality of tubes are positioned
in alternating rows relative to the first plurality of tubes, the rows extending transverse
to flow direction through the flow space.
[0012] In a further non-limiting configuration, the first set of tubes are not aligned with
the second set of tubes in the flow direction.
[0013] In a still further non-limiting configuration, the first set of tubes are arranged
across the flow direction of the heat exchanger with gaps defined between each pair
of adjacent tubes, and tubes of the second set of tubes are aligned in the flow direction
with the gaps in the first set of tubes.
[0014] In another non-limiting configuration, the first set of tubes and the second set
of tubes are aligned with each other in the flow direction.
[0015] In still another non-limiting configuration, the first plurality of tubes and the
second plurality of tubes are arranged in staggered alternating rows extending in
the flow direction.
[0016] In a further non-limiting configuration, a ratio of second diameter to the first
diameter is greater than 1:1 and up to 3:1.
[0017] In a still further non-limiting configuration, the second set of tubes has a diameter
that is at least 10% larger than the first set of tubes.
[0018] In another non-limiting configuration, the second set of tubes comprises between
about 30 and about 70% by number of the plurality of heat exchange tubes.
[0019] In still another non-limiting configuration, the plurality of heat exchanger tubes
are arranged at a transverse spacing (ST) such that a ratio of the transverse spacing
to an average diameter (D) of the plurality of tubes (ST/D) is between 1.5 and 2.5.
[0020] In a further non-limiting configuration, the plurality of heat exchanger tubes are
arranged at a longitudinal spacing (SL) such that a ratio of the longitudinal spacing
to an average diameter (D) of the plurality of tubes (SL/D) is between 1.0 and 3.0.
[0021] In a still further non-limiting configuration, the second set of tubes comprises
a row of the second set of tubes extending across the flow direction to reset any
wake shedding flow conditions from upstream of the row.
[0022] In another non-limiting configuration, the first set of tubes are arranged in hexagonal
patterns around each of the second set of tubes.
[0023] In a further non-limiting embodiment, in a method for operating a tube bundle heat
exchanger comprising a flow space for a first heat exchange medium; and a plurality
of heat exchange tubes for a second heat exchange medium, wherein the plurality of
heat exchange tubes extends at least partially across the flow space, wherein the
plurality of heat exchange tubes comprises at least a first plurality of tubes having
a first diameter and a second plurality of tubes having a second diameter different
from the first diameter, the method comprising flowing the first heat exchange medium
through the flow space at flow conditions to generate vortex shedding frequency; and
flowing the second heat exchange medium through the plurality of heat exchange tubes
at tube flow conditions to generate natural frequency, wherein the second set of tubes
are positioned such that there is no resonance between the vortex shedding frequency
and the natural frequency.
[0024] In another non-limiting configuration, the flowing steps result in heat exchange
between the first heat exchange medium and the second heat exchange medium.
[0025] In still another non-limiting configuration, the second diameter is at least 10%
greater than the first diameter.
[0026] In a further non-limiting configuration, tubes of the plurality of heat exchanger
tubes are arranged at a transverse spacing (ST) such that a ratio of the transverse
spacing to an average diameter (D) of the plurality of tubes (ST/D) is between 1.5
and 2.5.
[0027] In a still further non-limiting configuration, tubes of the plurality of heat exchanger
tubes are arranged at a longitudinal spacing (SL) such that a ratio of the longitudinal
spacing to an average diameter (D) of the plurality of tubes (SL/D) is between 1.0
and 3.0.
[0028] The foregoing features and elements may be combined in various combinations without
exclusivity, unless expressly indicated otherwise. These features and elements as
well as the operation thereof will become more apparent in light of the following
description and the accompanying drawings. It should be appreciated that the following
description and drawings are intended to be exemplary in nature and non-limiting.
