BACKGROUND OF THE DISCLOSURE
[0001] This disclosure relates to heat exchangers and, more particularly, to a conformal
heat exchanger having triangular offset strip fins that allow the heat exchanger to
bend along the flow direction of the fin pack.
[0002] Heat exchangers typically have a structure as shown in FIG. 1, also further discussed
below, wherein the heat exchanger is a stack of rigid components, for example, to
define hot side and cold side flows, and are brazed together to form a monolithic
cube. This leads to a rectangular, or box-shaped, non-conformal geometry. This type
of heat exchanger is effective in heat exchange with one or more fluids, but can be
difficult to accommodate in spaces that are not well suited to a box-shaped article.
[0003] Numerous applications of heat exchangers do not have a convenient box-shaped space
to accept a heat exchanger. As one example, gas turbine engines use heat exchangers,
and the spaces available are frequently annular or at least round in shape. Known
box-shaped heat exchangers can be difficult to utilize in such spaces.
SUMMARY OF THE DISCLOSURE
[0004] The present disclosure relates to a conformable or conformal heat exchanger which
can be bent or curved along a length of the flow passages defined in the heat exchanger.
[0005] In one non-limiting embodiment, a fin pack for a conformal heat exchanger, comprises
alternating rows of fins defined in a lateral plane, each row of fins comprising alternating
upward and downward extending peaks extending upwardly and downwardly from the lateral
plane, wherein adjacent rows of fins are connected by central portions in the lateral
plane, and wherein upward and downward extending peaks of adjacent rows are offset
from each other along the rows.
[0006] In a further non-limiting configuration, each upward extending peak of one row is
laterally aligned with a downward extending peak of an adjacent row.
[0007] In a still further non-limiting configuration, the upward and downward extending
peaks comprise legs extending between the lateral plane and the peak, and the central
portions comprise horizontal connecting portions defined in the plane, wherein the
horizontal connecting portions connect legs of alternating upward and downward extending
peaks along each row, and the horizontal connecting portions also connect to horizontal
connecting portions of each adjacent row.
[0008] In another non-limiting configuration, the legs are arranged at an angle with respect
to the lateral plane of between 50 and 80 degrees.
[0009] In still another non-limiting configuration, the angle is between 60 and 70 degrees.
[0010] In a further non-limiting configuration, the fin pack is defined from sheet metal
such that the central portions are contiguous sheet metal material with the adjacent
rows.
[0011] In a still further non-limiting configuration, each peak terminates in a rounded
peak.
[0012] In another non-limiting configuration, the rounded peak is defined in a material
having a thickness, and an inner radius of the rounded peak (IR) is greater than one-half
the thickness of the material.
[0013] In still another non-limiting configuration, the fin pack is flexible at the central
portions and, when bending at the central portions, an upward extending peak of one
row extends into a space created by a downward extending peak of the adjacent row.
[0014] In a further non-limiting embodiment, a conformal heat exchanger comprises the fin
pack as disclosed herein; and at least one parting plate arranged along the fin pack
in contact with at least one of the upward and the downward extending peaks.
[0015] In another non-limiting configuration, the fin pack is bonded to the at least one
parting plate at the upward and downward extending peaks.
[0016] In still another non-limiting configuration, the at least one parting plate comprises
grooves arranged to receive peaks of the fin pack.
[0017] In a further non-limiting configuration, the peaks of the fin pack are bonded to
the at least one parting plate in the grooves.
[0018] In another non-limiting configuration, the heat exchanger further comprises side
bars arranged along ends of the rows to define heat exchange flow paths along the
upward and downward extending peaks.
[0019] In still another non-limiting configuration, the at least one parting plate and the
fin pack are curved around an axis extending parallel to the rows.
[0020] In a further non-limiting embodiment, a method for making a conformable heat exchanger,
comprises die stamping a sheet of metal to produce a fin pack comprising alternating
rows of fins defined in a lateral plane, each row of fins comprising alternating upward
and downward extending peaks extending upwardly and downwardly from the lateral plane,
wherein adjacent rows of fins are connected by central portions in the lateral plane,
and wherein upward and downward extending peaks of adjacent rows are offset from each
other along the rows; positioning the fin pack between a first parting plate in contact
with the downward extending peaks and a second parting plate in contact with the upward
extending peaks; and bonding the upward and downward extending peaks to the first
parting plate and the second parting plate to define the conformable heat exchanger.
