Description
Low Profile Heat Exchanger and Method of Making the Same
Technical Field This invention relates to a low profile heat exchanger module for use in heat furnaces, steel melting furnaces, gas turbines which use recuperators and the like, and a method for forming the same.
Background Art United States Patent 3,759,323 issued to Harry J. Dawson et al describes an important prior art primary surface heat exchanger for use as a recupera¬ tor core of a gas turbine. Dawson et al discloses a heat exchanger core made from a multiplicity of thin metal sheets which have been individually cor¬ rugated, or folded in a wavy pattern according to the method described in United States Patent 3,892,119 issued to Miller et al. A large number of these metal plates are stacked on top of each other and the edges of the sheets are crushed to form the flat sections necessary to encase the assembly and to allow the attachment of suitable manifolding for conveying hot and cold fluids. The necessity for crushing the edges results in blockage, and hence the restriction of fluid flow. In addition, the depth of the corrugations in the unit described by Dawson et al is limited by the need to crush the edges. Deep corrugations or pleats cannot be crushed in an organized or predictable manner without causing severe blockage.
The pattern of the corrugations and the relatively
thick crushed edges of the individual sheets described by Dawson et al result in rigidity in all directions in the heat exchanger unit. This may lead to the development of high thermal strains, especially when transient loads are characterized by steep gradients. A major drawback of the prior art heat exchanger construction has been the presence of high stress concentration factors which have resulted from the need to crush the edges. In some applications the effect has been that of producing a multiplicity of cracks. Another problem has been the failure of the weld to penetrate at certain junctions, which results in a preformed crack. While such stress concentration factors may not be significant when the assembly is preloaded in compression, as intended, and when the transients are not steep, high stresses which lead to premature failures may appear under severe operating conditions and after prolonged periods of operation during which the preload is likely to be relaxed.
Disclosure of the Invention
The present invention is directed to a low pro¬ file heat exchanger module made from one or more compact, single sheet primary surface heat exchanger core units. Each unit is formed from a single sheet of thin material which has been pleated to any depth desired. Before pleating, the longitudinal edges of the thin sheet are serrated to provide fluid en¬ trance ramps that minimize blockage, and the surface of the sheet is embossed to define flow passages and provide a means for directing flow and controlling turbulence.
Other objects, advantages and features of the
invention will be more readily apparent from the following detailed description of a preferred embodi¬ ment of the invention when taken together with the accompanying drawings.
Brief Description of the Drawings
Figure 1 is a plan view of a portion of a single sheet of heat exchange material employed to form the heat exchange core of the present invention;
Figure 2 is a plan view of a portion of the single sheet of Figure 1 after embossing to show a "U" flow concept.
Figure 2* is a plan view of a portion of the single sheet of Figure 1 after embossing to show a "Z" flow concept. Figure 3 is a view in side elevation of the single sheet of Figure 2 during the pleating thereof;
Figure 4 is a diagrammatic illustration of a side view of a pleated assembly of the present inven¬ tion; Figure 5 is a diagrammatic illustration of an end view of a pleated assembly of the present inven¬ tion;
Figure 6 is a cross sectional view of the heat exchanger module of the present invention; Figure 7 is a diagrammatic illustration of an end view of the heat exchanger of the present invention;
Figure 8 is a plan view of a portion of a single sheet of heat exchange material of a second embodi¬ ment of the present invention; Figure 9 is a view in side elevation of the single sheet of the embodiment of Figure 8;
Figure 10 is a view in side elevation of the single sheet of the embodiment of Figure 8 during
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pleating thereof;
Figure 11 is a diagrammatic illustration of a third embodiment of the present invention; and
Figure 12 is a diagrammatic illustration of the method of producing the embodiment of Figure 11.
Best Mode For Carrying Out the Invention
Figure 1 illustrates a single sheet used to form one of the pleated assemblies of the heat exchanger module of the present invention. The single sheet, indicated generally at 10, is a long rectangular strip of heat exchange material, for example a suit¬ able thin metal, such as heat resistant steel. The width of the sheet 10 indicated at 12 determines the length of the resulting pleated assembly, and may be varied by the designer to fit the desired heat exchanger application. The longitudinal edges of the sheet are serrated' or cut in a sawtooth pattern so that the distance 14 between notches 16 is about equal to the desired height of the pleated assembly. The apexes or points of the serrated edge are shown at 18, and the distance of an edge 20 extending be¬ tween notch 16 and point 18 should preferably be equal to the height of the pleated assembly as indi- cated at 14 to eliminate fluid flow blockage. For example, the assembly may be about 1-2 inches in height at 14 and the width 12 may be about 6-7 inches.
Obviously, the configuration of the serrated edges of the sheet 10 can be altered to meet varying structural requirements. For example, the apexes 18 may be rounded instead of pointed, and the edge 20 can be curved rather than straight.