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] A detailed description of non-limiting embodiments of the present disclosure follows,
with reference to the attached drawings, wherein:
FIG. 1 schematically illustrates a conventional cross flow tube bundle heat exchanger;
FIG. 2 illustrates a series of different types of flow regimes that can occur due
to flow past heat exchanger tubes;
FIG. 3 illustrates the relationship between natural frequency and wake shedding frequency
for heat exchanger tubes by tube diameter;
FIG. 4 illustrates an offset pattern of heat exchanger tubes similar to that which
is used in FIG. 1;
FIG. 5 illustrates a pattern of tubes with different diameters arranged in rows transverse
to the flow direction in the heat exchanger;
FIG. 6 illustrates another pattern of tubes with different diameters arranged in offset
rows parallel to the flow direction;
FIG. 7 illustrates a further non-limiting configuration similar to that of FIG. 5,
but with first tubes and second tubes aligned along the flow direction;
FIG. 8 illustrates a further arrangement of tubes wherein a relatively larger plurality
of tubes are surrounded in hexagonal patterns of relatively smaller tubes; and
FIG. 9 illustrates another non-limiting configuration wherein the larger and smaller
diameter tubes are arranged diagonally across the flow space.
DETAILED DESCRIPTION
[0030] The disclosure relates to tube bundle heat exchangers. FIG. 1 schematically illustrates
such a heat exchanger 10 wherein a duct 12 carries a first flow 14 of heat exchange
medium that flows across a plurality of heat exchange tubes 16 carrying a second fluid
exchange medium. In such heat exchangers, heat transfer is effectively conducted between
the two heat exchange mediums. However, depending upon the mounting of the heat exchange
tubes, as well as diameter, material and other factors, each of the heat exchange
tubes will have a natural frequency induced by the flow. In addition, when fluid flows
past a "blunt" object such as tubes 16, the flow regime passing and following the
object can be significantly impacted.
[0031] FIG. 2 shows a series of different flows that can result due to flow past blunt objects
like heat exchanger tubes. One basic flow regime is a regime of unseparated flow as
illustrated at 18. In view 20, a flow regime is created which exhibits a fixed pair
of oppositely rotating vortices in the wake. In view 22, two regimes are created wherein
a vortex street is laminar. This flow pattern can be particularly disruptive as the
aligned lateral flows can impact downstream tubes at the same frequency which, depending
upon the specific application, can be in the range of 2-4 kHz. View 24 shows a transition
to turbulence in the vortex, and the vortex street is fully turbulent. View 26 shows
a flow regime wherein a laminar boundary layer has undergone turbulent transition,
leading to a narrower wake that is disorganized. In the last view 28, a turbulent
vortex street is reestablished.
[0032] In certain circumstances, any of the flow regimes illustrated in FIG. 2 can cause
issues. This is due to the combination of natural frequency illustrated by all heat
exchanger tubes, and flow shedding frequency caused by the wake as the flow passes
a tube. FIG. 3 illustrates a plot of these frequencies versus tube diameter. As shown,
natural frequency 30 steadily increases with tube diameter, while frequency of the
vortex shedding 32 decreases with increase of tube diameter. Where these frequencies
approach each other 34, resonance can occur that can cause damage to the tubes and
related structures. Incorporating tubes of different sizes as well as different flow
patterns can help to avoid resonance and thereby extend the useful life of the heat
exchanger. Further, as will be discussed below, heat exchange efficiency can also
be improved.
[0033] FIG. 4 shows another version of a conventional tube configuration wherein tubes all
having the same diameter are arranged in a staggered configuration rather than the
straight rows of FIG. 1. In the configuration of FIG. 4, vortex shedding can occur
differently, but downstream can have an even greater influence on tubes that they
impact. In consideration of FIG. 4 and the discussion of FIGS. 5-9 to follow, potential
flow regimes are illustrated and discussed as well. These illustrations are shown
only on selected portions of tubes, but are representative of the full flow field.
The flow fields for each of the configurations shown will have some similarities.
The first two rows of tubes will see relatively clean air. Depending upon Reynolds
number, the flow separates on the aft or downstream side of the tubes, producing a
vortex. The vortex is swept downstream to impinge on the next row of tubes. On subsequent
rows, instead of clean air, the vortex strikes the tube. Flow in this configuration
has some separation and also different relative speed. Flow immediately downstream
of the tube can have vortices and is relatively slow flow, while the flow alongside
the tubes and past the wake flow is faster. The flow is squeezed and expanded as it
works its way through the tube bank. This aids with mixing the heated flow (that near
the tubes) with the unheated, bulk flow. This can be considered as a steady-state
depiction, but there will also be periodic vortex shedding. Referring back to the
illustrations of FIG. 2, the effects of different Reynolds numbers is illustrated.
For a relatively low Reynolds number, flow can be similar to image 20, with low Reynolds
separation. At relatively higher Reynolds numbers, the vortex shedding becomes turbulent,
for example as shown in image 26 of FIG. 2.
