MICRO-TUBE METAL MATRIX HEAT EXCHANGER AND METHOD OF MANUFACTURE

Abstract

A heat exchanger is characterized by having two or more fluid flow circuits, each formed by multiple small cross-section “micro-tubes” contained within a surrounding metal structure, or “metal matrix.” Its function is to efficiently transfer heat from one fluid to another in a highly compact assembly. Most any metal or metal alloy can be considered for the micro-tubes. The micro-tubes, while typically arranged in alternating layers of alternating flow circuits, may be organized in any number of arrangements including co-linear and at cross angles to provide for co-flow, counter flow and cross flow. The metal matrix, is provided in one embodiment by a metal or metal alloy powder consolidated in a hot isostatic pressing (HIP) process. This process also joins the tubes together and to the matrix itself, producing a monolithic structure.

Claims

1. A method for forming a heat exchanger for transferring heat between two separate fluids, the method including the steps of: arranging a plurality of first tubes formed of a first material adjacent to a plurality of second tubes formed of a second material, and with interstices between the plurality of first tubes and the plurality of second tubes; at least partially filling the interstices of said arranging step with a metal powder formed of a third material, the third material different from at least the first material; at least partially filling at least some of the plurality of first tubes and/or the plurality of second tubes with a removable support media; and raising a combination of the plurality of first tubes, the plurality of second tubes, and the metal powder up to a sintering temperature for the third material, to sinter the metal powder into a metal matrix between the plurality of first tubes and the plurality of second tubes.

2. The method of claim 1 wherein said at least partially filling step includes the media having a melting point higher than the sintering temperature.

3. The method of claim 1 including the further step of removing the media after said raising step.

4. The method of claim 1 wherein said heating step occurs under pressure greater than atmospheric pressure.

5. The method of claim 4 wherein said heating step occurs within a hot isostatic press.

6. The method of claim 5 wherein the first material and the second material of said arranging step are different from each other.

7. The method of claim 5 wherein the first material and the second material of said arranging step are the same.

8. The method of claim 1 wherein said arranging step includes the first material forming the plurality of first tubes having a melting point higher than the temperature of said raising step.

9. The method of claim 1 wherein said arranging step includes the plurality of first tubes having a circular cross-section.

10. The method of claim 1 wherein said arranging step includes the plurality of first tubes and the plurality of second tubes being arranged with elongate central axes thereof parallel to each other for at least a portion of a length of the plurality of first tubes and the plurality of second tubes.

11. The method of claim 10 wherein said arranging step includes the plurality of first tubes and the plurality of second tubes being arranged in planar layers which alternate with each other.

12. The method of claim 11 wherein said arranging step includes the plurality of first tubes and the plurality of second tubes being arranged in a hexagonal close packed arrangement.

13. The method of claim 1 wherein the plurality of first tubes and the plurality of second tubes of said arranging step are arranged in a counter-flow relationship within the heat exchanger.

14. The method of claim 1 wherein said first set of tubes and said second set of tubes of said arranging step are arranged in a cross-flow relationship within the heat exchanger.

15. The method of claim 1 wherein at least the plurality of first tubes of said arranging step include protuberances on an inside surface of the plurality of first tubes, said protuberances enhancing a surface area of said inside surface of the plurality of first tubes relative to a plain cylindrical inside surface.

16. The method of claim 1 wherein said arranging step includes the heat exchanger having two pairs of opposing faces including two opposing side faces and two opposing end faces, said opposing side faces supporting opposing ends of the plurality of first tubes, said opposing end faces supporting opposing ends of the plurality of second tubes, the plurality of first tubes having central portions thereof extending parallel with central portions of the plurality of second tubes.

17. The method of claim 16 wherein the plurality of first tubes of said arranging step includes said central portions thereof extending in a direction parallel to a plane of said lateral faces, the plurality of first tubes including inlet portions thereof and outlet portions thereof between said central portions and said lateral faces which are oriented perpendicular to a plane of said lateral faces.

18. The method of claim 16 wherein the plurality of first tubes of said arranging step have at least portions thereof each including a matching series of regularly spaced bends between ends of each of the plurality of first tubes; and wherein the plurality of second tubes of said arranging step have at least portions thereof each including a matching series of regularly spaced bends between ends of each of the plurality of second tubes, the plurality of first tubes and the plurality of second tubes having a similar form to maintain a parallel relationship along at least portions thereof which include said series of regularly spaced bends therein.