[0021] In a non-limiting configuration, the method further comprises bending the conformable
heat exchanger around an axis parallel to the rows of the fin pack.
[0022] In a further non-limiting configuration, the first parting plate and the second parting
plate comprise grooves arranged to receive peaks of the fin pack, wherein the positioning
step positions the peaks in the grooves, and wherein the bonding step bonds the peaks
in the grooves.
[0023] In a still further non-limiting configuration, the method further comprises positioning
side bars along non-flow edges of the fin pack between the first parting plate and
the second parting plate, and wherein the bonding step also bonds the side bars to
the first parting plate and the second parting plate.
[0024] In another non-limiting configuration, the method further comprises making a plurality
of conformable heat exchangers and bending the plurality of conformable heat exchangers
to produce a plurality of curved conformable heat exchangers, and stacking the plurality
of curved conformable heat exchangers to produce a final multi-layer curved conformable
heat exchanger wherein each layer has a height measured as distance between the first
parting plate and the second parting plate, and wherein the plurality of curved conformable
heat exchangers have different heights with respect to each other.
[0025] 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
[0026] A detailed description of non-limiting embodiments of the present disclosure follows,
with reference to the attached drawings, wherein:
FIG. 1 illustrates a conventional box-shaped heat exchanger;
FIG. 2 illustrates a conventional offset fin configuration;
FIG. 3 illustrates a conformal triangular offset strip fin pack as disclosed herein;
FIG. 4 is a top view of a portion of FIG. 3;
FIG. 5 is a side view of a portion of two adjacent rows;
FIG. 6 is a side view of a central or connecting portion as disclosed herein;
FIG. 7 illustrates how a conformable fin pack as disclosed herein can flex along a
row.
FIG. 8 further illustrates a fin pack as disclosed herein, in this configuration formed
around a curved configuration;
FIG. 9 illustrates a parting plate with grooves for accommodating peaks of a fin pack;
FIGS. 10 and 11 present an enlarged view of a groove (FIG. 10) with a downward peak
(FIG. 11) held within the groove.
FIG. 12 illustrates assembly of a heat exchanger as disclosed herein;
FIGS. 13A-13C illustrates steps of bending a conformable heat exchanger as disclosed
herein; and
FIG. 14 illustrates stacked conformal heat exchangers.
DETAILED DESCRIPTION
[0027] The disclosure relates to non-conformal triangular offset strip fin heat exchangers.
[0028] FIG. 1 shows, in a partially exploded view, a conventional heat exchanger 1 wherein
corrugated fins 2, 3 are arranged on either side of flat plates 4 or brazing sheets,
with side bars 5 to seal flows from one another. The partially exploded assembly of
FIG. 1 is brazed into a box-shaped heat exchanger 1. Such a heat exchanger is rigid
and not conformal, and therefore is difficult to incorporate into some spaces.
[0029] FIG. 2 illustrates a conventional strip fin configuration 6 wherein rows 7 of fins
8 are stamped into sheet metal. The fins in adjacent rows are offset from each other,
and have substantially flat tops and bottoms as shown. Further, adjacent rows are
still connected to each other at top and bottom portions 9. While effective at heat
exchange in the proper situation, this type of fin structure or fin pack still has
no flexibility or ability to bend around an axis parallel to rows 7.
[0030] FIG. 3 illustrates a fin pack 10 of one disclosed embodiment wherein the fin pack
10 is defined by offset strips or rows 12 of fins, in this configuration triangular
fins 14. Fins 14 are defined by alternating upward and downward directed peaks 16,
18 that are connected along rows 12 by a central portion 20 which, in the illustrated
configuration, can be a substantially horizontal portion defined between legs 22 of
upward peaks 12 and legs 24 of downward peaks 18. Central portion 20 can define a
center plane of the fin pack. Fins 14 define a flow direction corresponding to flow
that will pass through fins 14 substantially transverse to rows 12, as illustrated
by arrow A.
