EXTREME ENVIRONMENT HEAT EXCHANGER

Abstract

The heat exchanger (10) includes a ceramic matrix composite (12) (stable at temperatures up to 1,650 C.) surrounding and defining a hot fluid conduit (14). A hardenable material (18) having a high thermal conductivity is formed into a heat transfer layer (16) surrounding the ceramic matrix composite (12). A metal pipe (20) is coextensive with the heat transfer layer (16) and defines at least a portion (22) of at least one cool fluid passage (24, 34, 54) defined adjacent to and in heat exchange relationship with the heat transfer layer (16) so that a fluid passing through the cool fluid passage (24, 34, 54) absorbs heat passing through the heat transfer layer (16) from the hot fluid passing through the hot fluid conduit (14).

Claims

1-17. (canceled)

18. A method of manufacturing an extreme environment heat exchanger, the method comprising: a. forming a ceramic matrix composite into an elongate form that defines a hot fluid conduit within the ceramic matrix composite, the ceramic matrix composite being configured to have mechanical stability at temperatures up to about 1,650 degrees Celsius; b. then, bonding a hardenable material having a thermal conductivity of at least 20 Btu/(hr. ft.sup.2 F.) to the ceramic matrix composite so that the hardenable material surrounds and is coextensive with the hot fluid conduit; c. then, machining the hardenable material to produce a heat transfer layer surrounding the ceramic matrix composite that, with the ceramic matrix composite, defines about a uniform thickness between an exterior surface of the heat transfer layer and the hot fluid conduit; d. securing the heat transfer layer and attached ceramic matrix composite within a circumferentially displaced metal pipe such that the metal pipe defines at least a portion of at least one cool fluid passage adjacent to an in heat exchange relationship with the heat transfer layer, wherein the circumferentially displaced metal pipe is circumferentially displaced from the heat transfer layer so that the cool fluid passage is a surrounding cool fluid passage defined between an interior space of the circumferentially displaced metal pipe and the exterior surface of the heat transfer layer; e. securing a coil seal between the exterior surface of the heat transfer layer and an interior surface of the circumferentially displaced metal pipe, wherein the coil seal overlaps itself thereby enabling differential thermal growth of the coil seal between the heat transfer layer and the metal pipe.

19. The method of claim 18, further comprising, after machining the hardenable material to about a uniform thickness, machining into an exterior surface of the heat transfer layer a plurality of channels having longitudinal axes parallel to a direction of flow of the hot fluid through the hot fluid conduit, then securing the heat transfer layer and attached ceramic matrix composite within a metal pipe so that the metal pipe covers the plurality of channels in the exterior surface of the heat transfer layer to form a plurality of cool fluid passages.

20. The method of claim 18, further comprising, after machining the hardenable material to about a uniform thickness, machining into an exterior surface of the heat transfer layer a plurality of channels having longitudinal axes parallel to a direction of flow of the hot fluid through the hot fluid conduit.

21. The method of claim 18, further comprising expanding the coil seal longitudinally axially and rotationally about itself to absorb heat and minimalize thermal expansion stress on the circumferentially displaced metal pipe.

22. The method of claim 18, wherein the hardenable material is selected from the group consisting of metals including silicon, silver, copper, aluminum, nickel, and nickel alloys, and ceramics including boron nitride, tungsten carbide, and silicon carbide, and wherein the hardenable material is reinforced with at least one of chopped fibers, hard ceramic particles, soft ceramic particles, carbides, graphite, carbon, glass, silicone carbide, silicon nitride or boron nitride, and combinations thereof.

23. The method of claim 18, wherein an exterior surface of the heat transfer layer defines a second portion of the at least one cool fluid passage so that the cool fluid passage is defined between the heat transfer layer and the surrounding metal pipe, and wherein the cool fluid passage is coextensive with the hot fluid conduit.

24. The method of claim 23, wherein the machining step comprise a plurality of second portions of cool fluid passages defined within the exterior surface of the heat transfer layer so that a plurality of cool fluid passages are defined between the heat transfer layer and the surrounding metal pipe, and wherein the plurality of cool fluid passages are coextensive with the hot fluid conduit.

25. The method of claim 18, wherein exterior surface of the heat transfer layer is machined to surface finish tolerances of about 0.005 (0.127 mm).

26. The method of claim 18, wherein the heat transfer layer has a thickness that is between about one-half and about ten times a wall thickness of the ceramic matrix composite tube surrounded by the heat transfer layer.