The pleated assembly is formed in a manner de-
picted in Figures 2 and 3 or 2' and 3. The serrated sheet of heat exchange material 10 is divided into sections or walls 22 and 24 whcih are embossed by means of conventional dies, shaped rollers or any other embossing techniques;. The embossing serves to separate the subsequently formed pleats of the heat exchanger accurately and to guide the fluid flow through the completed heat exchanger. The em¬ bossing may space the pleats for a distance of about .030 inches.
As illustrated in Figures 2 and 2*, each section 22 and 24 may be embossed in a U-shaped or Z-shaped configuration respectively as shown by the rows of bosses 26 on section 22 and the rows of bosses 28 on section 24. While only four rows of bosses 26 and four rows of bosses 28 are shown, the number of rows could be much higher and is limited only by the size of the sections 22 and 24. Fluid flow channels 27 are defined on' the face of each section 22 and 24 between the rows of bosses 26 and 28. The interruptions between bosses in a row induce fluid turbulence in the flow path defined thereby and thus enhance the heat transfer characteristics of the pleated assembly formed from the sheet 10. Since the sheet 10 will be pleated into a pleated assembly which forms part of the core of the heat exchanger module depicted in Figure 6, it is necessary to emboss the sheet so that the pleats are spaced far enough apart to allow fluid flow between them. This is accomplished by embossing sections 22 and 24 in opposite directions. Thus in Figure 2, the bosses 26 on section 22 project upwardly, while the bosses 28 on section 24 project downwardly. This alternate arrangement is maintained throughout the
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length of the sheet 10.
Once the sheet 10 is embossed, the sheet is pleated by folding it along lines or crest portions 34 between the sections or walls 22 and 24. Pleat- ing may be accomplished mechanically in any conven¬ tional manner, such as on machines utilizing dull- edged knife blades like those used for pleating filter paper in the manufacture of air cleaners and oil fil¬ ters, but which have been modified to pleat thin metal or heat exchange material rather than paper. Figure 3 shows the embossed sheet 10 being pleated and compressed at the lower end 36 to form the pleated assembly shown in Figure 4. The sections 22 and 24 of the sheet are compressed together until the raised bosses 26 and 28 contact the next adjacent section of the sheet. Thus the height of such bosses accurately controls the spacing between adjacent sections when the sheet 10 is pleated and compressed. To enable the bosses to perform this spacing function, it is imperative that the bosses on adjacent sections 22 and 24 be precluded from nesting when the sec¬ tions are compressed together. This may be accom¬ plished, as illustrated in Figure 2, by placing the bosses on section 24 so that they fall in the spaces between the bosses on section 22 when the two sections are pleated. In addition, the bosses may be of different depths, and it is possible to have both deep and shallow bosses on the same sheet. When sheet 10 is pleated and compressed as at 36 in Figure 3, a side view of the pleated assembly would appear as illustrated in Figure 4, but without items 40 in which the pleated assembly is indicated generally as 38. The embossing is omitted for clarity, but in actuality the fluid flow paths are defined
by the bosses previously described. Inclined fluid entrance ramps are formed by edges 20, between notches 16 and points 18, and the pleated assembly is in part held together by means of corrugated strips 40 which are welded to points 18 across each end of the assembly. This is shown in Figure 5, which depicts an end view of the pleated assembly, not showing the corrugated strip 40. The pleated as¬ sembly is also held together by welds 42 and 44 which plug one side of the open ends of the fluid passages between sections 22 and 24, leaving the remaining sides 43 and 45 open. The passages are plugged at both ends, although only one end is shown in Figure 5. Additional external clamping may be provided to preload the heat exchanger pleats.
The junction of points 18 and welds 42 and 44 creates a relativley inelastic, rigid assembly. However, if such an inelastic area is attached to a relatively elastic area, high thermal stresses cannot be generated. Since the corrugated strip permits limited flexibility along the overall width of the edge 38* which is distant from the weld zone and provides flexibility, and therefore high thermal stresses are substantially elimi- nated.
It will be noted with reference to Figure 5, that the welds 42 above the corrugated strip 40 are staggered with relation to the welds 44 below the strip. Thus fluid entry to every other fluid passage occurs above the strip while fluid entry to the inter¬ mediate fluid passages occurs below the strip. How¬ ever, since the edges 20 bordering the entry to a
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fluid passage form an inclined ramp having a length equal to the total height of the pleated assembly, unrestricted fluid flow into each passage is assured. The heat exchanger module 46 of the present invention may be formed by stacking at least two pleated assemblies 38 within a housing 48 as shown in Figure 6. The upper pleated assembly 38a is placed over the lower pleated assembly 38b with a spacer 50 between them. The spacer 50 is essentially either a solid sheet or a mesh or perforated strip and is shown extending along the entire length of line 34 between sections of the pleated assemblies from point 52 to point 54. However, the spacer 50 may be placed so that it stops short of points 52 and 54. It is possible, by varying the thickness and the length of the spacer 50, to reduce fluid flow blockage be¬ yond the reduction achieved by means of the fluid entry ramps defined by edges 20. As previously men¬ tioned in discussing Figure 1, the length of edges 20 should be equal to pleat depth 14 to minimize fluid flow blockage. Although the ramps are shown to be straight, longer ramps may be achieved within the same dimensions by curving edges 20, thus length¬ ening the ramps while maintaining the compactness of the unit.