[0031] Referring also to FIG. 4, a top-down view of a portion of fin pack 10 of FIG. 3 further
illustrates features of central portion 20. In addition to connecting successive peaks
16, 18 along a row 12, central portions 20 also connect adjacent rows 12. Further,
in one non-limiting configuration, central portion 20 is the only connection between
adjacent rows 12 as this allows bending or flexing of one row 12 relative to the next
row 12 at central portion 20, while offset peaks 16, 18 do not interfere with each
other during such flexing or bending. Still referring to FIG. 4, gaps can be seen
between rows 12. These gaps 12 can be provided in numerous ways, but can be lanced
during stamping of the structure, in one embodiment, as will be further discussed
below.
[0032] It is noted that fins 14 are described herein as having upward and downward peaks
16, 18. These directional orientations are taken with respect to a plane drawn through
fin pack 10, specifically through a central plane defined by central portions 20,
and considered when this plane is horizontal. It should of course be appreciated that
in use, the peaks may be oriented differently, for example if fin pack 10 is incorporated
into a heat exchanger to be mounted in an annular space of a gas turbine engine, then
the central portions 20 and center plane of the fin pack might not be horizontal.
Nevertheless, for purposes of disclosure, the upward and downward peaks 16, 18 should
be considered with respect to a horizontal center plane of the fin pack.
[0033] As also can be seen in both FIGS. 3 and 4, in adjacent rows 12, upward peaks 16 and
downward peaks 18 are offset from each other. Specifically, the offset is along row
12 such that an upward peak 16 is not adjacent to another upward peak in the adjacent
row. In the illustrated configuration, each upward peak 16 in one row 12 is adjacent
to a downward peak 18 in an adjacent row 12. As will be further discussed below, configuring
adjacent rows to be connected only by central portions 20, with upward and downward
peaks 16, 18 offset from each other, fin pack 10 can bend around an axis B that can
be substantially transverse to the longitudinal direction of extent of rows 12, or
that can be substantially parallel to the direction of flow. This greatly improves
the conformability of fin pack 10 as disclosed herein, especially as compared to the
configurations of FIGS. 1 and 2.
[0034] FIG. 5 is a side view along the flow direction A (FIG. 3) to further illustrate details
and configuration of peaks 16, 18, central portions 20 and legs 22, 24. As shown,
central portions 20 connect adjacent rows 12 in the flow direction and also connect
successive peaks 16, 18 in the direction of rows 12. Further, central portions define
a lateral plane from which upward and downward peaks 16, 18 extend.
[0035] FIG. 6 further illustrates a continuous connection region or central portion 20 between
successive legs 22, 24 along row 12. This configuration can be advantageous for numerous
reasons. First, this structure allows the fin pack to be conformable by allowing fin
pack 10 to bend along the flow direction, that is, around an axis B (FIG. 8) that
is substantially parallel to rows 12 and substantially transverse to the flow direction.
[0036] FIG. 7 illustrates how the disclosed configuration allows this flexibility. FIG.
7 illustrates a section through three adjacent rows 12a, 12b, 12c. Peaks 16 of rows
12a and 12c are offset from the peak 16 of row 12b, and instead peaks 16 are aligned
with a space between offset peaks 16 (not visible in FIG. 7) of row 12b. When fin
pack 10 as disclosed herein is flexed around axis B, upward peaks 16 of rows 12a and
12c can bend into a gap between legs of an adjacent peak because the adjacent peak
in row 12b is a downward peak 18. This is schematically illustrated by the broken
line position shown for upward peaks 16 on the left and right side of the figure,
bending into open space created by virtue of the fact that the adjacent upward peaks
are on either side of a downward peak 18. During such bending, fin pack 10 bends at
central portion 20. It should be noted that the broken line position of peaks 16 shown
in FIG. 7 would correspond to bending of fin pack 10 upwardly. In a configuration
where fin pack is to bend downwardly, adjacent rows 12 would pivot in the opposite
direction, with peak 18 of row 12b occupying space between peaks 18 (not visible in
FIG. 7) of rows 12a and 12b. This curvature is shown in FIG. 8 discussed below. Also,
it should be appreciated that while this discussion is in terms of a simple curvature
of fin pack 10, for example a single radius of curvature as shown in FIG. 8, fin pack
10 as disclosed herein also allows complex curvature of the fin pack, including curving
in portions that are in opposite directions, that is, some curving that is convex
upwardly and some curving that is convex downwardly. This flexibility greatly enhances
the ability for the fin pack as disclosed herein to be used in positions where conformability
is needed.