27. The method of claim 18, wherein the heat transfer layer has a thickness that is between about 1.27 millimeters and about 6.35 millimeters.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0017] FIG. 1 is a simplified schematic front plan drawing showing an extreme environment heat exchanger constructed in accordance with the present invention.

[0018] FIG. 2 is a simplified schematic front plan drawing showing a ceramic matrix composite formed into an elongate form defining a hot fluid conduit within the ceramic matrix composite.

[0019] FIG. 3 is a front plan view of the FIG. 2 formed ceramic matrix composite with a hardenable material bonded to surround the ceramic matrix composite.

[0020] FIG. 4 is a front plan view of the FIG. 3 formed ceramic matrix composite with the hardenable material machined to a uniform thickness about the ceramic matrix composite to form a heat transfer layer.

[0021] FIG. 5 is a front plan view of the FIG. 4 formed ceramic matrix composite with the heat transfer layer and showing a plurality of portions of cool fluid passages machined into an exterior stir face of the heat transfer layer.

[0022] FIG. 6 is a simplified, schematic front plan view of an extreme environment heat exchanger showing a metal pipe circumferentially displaced from the outer surface of the heat transfer layer and showing an overlapping coil seal secured between the metal pipe and the heat transfer layer.

[0023] FIG. 7 is a simplified, schematic front plan view of an alternative embodiment of the extreme environment heat exchanger showing a plurality of metal pipes secured within a corresponding plurality of channels machined in an outer surface of a heat transfer layer.

[0024] FIG. 8 is a simplified, schematic front plan view of another embodiment of the extreme environment heat exchanger showing a plurality heat discharge extensions defined by the heat transfer layer and extending away from the heat transfer layer and a way from the hot fluid conduit.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0025] Referring to the drawings in detail, an extreme environment heat exchanger for transferring heat from a hot fluid conduit to a cool fluid passage is shown in FIG. 1 and is generally designated by the reference numeral 10. The heat exchanger 10 includes a ceramic matrix composite 12 surrounding and defining a hot fluid conduit 14 and configured so that a hot fluid (not shown) passing along the conduit 14 cannot pass out of the conduit 14 through the ceramic matrix composite 12. The ceramic matrix composite 12 may also be manufactured to have mechanical stability at temperatures up to about 3,000 degrees Fahrenheit (1,650 degrees Celsius). (As described above, for purposes herein, the word about is to mean plus or minus 10%.)

[0026] A heat transfer layer 16 surrounds the ceramic matrix composite 12, and the heat transfer layer is made of a hardenable material 18 selected from the group consisting of metals including silicon, silver, copper, aluminum, nickel, nickel alloys, and ceramics including boron nitride, tungsten carbide, silicon carbide, the aforesaid hardenable materials reinforced with at least one of chopped fibers, hard ceramic particles, soft ceramic particles, carbides, graphite, carbon, glass, silicon carbide, silicon nitride or boron nitride, and combinations thereof. The hardenable material may also have a thermal conductivity of at least 20 Btu/(hr. ft.sup.2 F.). The hardenable material 18 may be applied to the ceramic matrix composite 12 by a variety of methods. An exemplary method is disclosed in U.S. Published Patent Application Bo. U.S. 2011/0219775 that was published on Sept. 15, 2011, and is owned by the owner of all rights in the present disclosure. The exemplary method is air plasma spray (APS) of the hardenable material 18 onto the ceramic matrix composite 12. The APS applied hardenable material 18 is then machined, such as by diamond grinding, so that the hardenable material 18 forms the heat transfer layer 16 surrounding the ceramic matrix composite 12. An exterior surface 28 of the heat transfer layer 16 may be machined to surface finish tolerances of about 0.005 (0.127 mm). The ceramic matrix composite 12 defining the hot fluid conduit 14 may have a uniform thickness.

[0027] As shown best in FIG. 1, a metal pipe 20 is coextensive with the heat transfer layer 16. (For purposes herein, the phrase coextensive with is to mean that the components that are coextensive with each other have a common point of beginning and ending and have longitudinal axes between the point of beginning and ending that are generally parallel to each other. In other words a metal pipe and a ceramic conduit are coextensive with each other if one surrounds the other as in FIG. 1, and if one is positioned alongside the other as in FIG. 7.) As shown in FIG. 1, the metal pipe 20 also defines portions 22 of cool fluid passages 24 defined adjacent to and in heat exchange relationship with the heat transfer layer 16 so that a fluid (not shown) passing through the cool fluid passages 24 absorbs heat passing through the heat transfer layer 18 from the hot fluid passing through the hot fluid conduit 14.