[0034] FIGS. 5-9 illustrate different configurations wherein the plurality of heat exchanger
tubes are provided as a first set or plurality of tubes 38 having a first diameter
and a second set or plurality of tubes 40 having a second diameter. Of course, this
is a non-limiting configuration and it is possible to have arrays of tubes with more
than 2, for example 3 or more, different diameters. While adding a further layer of
complexity to the overall net result on flow, this can also be modeled and tailored
to the specific environment to reduce the possibility of resonance. In one non-limiting
configuration of these embodiments, the second diameter is larger than the first diameter.
[0035] When different size tubes are introduced, the local Reynolds number changes, since
it is a function of the tube diameter and spacing. For the relatively smaller tubes,
the Reynolds number is lower and should produce more of a fixed pair of vortices,
similar to image 20 of FIG. 2. For the relatively larger tubes, at a higher Reynolds
number, the shedding will be more periodic.
[0036] In the configuration of FIG. 5, tubes are arranged in alternating rows that are substantially
transverse to the flow direction A. Further, these rows are themselves offset such
that tubes 38 are not aligned with immediately upstream tubes 40. In this configuration,
the vortex shedding from a large diameter tube 40 next encounters an offset pair of
small diameter tubes 38, and thus disrupts the vortex street and helps to prevent
resonance. The difference in diameter of the tubes 38, 40 disrupts the formation of
a coherent set of vortices. For example, in the configuration of FIG. 5, wakes of
neighboring tubes interfere with each other. In the configuration of FIG. 6, tubes
38, 40 are arranged in staggered rows arranged substantially parallel to flow direction
A. In this configuration, vortex shedding from each tube encounters a spaced pair
of different sized tubes downstream, and this also helps to disrupt any potential
resonance.
[0037] Changing the position of large and small tubes from the position in FIG. 5 to that
of FIG. 6 is believed to produce a different looking flow field. The impedance over
the smaller tubes, with a relatively larger spacing is lower than that of the larger
tubes. The flow rate is expected to be biased, even only a small amount, toward the
rows of smaller tubes. As a result, their Reynolds numbers will rise while the decrease
in flow rate on the large tubes lowers their respective Reynolds numbers. In the extreme
case, with very large and very small tubes, flow over the larger tubes could be starved.
Hence, the arrangement in FIG. 5 should have better thermal performance than that
of FIG. 6.
[0038] In the configuration of FIG. 7, tubes can be arranged in alternating and aligned
rows of tubes 40, 38 that are arranged substantially transverse to flow direction
A. In this configuration, vortex shedding from any tube next encounters a tube of
a different diameter immediately downstream, again serving to disrupt resonance. On
the other hand, this configuration, known as an in-line arrangement, can be less efficient
in heat exchange because flow can move directly along between the rows.
[0039] In the configuration of FIG. 8, relatively large diameter tubes 40 can be arranged
in an offset pattern, with each tube 40 surrounded by a hexagonal pattern of smaller
diameter tubes 38. In FIG. 8, lines show the actual hexagonal positioning, but these
lines are only for further illustration and do not represent a structural component
of the tube pattern. This results in a more complex interaction of vortex shedding
interaction with lateral interference of the vortices which again serve to help disrupt
the potential for resonance.
[0040] Specifically, the configuration of FIG. 8 should produce a blending of staggered
and in-line arrangement. The larger tubes are staggered but the smaller tubes are
in-line. The flow striking the larger tubes is always produced by the wake of the
smaller tubes, with a low Reynolds vortex. The larger tube will have a larger Reynolds
number and produce the relative cortex pattern, which now strikes the downstream,
smaller tube. These large and small vortices can be expected to mix rather quickly
and have a somewhat uniform size after the first few rows. Locally, right behind a
given tube, the shedding will be similar to what is shown in FIG. 2, for example at
20.
[0041] In the configuration of FIG. 9, a further pattern can have the smaller diameter tubes
38 and the larger diameter tubes 40 arranged diagonally across the flow space as shown.
In this configuration, each transverse row of tubes comprises alternating large and
small diameter tubes, and although the tubes are also in line in the flow direction
A, they alternate in the flow direction as well between small diameter and large diameter
tubes. This configuration also helps to interrupt flow vortices at each level to help
prevent an undesirable vortex street and resonance as discussed above.
