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.
Heat exchangers typically have a structure as shown in
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.
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.
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.
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.
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.
In another non-limiting configuration, the legs are arranged at an angle with respect to the lateral plane of between 50 and 80 degrees.
In still another non-limiting configuration, the angle is between 60 and 70 degrees.
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.
In a still further non-limiting configuration, each peak terminates in a rounded peak.
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.
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.
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.
In another non-limiting configuration, the fin pack is bonded to the at least one parting plate at the upward and downward extending peaks.
In still another non-limiting configuration, the at least one parting plate comprises grooves arranged to receive peaks of the fin pack.
In a further non-limiting configuration, the peaks of the fin pack are bonded to the at least one parting plate in the grooves.
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.
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.
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.
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.
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.
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.
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.
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.
A detailed description of non-limiting embodiments of the present disclosure follows, with reference to the attached drawings, wherein:
The disclosure relates to non-conformal triangular offset strip fin heat exchangers.
Referring also to
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.
As also can be seen in both
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 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.
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.
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.
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.
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.
It should be appreciated that a heat exchanger can be made with numerous layers that would be assembled as discussed with respect to
When a stacked conformable heat exchanger is desired, successive layers can be produced with different amounts of curvature, for example as shown in
In this configuration, the outer heat exchange layer or top layer of
It should be appreciated that when prepared with layers of different height, the height of a radially inner layer, or Hinner, would in one non-limiting configuration be less than the height of a radially outer layer, or Houter, for example as shown in
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
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.
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.
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.
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.
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.