19. The method of claim 18 wherein said regularly spaced bends are spaced from each other by linear sections such that the plurality of first tubes and the plurality of second tubes have a zig-zag form over portions thereof.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0044] FIG. 1 is a perspective view of a single tube within one embodiment of the heat exchanger of this invention, with the tube featuring bends therein to promote turbulent flow and greater heat transfer. The shape of the tube can be varied. For instance, the cross-section can be non-circular, and the bend radii, pitch and amplitude can be varied to optimize heat transfer, while minimizing pressure drop or for other purposes.

[0045] FIG. 2 is a perspective view of two layers of tubes within an array of tubes of the heat exchanger, according to one embodiment of this invention. A first layer of tubes is part of a circuit A and the second layer of tubes on top of the first layer of tubes is part of a circuit B. In the embodiment shown, tubes within circuit B feature bends therein while tubes within circuit A are straight, except they bend near ends thereof to exit the array of tubes on sides of the array of tubes lateral to where the tubes of circuit B enter and exit the array.

[0046] FIG. 3 is a top plan view of a single layer of tubes within circuit A, and with metal matrix powder shown between the tubes.

[0047] FIG. 4 is a top plan view of two layers of tubes with a lower layer of tubes within circuit A and with an upper layer of tubes within circuit B, and with metal powder shown between the tubes of each layer and between the layers.

[0048] FIG. 5 is a perspective view of an array of tubes including a set of tubes of circuit A within multiple layers and interposed with multiple layers of tubes within circuit B, similar to that which is shown in FIG. 2, but with multiple repeating patterns of layers of tubes of circuit A and tubes of circuit B, to complete the entire array of tubes, and before addition of metal powder and completion of the metal matrix in which the array of tubes is embedded.

[0049] FIG. 6 is a perspective view of that which is shown in FIG. 5 after addition of powder between the various tubes within the array of tubes, and after heating and/or applying pressure to the powder filling gaps space within the array of tubes to solidify the matrix of metal powder in which the array of tubes is embedded, and completing the heat exchanger of this invention, except for addition of manifolds to supply and remove fluids passing along circuit A and circuit B through the heat exchanger.

[0050] FIG. 7 is a perspective view of the heat exchanger of this invention, according to one embodiment, and similar to that which is shown in FIG. 6, but with the addition of manifolds for delivery and removal of fluids along circuit A and along circuit B, through the heat exchanger.

[0051] FIG. 8 is a sectional view take a long line 8-8 of FIG. 7 and illustrating how layers of tubes within multiple separate circuits can be close packed together to minimize gap space therebetween.

[0052] FIG. 9 is a sectional view similar to that which is shown in FIG. 8, but in an alternative embodiment where separate layers of tubes are oriented body centered relative to adjacent layers, and enlarging gap space between the tubes within the array of tubes in this alternative environment.

[0053] FIG. 10 is a sectional view similar to that which is shown in FIGS. 8 and 9, but illustrating how a prior art typical PCHE has non-circular channels provided within separate layers following and additive 3-D printing type process, according to the prior art.

[0054] FIG. 11 is a flow chart illustrating steps in one method of manufacturing the heat exchanger of FIGS. 6 and 7, according to one embodiment of this invention.

[0055] FIG. 12 is a flow chart illustrating details of a first step in the manufacturing method to FIG. 11.

[0056] FIG. 13 is a flowchart illustrating an alternative embodiment of that which is depicted in FIG. 12.

DESCRIPTION OF THE PREFERRED EMBODIMENT

[0057] Referring to the drawings, wherein like reference numerals represent like parts throughout the various drawing figures, reference numeral 10 (FIGS. 6 and 7) is directed to a heat exchanger according to one embodiment of this invention which is made up of multiple layers 25, 45 of first tubes 30 and second tubes 50 which together make up a circuit A 20 and a circuit B 40 passing through the heat exchanger 10. The array 100 of tubes 30, 50, have gap space therebetween filled with a matrix 60 of metal powder which is solidified, such as by action of a hot isostatic press to solidify the metal matrix 60 with the array 100 of tubes 30, 50 embedded therein. Such a configuration allows for different materials to be used for circuit A and/or circuit B and for the metal matrix 60, and so that the heat exchanger can provide optimal corrosion resistance, heat transfer properties, thermal properties, pressure containment properties and customization.