[0028] FIGS. 1 and 5 show that a second portion 26 of the cool fluid passages 24 may be defined within an surface 28 of the heat transfer layer 16 so that the cool fluid passages 24 are defined between the heat transfer layer 16 and the surrounding metal pipe 20. The one or more cool fluid passages 24 are also coextensive with the hot fluid conduit 14. The one or more cool fluid passages 24 are therefore defined between the heat transfer layer 16 and the surrounding metal pipe 20.

[0029] FIG. 6 shows a displaced metal pipe embodiment 30 of the extreme environment heat exchanger 10. In this embodiment 30, a surrounding, coextensive metal pipe 32 is circumferentially displaced from the heat transfer layer 16 so that a surrounding cool fluid passage 34 is defined between an interior surface 36 of the displaced metal pipe 32 and the exterior surface 28 of the heat transfer layer 16. (For purposes of FIG. 6 and the description of the displaced metal pipe embodiment 30, components that are virtually identical to the components described above of the FIGS. 1-5 embodiment are shown in FIG. 6 as primes of the reference numerals used in FIGS. 1-5.)

[0030] The displaced metal pipe embodiment 30 may also include a plurality of portions 26 of cool fluid passages 24 defined within the exterior surface 28 of the heat transfer layer 16. This increases the exterior surface area 28 of the heat transfer layer 16 exposed to a cooling fluid passing through the surrounding cool fluid passage 34 and/or the cool fluid passages 24 that are defined between the metal pipe 32 and exterior surface 28 of the heat transfer layer 16.

[0031] The displaced metal pipe embodiment 30 may also include a metal coil seal 40 secured between the exterior surface 28 of the heat transfer layer 16 and the interior surface 36 of the metal pipe 32. The coil seal 40 may not be bonded or otherwise permanently secured to the exterior surface 28 of the heat transfer layer 16. The coil seal 40 (as shown in FIG. 6) overlaps itself and therefore enables differential thermal growth or physical expansion of the coil seal 40 between the heat transfer layer 16 and the metal pipe 32 in directions parallel to perpendicular to and rotationally about an axis of fluid flow within the hot fluid conduit 14. This minimizes thermal expansion of the surrounding metal pipe 32 by effectively concentrating heat within the coil 40 and by also reducing a rate of heat transfer into the metal pips 32. The metal coil seal 40 may be fabricated of high-temperature metals, stich as a nickel alloy.

[0032] The coil seal 40 may also provide, portions 22 of a plurality of cool fluid passages 24 having other portions 26 of the cool fluid passages 24 defined within the exterior surface 28 of the beat transfer layer 16. In this embodiment, most of the heat transferred from the hot fluid moves into the cool fluid flowing through the cool fluid passages 24 while the coil seal 40 expands longitudinally, axially and rotationally about itself. This serves to protect the surrounding, circumferentially displaced metal pipe 32 from damaging thermal expansion. The metal coil seal 40 may also be configured to be coextensive with the heat transfer layer 16.

[0033] FIG. 7 shows a multi-tube embodiment 50 of the extreme environment heat exchanger 10. This embodiment 50 includes a plurality of metal pipes 52, wherein each metal pipe 52 defines a complete cool fluid passage 54. Each metal pipe 52 is also secured adjacent to and coextensive with the heat transfer layer 16. A further aspect of this embodiment includes the exterior surface 28 of the heat transfer layer 16 defining a plurality of channels 56 configured so that each, of the plurality of metal pipes 54 is secured within each of the plurality of channels 56 to increase a rate of heat movement between the heat transfer layer 16 and the cool fluid passages 54 defined by the metal pipes 52. Additionally, the metal pipes 52 may foe bonded within the channels 56 to further increase a rate of heat movement or transfer, so that the metal pipes 52, heat transfer layer 16 and the hot fluid conduit 14 defined by the ceramic matrix composite 12 form an integral, multi-tube extreme environment heat exchanger 50.

[0034] FIG. 8 shows a heat-discharge extension embodiment 60 of the extreme environment heat exchanger 10. This embodiment 60 includes a hot fluid conduit 14 defined by a ceramic matrix composite 12 and surrounded toy a coextensive, heat transfer layer 16 of hardenable material 18. The heat transfer layer 16 also defines a plurality of heat discharge extensions 62 extending from the exterior surface 28 of the heat transfer layer 16 and away from the hot fluid conduit 14 . A plurality of cool fluid passages 64 are defined between the heat discharge extensions 62. The heat discharge extensions 62 may take the form of fins and pins defined by the hardenable material 18 with the above described high thermal conductivity, such as metals including silicon, silver, copper, aluminum, nickel, nickel alloys. A length of extension of the heat discharge extensions away from and perpendicular to the hot fluid conduit 14 may be between about one-half and about ten times a wall thickness of the ceramic matrix composite tube 12. (For purposes herein, the phrase wall thickness of the