Hot and cold fluid manifolds are attached to the ends of the two stacked pleated assemblies as shown in Figure 6, and result in a low profile heat exchanger. Inlet manifolds 56 provide hot fluid, for example hot exhaust gas from a gas turbine, through fluid passages 58. This hot fluid follows the path shown by the white arrows 58 to outlet manifolds 60 which collect the previously hot fluid after heat has been transferred therefrom in the heat exchanger
σore. Since the heat exchanger of the present inven¬ tion is a counterflow type heat exchanger, cool fluid, as, for example air from the compressor of a gas turbine engine, is supplied to the path shown by arrows 64 by a cool fluid inlet manifold 62. This cool fluid flows through the pleated assemblies 38a and 38b along the paths indicated by the dark arrows, is heated, and then is collected by an outlet mani¬ fold 66. The corrugated strips 40 are preferably welded to the housing 48 to form the manifolding. The width of corrugated strip 40 introduces a desired flexi¬ bility into the heat exchanger unit, as it allows the reduction of stresses in the presence of thermal gradients. It is also possible, but less desirable, to weld rigid manifolding directly to the pleated assemblies, which is not shown in Figure 6. However, this means of attaching the manifolding to the pleated assembly does not provide the flexibility and conse- quent dissipation of thermal stresses possible with the arrangement shown in Figure 6.
Figure 7 illustrates an end view of the heat exchanger module 46 used as a recuperator for re¬ ceiving hot exhaust gas and compressed air from a gas turbine engine. Hot gas input manifolds 56 are at the top and bottom and the hot combustion air output manifold 66 is in the center. Hot gas flows in alternate passages 58 while air to be heated flows in the opposite direction through the intermediate passages 64. The housing 48 closes the open ends of the passages 58.
A second embodiment of the present invention is diagrammatically shown in Figures 8, 9, and 10. Heat exchanger sheet material 72, which has been
serrated along the longitudinal edges in the same manner as sheet 10 in Figure 1 and subsequently em¬ bossed, is bent between points 68 and 70 by passing it over shaped rollers, which are not shown in Figure 8, prior to pleating to form a sheet which is rippled in cross section (Figure 9). This structure provides flexibility to the pleats in the direction 68-70. Figure 10, which corresponds to Figure 3, shows the rippled sheet 72 being pleated and compressed into a bent pleated assembly 74. The method depicted in Figures 8, 9, and 10 results in increased flexibil¬ ity, not only in the pleats themselves, but also in the welded plugs 42 and 44 used to seal alternate flow passages as shown in Figures 5 and 7. Additional flexibility in the direction of sheet width 12 shown in Figure 1 can be introduced in still another embodiment of the present invention. The compressed pleated assembly shown at 36 in Figure 3 can be made to assume an arcuate shape or even an *S" shape, (not shown) when viewed in the direction of the crest portions or edges 34, as depicted in Figure 11.
Finally, the sheet 10 can be treated in an al¬ ternate method after pleating to enhance fluid flow and flexibility* This is accomplished as shown in Figure 12. A pleated and compressed sheet, indi¬ cated generally at 76, is passed over a roller 78, which causes the pleats to separate as at 80 while remaining compressed at 82, thus allowing cams, rollers, pawls, or other suitable mechanisms to be introduced into the wide gaps at 80 to spread the pleats at edge 34 to any desired distance. After passing over roller 78, the pleated and compressed sheet passes over roller 84 where the wide gaps 80 become compressed
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at 86 and the pleats which were compressed at 82 become separated at 88, thus permitting the same type of cams, rollers or pawls to bow the pleats as at 34, resulting in a compact and bowed, pleated assembly after the core passes over the roller 84 as shown in Figure 11. This introduces flexibility in the direction of the width of the strip thus minimizing thermal stresses.
Industrial Applicability The heat exchanger module 46 may be effectively employed as a recuperator for a gas turbine engine or for other heat exchange applications, as, for example, in steel heat treating or melting furnaces. The inlet manifold 62 is connected to a source of cool fluid to be heated while the inlet manifolds 56 are connected to a source of heated fluid. In a gas turbine engine, the inlet manifolds 56 would be connected to receive hot exhaust gases from the engine while the inlet manifold 62 would be connected to receive compressor discharge air from the engine. As the cooler discharge air passes through the pleated assemblies 38a and 38b with the counter flowing hot exhaust gas, the air is heated by the heat transfer provided by heat exchange sections 22 and 24. The exhaust gas then passes out of the outlet manifolds 60 and is normally vented to the atmosphere while the heated air passes to the outlet manifold 66. This outlet manifold is connected to the σombustor of the gas turbine engine and proceeds on through the engine in the conventional manner.
Other aspects, objects and advantages of this invention can be obtained from a study of the draw¬ ings, the disclosure, and the appended claims.