[0058] In essence, and with particular reference to FIGS. 5-7, basic details of the heat exchanger 10 are described, according to one embodiment of this invention. The array 100 of tubes includes first tubes 30 provided in multiple separate layers 25, which together comprise circuit A 20. The array 100 also includes second tubes 50 provided in multiple separate layers 45 which together comprise circuit B 40. Gap space between the tubes 30, 50 of the array 100 are filled with a metal matrix 60. The first tubes 30, second tubes 50 and metal matrix 60 are made up of at least two different materials, and optionally three different materials.

[0059] To form the heat exchanger 10, in one embodiment, first tubes are arranged in a first layer 25, followed by second tubes 50 within a layer 45. Another layer 25 of first tubes 30 is then provided, followed by another layer 45 of second tubes 50. This process is repeated until a full array 100 of tubes 30, 50 have been provided. Space between the tubes 30, 50 is filled with metal powder 62 to fully embed the tubes 30, 50, except for at ends thereof. The assembly is then placed within a hot isostatic press (or other heat and/or temperature applying equipment) and the powder 62 is sintered or otherwise solidified into a solid matrix 60 within which the array 100 of tubes 30, 50 are embedded. Finally, manifolds 70, 72, 74, 76 are placed over ends of the tubes 30, 50 from similar circuits 20, 40 for supply and removal of fluids passing through the heat exchanger 10.

[0060] The novel HX of the present invention is described as a micro-tube metal matrix heat exchanger, a completed version of which is shown in FIG. 7. This particular representation is of a counter or co-flow arrangement. Cross-flow and multiple circuits (i.e. greater than two) are also possible.

[0061] Although similar in outer appearance to other compact heat exchangers such as PCHEs/CPHXs, there are significant differences in the design and layout of the heat exchanger 10 internal passages as illustrated by FIGS. 8-10. And while other heat exchangers have used micro-tubing to create small passages, the heat exchanger 10 of this invention incorporates a metal matrix 60 for additional structural strength. The heat exchanger core is constructed from an assembly of micro-tubes 30, 50, surrounded by a metal matrix 60. The tubes 30, 50, which are commercially available in sizes and materials of interest, are formed to the desired shape, e.g. a wavy pattern to promote turbulence is shown in FIGS. 1-4 and laid or woven in layers 25, 45. While round tubes are shown, different cross-sections are also possible. FIGS. 8 and 9 show two potential layouts, a planar packaging (FIG. 9) and a close packed hexagonal packing (FIG. 8). The latter packaging provides the closest possible packing for tubes 30, 50 of an identical outside diameter, and thus are the most efficient from a compactness and heat transfer standpoint. The matrix is formed by filling the interstices between tubes 30, 50 with fine metal powder 60 and then sintering and compacting the assembly in a hot isostatic pressing (HIP) process.

[0062] The layouts of FIGS. 8-10 have been scaled so as to provide the same hydraulic diameter for the three configurations and thus essentially the same pressure drop, all else being equal. It can be seen that a higher density of flow channels and a closer distance of approach between circuits is possible with the heat exchanger 10 when compared to the PCHE/CPHX D. Coupled with the round cross-section of the heat exchanger 10 of this invention, this packing provides for optimal heat transfer. For the same flow area there is an increase of around 16% in the hydraulic diameter. The circular cross-section also provides a more optimal structural configuration. It can also be seen, from a particulate plugging standpoint, the heat exchanger 10 tube 30, 50 configurations provide a larger passageway than the semi-circular cross-section E of the PCHE D, for the similar pressure drop, thus providing a more robust functional design. The semi-circular cross-section E of the PCHE D produces a non-optimal configuration from a structural standpoint and has the interlayer parting line at the corner, producing a stress riser. The circular heat exchanger 10 configuration shown in FIGS. 8 and 9 is generally preferred, especially from a structural standpoint.

[0063] In the heat exchanger 10, primary structural integrity is provided by the tube 30, 50 walls 32, 52, with secondary structure provided by the metal matrix 60, intrinsically producing a more robust design than that available from the planer diffusion bonded PCHE/CPHX D, due to redundancy. The HIP processing of the heat exchanger 10 bonds the tubes 30, 50 and matrix 60 together, to produce a monolithic structure.