[0035] ceramic matrix composite tube 12 is to mean a shortest distance between and interior and an exterior wall of the tube 12.) The wall thickness of the ceramic matrix composite tube 12, in an exemplary embodiment may range from between about 0.05 inches to 0.25 inches (1.27 mm to 6.35 mm). The heat discharge extensions 62 may take the form of fins (as shown in FIG. 8) or pins (not shown). Fin-shaped discharge extensions 62 may be continuous (as shown in FIG. 8) or may be discontinuous (not shown), and the extensions 62 may extend in a direction away from the heat transfer layer 16 and generally parallel to a longitudinal axis of flow of the hot fluid through the ceramic matrix, composite tube 12 hot fluid conduit 14. As described above, the heat discharge extensions 62 may also extend along a non-linear, tortuous path (not shown) so that the heat discharge extensions 82 make cooling fluid follow a greater distance per unit of hot fluid flow through the hot fluid conduit 14 to increase an amount of heat transfer to the cooling fluid passing adjacent the heat discharge extensions 62 to thereby increase an efficiency of the heat discharge extension heat exchanger 60.

[0036] The disclosure also includes manufacture of the heat transfer layer 16 so that the exterior surface of the heat transfer layer 28 is formed so that the layer is between about one-half and about ten times a wall thickness of the ceramic matrix composite tube 12. In an exemplary embodiment, the thickness of the wall of the ceramic matrix composite tube 12 ranges from between about 0.05 inches and about 0.25 inches (about 1.27 mm to about 6.35 mm).

[0037] This disclosure also includes a method of manufacturing the extreme environment heat exchanger 10. The method includes fabricating the hot fluid conduit 14 by forming a ceramic matrix composite 12 into an elongate form of about a uniform thickness 12 that defines the hot fluid conduit 14 within the ceramic matrix composite 12. Next, the hardenable material 18 is bonded to the ceramic matrix composite 12 so that the hardenable material 18 surrounds and is coextensive with the hot fluid conduit 14 defined by the ceramic matrix composite 12. Then, the hardenable material 18 is machined to produce the heat transfer layer 16 having about a uniform thickness surrounding the ceramic matrix composite 12, so that the thickness is between about one-half and about ten times a wall thickness of the ceramic matrix composite tube. The method may also include machining into the exterior surface 28 of the heat transfer layer 16 a plurality of channels 56 (FIG. 7) or a plurality of second portions 26 (FIG. 1) of cool fluid passages 24 having longitudinal axes parallel to a direction of flow of the hot fluid through the hot fluid conduit 14 and then securing a metal pipe 52 within each of the plurality of channels 56. The method may also include forming the heat transfer layer 16 to define a plurality of heat discharge extensions 62 instead, of the plurality of channels 56.

[0038] The method may also include securing the heat transfer layer 16 and attached ceramic matrix composite 12 within the metal pipe 20 so that the metal pipe 20 covers the plurality of channels 56 in the exterior surface 28 of the heat transfer layer 16 to form a plurality of cool fluid passages 24. The method may also include securing the heat transfer layer 16 and attached ceramic matrix composite 12 within a circumferentially displaced metal pipe 32, securing the coil seal 40 between the exterior surface 28 of the heat transfer layer 16 and an interior surface 36 of the displaced metal pipe 32 so that the coil seal 40 covers the plurality of second portions 26 (FIG. 1) of cool fluid passages 24 in the heat transfer layer 16, and the coil 40 expanding longitudinally, axially and rotationally about itself to absorb heat and minimize thermal expansion stress on the displaced metal pipe 32.

[0039] It is pointed out that silicon carbide based ceramic matrix composites are superior to metals in corrosion resistance for chemicals such as hydrofluoric acid, bromine, and nitric acid. The ceramic matrix composite may also be manufactured to exterior surface finish tolerances of about 0.005 inches (0.127 millimeters (mm)).

[0040] While the above disclosure has been presented with respect to the described and illustrated embodiments of an extreme environment heat exchanger 10, 30, 50, and 60 it is to be understood that other embodiments are within the scope of this disclosure. While the described and illustrated embodiments show cylindrical fluid conduits, pipe and tubes, it is to be understood that the conduits, pipes and tubes may take non-cylindrical forms, such as box-like or variable shape forms, etc. Accordingly, reference should be made primarily to the following claims rather than the foregoing description to determine the scope of the disclosure.