[0037] FIG. 8 illustrates a conformable fin pack 10 curved around axis B, or along the flow
direction. In this illustration, fin pack 10 is supported on a parting plate 28. Parting
plates 28 can be used to complete fin pack 10 into a heat exchanger, closing off upper
and lower surfaces of the intended flow area.
[0038] FIG. 9 further illustrates a parting plate 28 which, in this configuration, has a
series of grooves 30 sized to receive peaks 18 (or 16) of a fin pack 10. FIGS. 10
and 11 further illustrate grooves 30, which receive peaks 16, 18 and, in one configuration,
can be brazed or otherwise joined such that peaks are firmly held in grooves, preferably
mechanically and also through bonded material.
[0039] The depth of grooves can be selected to provide as much support for the rounded peaks
of the fin pack as desired. Shallow grooves, for example about 0.001 (0.025 mm) inches
in depth, can be useful as providing contact area to support and enhance bonding of
a peak positioned in the groove. A deeper groove increases the contact area, but also
requires more machining and can lead to the need for a parting plate of greater thickness
that may not be desired.
[0040] FIG. 12 illustrates an assembly process for assembling a heat exchanger 32 including
a fin pack 10 as disclosed herein.
[0041] First, fin pack 10 can be formed through a number of different processes. One process,
however, is to obtain a substantially flat sheet of material, and stamp the material
to form the desired offset fins and also to separate adjacent rows except for central
portions 20. Such a stamping process is one desirable manner of making fin pack 10
but a person skilled in the art will readily recognize that other manufacturing techniques
could be utilized to obtain the desire structure.
[0042] Next fin pack 10 is positioned on a parting plate 28 with downward peaks 18 located
in grooves 30. Side bars 34 can be positioned on parting plate 28 on either side of
fin pack 10 to further define the desired flow direction along arrow A.
[0043] Another parting plate 28 (a top parting plate) can then be positioned on top of fin
pack 10 and side bars 34, with upward peaks 16 in grooves 30 of top parting plate
28.
[0044] Once the components are assembled as described, the components can then be brazed
together. One particularly suitable manner of bonding includes Fast Assisted Sintering
Technique (FAST) or Spark Plasma Sintering (SPS) technique.
[0045] It should be appreciated that a heat exchanger can be made with numerous layers that
would be assembled as discussed with respect to FIG. 12. When it is not needed for
the heat exchanger to be conformable, then all layers can be assembled and then brazed
at the same time into a cube or box-shape. However, when it is desired for the heat
exchanger 32 to be conformable, then a single layer assembled and brazed as discussed
above can then be rolled to obtain the desired curve. This is illustrated in FIGS.
13A-13C, where a flat heat exchanger 32 is the starting configuration, manufactured
for example as discussed above. This flat assembly can then be passed through rollers
to gradually introduce the desired curve to the assembly.
[0046] FIG. 13B shows a curve of heat exchanger 32 after a first pass through rollers, and
FIG. 13C shows a final curvature, after sufficient passes through the rollers. For
this purpose, in one non-limiting configuration, a 3-4 bar roller is suitable.
[0047] When a stacked conformable heat exchanger is desired, successive layers can be produced
with different amounts of curvature, for example as shown in FIG. 14, where the bottom
heat exchange layer is curved the most, and the top is curved the least. As shown
in FIG. 14, another fin structure 36 can be introduced between each of the conformable
heat exchangers 32 to be stacked, for example to produce a cross-flow heat exchanger.