[0042] The flow field that results in FIG. 9 can be somewhat different from the other tube
configurations. Keeping with the vortex shedding pattern based on tube size, the smaller
tubes produce a symmetric vortex pair. The larger tubes have more periodic shedding.
As a result, the vortex wake of the larger tubes may encompass the smaller, downstream
tube. In FIGS. 5 and 6, the flow striking the small tubes was rather smooth. Here,
that only holds for the first row. After that, all the smaller tubes are in the wake
of larger tubes. This is expected to produce a particularly chaotic flow field to
the point of mimicking a higher Reynolds number vortex pattern. This in turn should
result in higher Nusselt numbers and improved thermal performance.
[0043] In another configuration, the lateral or transverse spacing (ST), that is, the spacing
between tubes in a direction transverse to the flow direction (See ST in FIG. 9),
can be selected such that a ratio of the transverse spacing to an average diameter
(D) of the plurality of tubes (ST/D) is between 1.5 and 2.5. Further, the longitudinal
spacing (See SL in FIG. 9), or spacing between tubes in the longitudinal direction,
or parallel to the flow direction A, can be selected such that a ratio of the longitudinal
spacing to an average diameter (D) of the plurality of tubes (SL/D) is between 1.0
and 3.0. These spacings, which can be incorporated into any of the disclosed embodiments
of FIGS. 5-9, can also help to break up any undesirable formation of a vortex street
or resonance, and thereby enhance the useful lifetime of the tube bundle heat exchanger,
and also help to reduce the noise from operating the heat exchanger.
[0044] As set forth herein, it should be appreciated that heat exchanger tubes are arranged
in various different patterns. Further, these different ranges of difference in size.
In one non-limiting configuration, it may be desirable to have a ratio of size of
the large diameter tubes to size of small diameter tubes of greater than 1:1 and up
to about 3:1. Further, in another non-limiting configuration, it is desirable that
the larger diameter tubes have a diameter that is at least about 10% greater than
the diameter of the small diameter tubes.
[0045] In another non-limiting configuration, there is a prescribed range of ratio of the
number of small diameter tubes to large diameter tubes. This range can suitably be
between about 30 and about 70% by number of the plurality of tubes. This blend of
small and large diameter tubes allows for effective arrangement of the tubes such
that the wakes or vortices shed from each tube are cancelled out by other wakes or
vortices shed from other (for example adjacent) tubes.
[0046] The tubes of different diameter can themselves carry a different flow volume of heat
exchange medium, or they can have thicker walls, for example due to hoop stress. While
this might reduce the difference in flow to some extent, generally, the larger diameter
tubes will still have a larger inner diameter and therefore a larger flow area. This
can also be compensated by having fewer large diameter tubes, for example, if it is
desired to do so.
[0047] Heat exchange tubes of differing diameter are readily available and can be obtained
and incorporated into heat exchangers using known techniques.
[0048] It should also be appreciated that although the drawings present the different flow
patterns in terms of a relatively straight flow duct, the principles disclosed herein
are readily applicable to other, potentially more complex, flow ducts and heat exchange
tube patterns, all within the broad scope of the present disclosure.
[0049] As disclosed herein, use of different diameter tubes in tube heat exchangers can
help to ensure that the wake frequency is not similar to the natural frequency of
the tubes, and thereby avoid resonance that can negatively impact the useful life
of the tubes and heat exchanger.
[0050] The foregoing description is exemplary of the subject matter of the invention disclosed
herein. Various non-limiting embodiments are disclosed, however, one of ordinary skill
in the art would recognize that various modifications and variations in light of the
above teachings will fall within the scope of the appended claims. It is therefore
to be appreciated that within the scope of the appended claims, the disclosure may
be practiced other than as specifically described. Thus, the scope of the present
claims is not specifically limited by the details of specific embodiment disclosed
herein, but rather the claims define the full and reasonable scope of the invention.
1. A tube bundle heat exchanger (10), comprising:
a flow space for a first heat exchange medium; and
a plurality of heat exchange tubes (38, 40) for a second heat exchange medium, wherein
the plurality of heat exchange tubes (38, 40) extends at least partially across the
flow space, wherein the plurality of heat exchange tubes (38, 40) comprises at least
a first plurality of tubes (38) having a first diameter and a second plurality of
tubes (40) having a second diameter different from the first diameter.