[0064] As mentioned, the tubes from which the heat exchanger 10 are produced are commercially available as either fractional or hypodermic tubing 30, 50. While both welded and seamless extruded tubing are available, seamless is the preferred embodiment from a structural standpoint, but with the supporting matrix 60, welded tubing 30, 50 will be acceptable for certain applications. Stainless steel, nickel based alloys and even refractory alloys are available in the sizes and wall 32, 52 thicknesses of interest and custom materials are readily produced. Tube 30, 50 configurations can also be varied to enhance heat transfer. Along with the wavy tubes 12 previously described, tubes 30, 50 can have internal protuberances and/or be twisted or otherwise configured to enhance heat transfer while minimizing pressure drop. Internal protuberances can be formed by simply dimpling the tube 30, 50 from the outside.

[0065] With the heat exchanger 10 construction, it is possible to mix materials to provide the optimal selection for corrosion and thermal compatibility and cost effectiveness with the respective circuit 20, 40 fluids at desired service temperatures. For example, for a fluoride molten salt HX that is coupled with H.sub.2O (Rankine cycle) or sCO.sub.2 (Brayton cycle) at temperatures in excess of 700° C., a high nickel alloy tube 30, 50 can be used on the salt circuit while lower cost stainless steel tubes 50, 30 can be applied to the opposite circuit, all contained within a low-cost stainless steel matrix 60. A significant advantage when compared to a typical PCHE/CPHX D that would require fabrication entirely from the high cost material. For another example, a type of molten salt reactor that utilizes two types of salts, e.g. fuel salts and chloride/fluoride salts, as a means of transferring heat from the reactor to secondary heat exchanger would inherently require two different types of corrosion resistant materials to combat the differing corrosion issues associated with the two types of salts.

[0066] An additional benefit of the heat exchanger 10 technology of this invention lies in the tolerance available from the use of tubing 30, 50 to form the passageways. The inside diameter of the micro-tubing used, in the sizes of interest, are expected to vary ˜+/−0.002″ or less. For an equivalent sized passage in a PCHE D or CPHX, the variation would be approximately double this amount. This tolerance control leads to a lower variation in pressure drop and improved performance.

[0067] The process for producing the matrix 60 is well-known, typically referred to as Powder Metallurgy—Hot Isostatic Pressing or PM-HIP. This process is used to make powder metallurgy billets and near-net components. Considerable interest and effort has been expended by the nuclear industry to investigate and allow PM-HIP components for pressure containing devices such as valve bodies and pump housings. The aerospace industry has also investigated and utilizes the process. As mentioned, the matrix 60 can be selected from any number of low cost alloys compatible with the process and application but it can also be a material such as copper or other high conductivity material to enhance heat transfer.

[0068] While a fully densified matrix 60 has been discussed so far, a compliant matrix 60 is also possible. One method to produce this would be low temperature sintering. This process would leave voids in the matrix 60 that would reduce its stiffness and aid compliance if required for the desired application.

[0069] Heat exchanger 10 core (FIGS. 2, 5 and 6) fabrication can be viewed as primarily additive manufacturing processing, making highly efficient use of resources and the materials of construction. The tubes 30, 50 are fabricated in an extrusion or roll and welding process; the matrix powder 60 is produced in a combination of mechanical, thermal and chemical processes; and the joining or assembly takes place in the HIP process. Essentially 100% of the input material is used in making the heat exchanger 10. Machining of the matrix 60 for attachment of manifolds 70, 72, 74, 76 is the only subtractive process. By contrast, in a PCHE/CPHX D, a significant amount of the original sheet material is machined away prior to assembly—material waste that cannot be recouped. This can be as much as 40% of material removal.

[0070] In summary, the multiple attributes of the heat exchanger 10 make it ideal for cost-effective, high temperature and corrosion resistant heat exchangers for next generation applications and existing applications requiring high performance at low cost. The approach makes efficient use of dedicated materials to address corrosion and cost issues while utilizing available technologies and manufacturing processes.