These fin structures 36 could be any conventional folded fin pack, and would be arranged
to carry the other fluid stream with which heat exchange is to be conducted. Arranged
in the orientation shown in FIG. 14, conventional fin structures have sufficient flexibility
in this direction to fit between the adjacent heat exchangers 32 and curve to the
appropriate shape or configuration.
[0048] In this configuration, the outer heat exchange layer or top layer of FIG. 14 may
have a longer arc length as compared to the lower heat exchange layer(s) or heat exchangers
32. This can lead to increased pressure loss and reduced mass flow, but can be compensated
by having different passage height for each layer, that is, the height of the inner
or lower heat exchanger layer in FIG. 14 (H
inner) can be less than the height of the outer or upper heat exchanger layer (H
outer). In this regard, it should be appreciated that the height of a layer is defined
as the space between the parting plates of the layer. With heat exchangers 32 being
conformable and, for example, being combined into a curved structure as is illustrated
in FIG. 14, and with the different layers of a stacked structure having a different
height, this serves to balance the mass flow through the layers and avoid the problems
that might otherwise be caused by an imbalanced mass flow.
[0049] It should be appreciated that when prepared with layers of different height, the
height of a radially inner layer, or H
inner, would in one non-limiting configuration be less than the height of a radially outer
layer, or H
outer, for example as shown in FIG. 14.
[0050] The fin pack 10 as disclosed herein has been referred to as having triangular fins.
This refers to the shape of the fins wherein each peak is defined where two legs meet,
at a rounded peak. It should be appreciated that the fins as disclosed herein do not
need to be strictly triangular, but this is one configuration of particular interest.
Further, and as discussed above, legs defining successive peaks along a row are separated
by lateral or horizontal central portions 20 (see FIG. 6), and this can be advantageous
as offset upper and lower leg segments can help to offset or accommodate thermal expansion.
Further, with the shape of fins as disclosed herein, pressure loading is concentrated
at the central portion, and the rounded interface of the peaks within grooves helps
to prevent buckling during bonding.
[0051] As mentioned herein, the peaks of each defined fin can be rounded peaks, and in one
non-limiting configuration, each rounded peak can have an inner radius (IR) which
can be greater than or equal to one-half of a thickness of the material from which
the rounded peaks are formed.
[0052] The legs of the fins of fin pack 10 can be angled for wider or narrower spacing,
and this spacing can help to provide fin pack 10 with desired properties to handle
or respond to stress during assembly, bonding and use. In one non-limiting configuration,
the legs can be angled relative to the horizontal plane in which connection portions
20 are defined, at an angle between 50 and 80 degrees, or between 60 and 70 degrees,
and angles of 60 or 70 degrees are particularly suitable.
[0053] During use, the heating and cooling to which heat exchanger 32 is exposed will induce
stress into the component, for example at central portion 20. This may ultimately
lead to portions of the fin pack to break, but the fin pack will nevertheless remain
bonded to the parting plates and side bars.
[0054] It should be appreciated that a conformable fin pack and heat exchanger have been
disclosed herein which allow a heat exchanger to be used in conformable manner to
fit available areas that do not readily accept a box-shaped heat exchanger, thereby
helping to put better use to available space, for example in the context of a gas
turbine engine.
[0055] 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 fin pack (10) for a conformal heat exchanger (32), comprising:
alternating rows (12) of fins (14) defined in a lateral plane, each row (12) of fins
(14) comprising alternating upward and downward extending peaks (16, 18) extending
upwardly and downwardly from the lateral plane, wherein adjacent rows (12) of fins
(14) are connected by central portions (20) in the lateral plane, and wherein upward
and downward extending peaks (16, 18) of adjacent rows (12) are offset from each other
along the rows (12).
2. The fin pack (10) of claim 1, wherein each upward extending peak (16) of one row (12)
is laterally aligned with a downward extending peak (18) of an adjacent row (12).
3. The fin pack (10) of claim 1 or 2, wherein the upward and downward extending peaks
(16, 18) comprise legs (22, 24) extending between the lateral plane and the peak (16,
18), and wherein the central portions (20) comprise horizontal connecting portions
defined in the plane, wherein the horizontal connecting portions connect legs (22,
24) of alternating upward and downward extending peaks (16, 18) along each row (12),
and the horizontal connecting portions also connect to horizontal connecting portions
of each adjacent row (12),
wherein, optionally, the legs (22, 24) are arranged at an angle with respect to the
lateral plane of between 50 and 80 degrees,
wherein, further optionally, the angle is between 60 and 70 degrees.