2. The tube bundle heat exchanger (10) of claim 1, wherein the second plurality of tubes
(40) are positioned relative to the first plurality of tubes (38) such that, during
expected flow conditions through the flow space, wake shedding frequency exhibited
by the plurality of heat exchange tubes (38, 40) does not match natural frequency
of the plurality of heat exchange tubes (38, 40).
3. The tube bundle heat exchanger (10) of claim 1 or 2, wherein the second diameter is
larger than the first diameter.
4. The tube bundle heat exchanger (10) of claim 3, wherein the second plurality of tubes
(40) are positioned in alternating rows relative to the first plurality of tubes (38),
the rows extending transverse to flow direction through the flow space.
5. The tube bundle heat exchanger (10) of claim 4, wherein the first set of tubes (38)
are not aligned with the second set of tubes (40) in the flow direction,
wherein, optionally, the first set of tubes (38) are arranged across the flow direction
of the heat exchanger (10) with gaps defined between each pair of adjacent tubes,
and wherein tubes of the second set of tubes (40) are aligned in the flow direction
with the gaps in the first set of tubes (38).
6. The tube bundle heat exchanger (10) of claim 4, wherein the first set of tubes (38)
and the second set of tubes (40) are aligned with each other in the flow direction.
7. The tube bundle heat exchanger (10) of claim 4, wherein the first plurality of tubes
(38) and the second plurality of tubes (40) are arranged in staggered alternating
rows extending in the flow direction.
8. The tube bundle heat exchanger (10) of any of claims 3 to 7, wherein:
a ratio of second diameter to the first diameter is greater than 1:1 and up to 3:1;
and/or
the second set of tubes (40) has a diameter that is at least 10% larger than the first
set of tubes (38); and/or
the second set of tubes (38) comprises between about 30 and about 70% by number of
the plurality of heat exchange tubes (38, 40).
9. The tube bundle heat exchanger (10) of any of claims 3 to 8, wherein the plurality
of heat exchanger tubes (38, 40) are arranged at a transverse spacing (ST) such that
a ratio of the transverse spacing to an average diameter (D) of the plurality of tubes
(ST/D) is between 1.5 and 2.5.
10. The tube bundle heat exchanger (10) of any of claims 3 to 9, wherein the plurality
of heat exchanger tubes (38, 40) are arranged at a longitudinal spacing (SL) such
that a ratio of the longitudinal spacing to an average diameter (D) of the plurality
of tubes (38, 40) (SL/D) is between 1.0 and 3.0.
11. The tube bundle heat exchanger (10) of any of claims 3 to 10, wherein the second set
of tubes (40) comprises a row of the second set of tubes (40) extending across the
flow direction to reset any wake shedding flow conditions from upstream of the row.
12. The tube bundle heat exchanger (10) of any of claims 3 to 11, wherein the first set
of tubes (38) are arranged in hexagonal patterns around each of the second set of
tubes (40).
13. A method for operating a tube bundle heat exchanger (10) comprising a flow space for
a first heat exchange medium; and a plurality of heat exchange tubes (38, 40) for
a second heat exchange medium, wherein the plurality of heat exchange tubes (38, 40)
extends at least partially across the flow space, wherein the plurality of heat exchange
tubes (38, 40) comprises at least a first plurality of tubes (38) having a first diameter
and a second plurality of tubes (40) having a second diameter different from the first
diameter, the method comprising:
flowing the first heat exchange medium through the flow space at flow conditions to
generate vortex shedding frequency; and
flowing the second heat exchange medium through the plurality of heat exchange tubes
(38, 40) at tube flow conditions to generate natural frequency, wherein the second
set of tubes (40) are positioned such that there is no resonance between the vortex
shedding frequency and the natural frequency.
14. The method of claim 13, wherein:
the flowing steps result in heat exchange between the first heat exchange medium and
the second heat exchange medium; and/or
the second diameter is at least 10% greater than the first diameter.
15. The method of claim 13 or 14, wherein:
tubes of the plurality of heat exchanger tubes (38, 40) are arranged at a transverse
spacing (ST) such that a ratio of the transverse spacing to an average diameter (D)
of the plurality of tubes (ST/D) is between 1.5 and 2.5; and/or
tubes of the plurality of heat exchanger tubes (38, 40) are arranged at a longitudinal
spacing (SL) such that a ratio of the longitudinal spacing to an average diameter
(D) of the plurality of tubes (SL/D) is between 1.0 and 3.0.