[0071] More specifically, and with particular reference to FIGS. 1 and 2, basic details of individual tubes 12 within the heat exchanger 10 (FIGS. 6 and 7) are described, according to an exemplary embodiment. The individual tubes 12 extend between ends 14 and have a hollow interior through which a fluid can be conducted. In one embodiment, bends 16 are provided at regular intervals between the ends 14. Such bends 16 can increase turbulence and promote heat transfer, such as by disturbing any boundary layer of the fluid adjacent to an interior wall of the individual tubes 12. In some embodiments, such as with the lower layer 25 within FIG. 2, individual tubes can be straight, rather than having bends 16 therein. These first tubes 30 within layer 25 depicted in FIG. 12 are straight, except near ends 22, 24 thereof where they bend one time to allow an inlet end 22 and outlet end 24 of circuit A 20 to extend out of lateral sides of the heat exchanger 10, rather than out of ends of the heat exchanger 10 where circuit B 40 tubes 50 exit heat exchanger 10. In this way, separate manifolds 70, 72, 74, 76 (FIG. 7) can easily be attached to the heat exchanger 10 to feed fluids to the circuits 20, 40 (along arrows A and B) and remove fluids from the circuits 20, 40.

[0072] Each of the first tubes 30 within the layer 25 extend from an inlet end 22 to an outlet end 24. Similarly, each of the second tubes 50 within the layer 45 including an entry 42 opposite an exit 44. The layers 25, 45 provide portions of separate circuits 20, 40 passing through the heat exchanger 10. These ends 22, 24 and entry/exit 42, 44 are grouped together at locations on the heat exchanger 10 separate from other groupings, so that manifolds 70, 72, 74, 76 can most conveniently be attached to the heat exchanger 10.

[0073] While in this one embodiment (FIG. 2) one layer 25 is shown with straight tubes 30 and the other layer 45 is shown with tubes 50 featuring bends 16, the tubes 30, 50 could all be straight, or could all have bends 16 therein, or could otherwise be configured within the layers 25, 45. As another alternative, layers 25, 45 could each be formed of a mixture of tubes 30, 50, associated with different circuits 20, 40.

[0074] With particular reference to FIGS. 3 and 4, further details of these layers 25, 45 of tubes 30, 50 are depicted. Powder 62 which is later solidified into the metal matrix 60 are shown within FIGS. 3 and 4. In one embodiment, this powder 62 is laid down along with placement of layers 25 of first tubes 30 and layers 45 of second tubes 50 within the two circuits 20, 40, to most effectively ensure that metal power 62 is uniformly placed, filling all voids between the tubes 30, 50. FIGS. 3 and 4 illustrate further how in one embodiment all of the tubes 30 of the layer 25 and second tubes 50 of the layer 45 can feature bends 16 therein in one embodiment. Such an arrangement can facilitate close packing (FIG. 8) between the layers, while configurations where some layers 25 have straight tubes 30 and other layers 45 have tubes 50 with bends 16 therein best facilitate body centered arrangements between layers such as that depicted in FIG. 9.

[0075] Which particular reference to FIGS. 8 and 9, further details of the tubes 30, 50 are described, according to various different embodiments. In FIG. 8 tubes 30 of the layer 25 and the tubes 50 of the layer 45 are close packed together to minimize gap space and to maximize contact between adjacent tubes within the array 100 (FIG. 5) of tubes 30, 50 making up the heat exchanger 10. In contrast, in FIG. 9 a body centered arrangement is provided between tubes 30, 50 of the various layers 25, 45, increasing gap space and facilitating a wide variety of arrangements of tubes 30, 50 within layers 25, 45.

[0076] Each of the first tubes 30 is made up of walls 32 having a wall thickness defined by a distance between an inner surface 34 and an outer surface 36. Inner surfaces 34 define that portion of the first tube 30 which are in direct contact with fluids passing through the tubes 30 of circuit A 40. The outer surface 36 comes into contact with second tubes 50 as well as with other first tubes 30 in typical embodiments, and into contact with the metal matrix 60 which fills gaps between the tubes 30, 50.

[0077] Thickness of these walls 32 can be made thinner than might otherwise be the case to handle pressures of fluids passing therethrough, because the walls 32 are supported on an exterior side thereof by the matrix 60, as well as by adjacent tubes 30, 50. Furthermore, thinner walls can save on exotic material costs which might be utilized to handle challenging fluid characteristics including corrosiveness, and extremes of temperature and pressure, when the heat exchanger 10 is operating as intended, or when experiencing off design states of operation.

[0078] While each of the first tubes 30 are shown with a circular cross-section, these first tubes 30 could alternatively have some other cross-section, such as a square cross-section or other cross-sectional form. In one embodiment, protuberances 35 extend inwardly from the inner surface 34 of the walls 32. Such protuberances can promote turbulence and improve heat transfer effectiveness. In one embodiment, such protuberances 35 are formed by forming dimples 37 on the outer surface 36, and with the walls 32 being sufficiently thin that the dimples 37 extend through the walls 32 to leave the protuberances 35 on the inner surface 34.