4. The fin pack (10) of claim 1, 2 or 3, wherein the fin pack (10) is defined from sheet
metal such that the central portions (20) are contiguous sheet metal material with
the adjacent rows (12).
5. The fin pack (10) of any preceding claim, wherein each peak (16, 18) terminates in
a rounded peak,
wherein, optionally, the rounded peak is defined in a material having a thickness,
and wherein an inner radius of the rounded peak (IR) is greater than one-half the
thickness of the material.
6. The fin pack (10) of any preceding claim, wherein the fin pack (10) is flexible at
the central portions (20) and, when bending at the central portions (20), an upward
extending peak (16) of one row (12) extends into a space created by a downward extending
peak (18) of the adjacent row (12).
7. A conformal heat exchanger (32), comprising:
the fin pack (10) of any preceding claim; and
at least one parting plate (28) arranged along the fin pack (10) in contact with at
least one of the upward and the downward extending peaks (16, 18).
8. The heat exchanger (32) of claim 7, wherein:
the fin pack (10) is bonded to the at least one parting plate (28) at the upward and
downward extending peaks (16, 18); and/or
the at least one parting plate (28) comprises grooves (30) arranged to receive peaks
(16, 18) of the fin pack (10), wherein, optionally, the peaks (16, 18) of the fin
pack (10) are bonded to the at least one parting plate (28) in the grooves (30).
9. The heat exchanger (32) of claim 7 or 8, further comprising side bars (34) arranged
along ends of the rows (12) to define heat exchange flow paths along the upward and
downward extending peaks (16, 18).
10. The heat exchanger (32) of claim 7, 8 or 9, wherein the at least one parting plate
(28) and the fin pack (10) are curved around an axis extending parallel to the rows
(12).
11. A method for making a conformable heat exchanger (32), comprising:
die stamping a sheet of metal to produce a fin pack (10) comprising alternating rows
(12) of fins (14) defined in a lateral plane, each row (12) of fins (14) comprising
alternating upward and downward extending peaks (16, 18) extending upwardly and downwardly
from the lateral plane, wherein adjacent rows (12) of fins (14) are connected by central
portions (20) in the lateral plane, and wherein upward and downward extending peaks
(16, 18) of adjacent rows (12) are offset from each other along the rows (12);
positioning the fin pack (10) between a first parting plate (28) in contact with the
downward extending peaks (18) and a second parting plate (28) in contact with the
upward extending peaks (16); and
bonding the upward and downward extending peaks (16, 18) to the first parting plate
(28) and the second parting plate (28) to define the conformable heat exchanger (32).
12. The method of claim 11, further comprising bending the conformable heat exchanger
(32) around an axis parallel to the rows (12) of the fin pack (10).
13. The method of claim 11 or 12, wherein the first parting plate (28) and the second
parting plate (28) comprise grooves (30) arranged to receive peaks (16, 18) of the
fin pack (10), wherein the positioning step positions the peaks (16, 18) in the grooves
(30), and wherein the bonding step bonds the peaks (16, 18) in the grooves (30).
14. The method of claim 11, 12 or 13, further comprising positioning side bars (34) along
non-flow edges of the fin pack (10) between the first parting plate (28) and the second
parting plate (28), and wherein the bonding step also bonds the side bars (34) to
the first parting plate (28) and the second parting plate (28).
15. The method of any of claims 11 to 14, further comprising making a plurality of conformable
heat exchangers (32) and bending the plurality of conformable heat exchangers (32)
to produce a plurality of curved conformable heat exchangers (32), and stacking the
plurality of curved conformable heat exchangers (32) to produce a final multi-layer
curved conformable heat exchanger (32) wherein each layer has a height measured as
distance between the first parting plate (28) and the second parting plate (28), and
wherein the plurality of curved conformable heat exchangers (32) have different heights
with respect to each other.