[0079] Similar to the first tubes 30, the second tubes 50 also include walls 52 bounded by an inner surface 54 opposite an outer surface 56, and with optional protuberances 55 and/or dimples 57 thereon. Other characteristics of the second tubes 50 can vary in a manner similar to that described above with respect the first tubes 30. Typically, the second tubes 50 are formed from a different material than that from which the first tubes 30 are formed. In one embodiment, one of the fluids passing through the heat exchanger 10 is non-corrosive, or less corrosive, or corrosive in a different way than the tubes 30 of the alternate circuit within heat exchanger 10. The tubes 50 can thus be optimized for the fluid they are containing, and to minimize cost. In one embodiment, the second tubes 50 can be formed of a similar material from which the matrix 60 is formed. As another alternative, the first tubes 30 and second tubes 50 can be formed of a common material which is different from that of the metal matrix 60.

[0080] While the tubes 30, 50 have been described as being within two circuits 20, 40, it is conceivable that more than two circuits 20, 40 might be provided in an alternative heat exchanger. For instance, a heat exchanger might be configured which exchanges heat between three different fluids passing through three different circuits, while each of the different circuits could be made of tubes formed of similar or different materials to the materials forming the other tubes of the other circuits and providing the matrix 60.

[0081] With particular reference to FIG. 10, a prior art PCHE D cross-section is shown to contrast with the cross-sections of the arrays 100 of tubes 30, 50 according to embodiments of this invention. To facilitate 3-D printing thereof, the channels E are typically non-circular in form and less optimally configured. Also, opportunities to utilize lower cost and/or less corrosive materials at strategic locations are not facilitated, or made significantly more complex (such as with coatings, etc.).

[0082] With particular reference to FIGS. 5-7, details of the metal matrix 60 and manifold 70 are described, according to an exemplary embodiment. In a preferred environment, the matrix 60 begins as powder 62 placed between tubes 30, 50 within the array 100. Typically this powder 62 is a metal powder selected for appropriate heating and temperature performance, as well as suitable heat transfer performance and cost minimization, as well as structural strength, especially when high-pressure containment is to be provided by the matrix 60 (at least as a backup). Typically this powder 62 is applied while the array 100 of tubes is already within a press having a mold cavity shaped similar to a desired final shape for a heat exchanger 10. Force, such as provided by a press platen from above (along arrow C of FIG. 6) can be applied to this matrix 60, along with heat, in a hot isostatic press to sinter and/or otherwise solidify (such as by fully melting) the powder 62 into a solid matrix 60.

[0083] The heat exchanger 10 can then be removed from the press. Finally, ends of the first tubes 30 and second tubes 50 within the two circuits 20, 40 can be ground if necessary or otherwise cut to final size (if needed), and manifolds can be added. In particular, the first inlet manifold 70 can overlay inlet end 22 of circuit A 20. A first outlet manifold 72 can be placed over the outlet end 24 of tubes 30 of circuit A 20. A second inlet manifold 74 can be placed over entry end 42 of second tubes 50 within circuit B 40. A second outlet manifold 76 can be placed over exit 44 ends of the second tubes 50 within circuit B 40. The manifolds 70, 72, 74, 76 facilitate flow along the various circuits 20, 40 including circuit A flow along arrow A and circuit B flow along arrow B. While these arrows generally illustrate counterflow, other forms of flow could be provided by rearranging the tubes 30, 40 within the heat exchanger 10 or adjacent plumbing.

[0084] FIGS. 11-13 illustrate steps in the manufacturing process described above. An overview of the process of manufacture 80 includes first forming the tube array including circuit A tubes 30 and circuit B tubes 50, as step 82. This is followed by embedding the array in powder matrix 60, according to step 84. The matrix is been solidified according to step 86. Finally, manifolds are added according to step 88. This first step 82 in the manufacturing method 80 can be broken down in one embodiment shown in FIG. 12. An alternative tube array placement process 182 is depicted in FIG. 13. A variety of other alternative placement steps could be provided according to alternative embodiments. As an alternative to adding the powder matrix after fully forming up the tube 30, 50 array 100, the powder could be applied as the layers 25, 45 are built up. While matrix solidification is described primarily as utilizing a hot isostatic press, it is conceivable that temperature alone could be utilized to sinter or otherwise heat into a solid form the matrix 60. The matrix 60 could be solidified by other means, such as utilizing some form of binding agent as a further alternative.

[0085] As an option when manufacturing the heat exchanger 10, the tubes 30, 50 (at least some of them) can be at least partially filled with support media. In one embodiment, the media is in the form of small pellets sized small enough that they can substantially fill interiors of the tubes 30, 50. Filling of the tubes 30, 50 with media allows for the HIP process to occur without deforming the tubes, 30, 50, especially by collapsing the tubes 30, 50 due to the pressure associated with the HIP process. Other related processes which involve pressure and/or heat could similarly minimize tube 30, 50 deformation by placing the media into the tubes, 30, 50. The media is typically in the form of beads of microscopic or near microscopic size. At a minimum, the media is a form of beads that are at least an order of magnitude smaller than a diameter of the tubes 30, 50.

[0086] The media is preferably formed of a material which can withstand high temperatures and high pressures without significant deformation. As one example, alumina ceramic beads of about 10 micron average size can be used as the media. A shape of the media in one embodiment is spherical.

[0087] With reference to FIG. 11, the media can be added into the tubes 30, 50 in a step 83 which could be provided before the tubes 30, 50 are placed where desired, or after the tubes 30, 50 are placed where desired, and before the matrix material is put in place into interstices outside of the tubes 30, 50, or after the matrix material has been put in place outside of the tubes 30, 50.

[0088] While it is generally desirable that the media does not collapse at all under pressures applied by the HIP or other process, some deformation of the media could occur, provided the media can still be removed after the matrix material has been sintered from a powder into a more solid form. While it is also generally desirable that the media does not melt under the temperatures associated with the HIP or other process to solidify the matrix, the media could, in at least one embodiment, melt into a liquid provided that the ends of the tubes 30, 50 are plugged to avoid such liquid escaping in an appreciable amount, or the process would need to be sufficiently rapid that the application of pressure would cease before an appreciable amount of such liquid escapes from the tubes 30, 50.

[0089] When such support media is utilized inside of the tubes 30, 50, a final step involves removing the media, typically before manifolds are added to the ends of the tubes 30, 50. Options for such a removal step can include application of suction, application of pressurized air, utilization of at least one elongate fiber placed in the end of the tube 30, 50 to push out the media, utilizing gravity, vibration and/or other appropriate media removal techniques (alone or in combination).

[0090] In an alternative embodiment, the media can be selected from a material which does deform slightly under pressure, or the media could less than entirely fill at least some of the tubes 30, 50 and the pressure associated with the HIP or other process would cause small amounts of tube 30, 50 deformation. Such small amounts of deformation could have the beneficial effect of roughening interior surfaces of the tubes 30, 50 to enhance heat transfer therealong, and could also facilitate some degree of compaction of the tubes 30, 50 together, which, in turn, could cause the heat exchanger 10 to have a more compact volume after completion of manufacture.

[0091] Utilizing the media also can beneficially allow for wall thicknesses of the tubes 30, 50 to be reduced to thicknesses less than would otherwise be able to withstand the pressure associated with the HIP or other matrix solidification process, so the thicknesses of the tubes 30, 50 can be optimized beyond what would otherwise be possible. Thus, in one embodiment, wall thicknesses for the tubes 30 and/or tubes 50 are less than a thickness which could withstand the pressure associated with the HIP process, without the presence of the media within the tubes 30, 50. One example pressure for one HIP process is about 15,000 psi (or greater).

[0092] This disclosure is provided to reveal a preferred embodiment of the invention and a best mode for practicing the invention. Having thus described the invention in this way, it should be apparent that various different modifications can be made to the preferred embodiment without departing from the scope and spirit of this invention disclosure. When embodiments are referred to as “exemplary” or “preferred” this term is meant to indicate one example of the invention, and does not exclude other possible embodiments. When structures are identified as a means to perform a function, the identification is intended to include all structures which can perform the function specified. When structures of this invention are identified as being coupled together, such language should be interpreted broadly to include the structures being coupled directly together or coupled together through intervening structures. Such coupling could be permanent or temporary and either in a rigid fashion or in a fashion which allows pivoting, sliding or other relative motion while still providing some form of attachment, unless specifically restricted.