3D PRINTED FEATURES ON NUCLEAR FUEL CLADDING FOR OPTIMIZED HEAT TRANSFER

Abstract

A nuclear fuel cladding with improved thermomechanical properties is provided. The nuclear fuel cladding includes a double-walled construction having inner and outer hexagonal sidewalls. The inner sidewall and the outer sidewall are spaced apart from each other to form a cooling channel therebetween, and the inner sidewall surrounds a nuclear fuel and is spaced apart from the nuclear fuel by a small gap. Helical fins extend into the cooling channel to interconnect the inner sidewall and the outer sidewall. Resilient fingers extend toward the nuclear fuel through the small gap to comply with variations in the size of the nuclear fuel due to fabrication tolerances as well as thermal expansion and swelling of the nuclear fuel, for example UO.sub.2, when undergoing fission. The nuclear fuel cladding is formed according to an additive manufacturing process, for example laser powder bed fusion printing.

Claims

1. A reactor comprising: a barrel; and a core module encapsulated within the barrel, the core module containing a plurality of fuel cans packed therein, each of the plurality of fuel cans comprising a fissile fuel and cladding, the cladding comprising: a pair of walls formed from a first metal alloy and spaced apart from each other to form a channel configured to circulate a cooling gas during operation of the reactor, wherein the pair of walls is arranged and configured to encapsulate the fissile fuel and form a gap between the fissile fuel and one wall of the pair of walls that is adjacent to the fissile fuel, first structures formed from a second metal alloy and extending into the channel, and second structures formed from a third metal alloy and extending toward the fissile fuel through the gap, the second structures being flexible to (i) comply to variations in size of the fissile fuel introduced during manufacturing or caused by operation of the reactor, (ii) improve heat transfer through the gap, and (iii) prevent collapse of the gap and strain on the sidewalls of the fuel can.

2. The reactor of claim 1, wherein the first and second structures of the cladding have geometries comprising one or more of springs, fins, or knobs.

3. The reactor of claim 1, wherein the cladding includes first and second nested hexagonal sleeves.

4. The reactor of claim 1, wherein the first structures include a plurality of fins that interconnect a first one of the pair of walls with a second one of the pair of walls.

5. The reactor of claim 1, wherein the cooling gas circulated through the channel during operation of the reactor comprises He.

6. The reactor of claim 1, wherein the first metal alloy is Type 304 or Type 316 stainless steel.

7. The reactor of claim 1, wherein the first metal alloy is 316L stainless steel.

8. The reactor of claim 1, wherein the first metal alloy, the second metal alloy, and the third metal alloy comprise the same metal alloys.

9. The reactor of claim 1, wherein the first metal alloy, the second metal alloy, and the third metal alloy comprise at least two different metal alloys.

10. The reactor of claim 1, wherein the first metal alloy, the second metal alloy, and the third metal alloy each comprise a different metal alloy.

11. The reactor of claim 1, wherein the first metal alloy comprises stainless steel and wherein the third metal alloy comprises a copper alloy.

12. Cladding for a fissile fuel, the cladding comprising: an inner wall and an outer wall formed from a first metal alloy and spaced apart from each other to form a cooling channel therebetween, wherein the fissile fuel is surrounded by the inner wall, and wherein a radially-inward facing surface of the inner wall is spaced apart from the fissile fuel via a radial gap; first structures formed from a second metal alloy that extend into the cooling channel to interconnect the inner wall and the outer wall; and second structures formed from a third metal alloy that extend toward the fissile fuel through the gap, the second structures being flexible to comply to variations in size of the fissile fuel due to fabrication tolerances as well as thermal expansion and swelling of the fissile fuel when undergoing fission.

13. The cladding of claim 12, wherein the first structures include a plurality of fins that interconnect a first one of the pair of walls with a second one of the pair of walls.

14. The cladding of claim 12, wherein the second structures include a plurality of resilient fingers extending radially inward from the inner wall.

15. The cladding of claim 12, wherein the inner wall and the outer wall comprise nested hexagonal sleeves.

16. The cladding of claim 12, wherein the first metal alloy is Type 304 or Type 316 stainless steel.

17. The cladding of claim 12, wherein the first metal alloy, the second metal alloy, and the third metal alloy comprise at least two different metal alloys.

18. The cladding of claim 17, wherein the first metal alloy comprises stainless steel and wherein the third metal alloy comprises a copper alloy.

19. The cladding of claim 12, wherein the first metal alloy, the second metal alloy, and the third metal alloy each comprise a different metal alloy.

20. A method for additively manufacturing the cladding of claim 14, the method including laser powder bed fusion 3D printing.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0011] FIG. 1 illustrates heat transfer from a nuclear fuel to a thermal fluid (a moving coolant).

[0012] FIG. 2 is a top-down view of a fuel can including a double-walled cladding and a nuclear fuel.

[0013] FIG. 3 illustrates a portion of the double-walled cladding as including knobs or resilient fingers.

[0014] FIG. 4 illustrates multiple fuel cans including a double-walled cladding in a side-by-side relationship.

[0015] FIG. 5 illustrates a nuclear fuel module including a plurality of adjacent hexagonal fuel cans.

[0016] FIG. 6 illustrates an exemplary nuclear reactor for use with the nuclear fuel cladding of the current embodiments.

DETAILED DESCRIPTION OF THE CURRENT EMBODIMENTS

[0017] As discussed herein, the current embodiments include a double-walled cladding structure that is additively manufactured using laser powder bed fusion. The cladding structure contains internal spring mechanisms to enhance heat transfer and to accommodate variable fuel dimensions as well as fuel thermal expansion and irradiation-induced swelling. The flow of coolant through the double-walled cladding structure can be optimized radially and axially via interconnecting fins, thereby yielding uniform coolant outlet temperature distributions. The rigid, double-walled cladding structure also establishes a fixed cooling channel that is independent of the surrounding fuel elements. Compared to conventional reactors in which the cooling channel is established between multiple adjacent fuel elements and depends on the fit-up of the entire reactor core, the uncertainties in the coolant channel geometry in the present invention are greatly reduced.

[0018] Referring now to FIGS. 2-4, a double-walled cladding structure for a nuclear fuel 100 is illustrated and generally designated 10. Collectively, the cladding structure 10 and the nuclear fuel 100 comprise a fuel can 12 (i.e., a nuclear fuel element) for a nuclear reactor. The cladding structure 10 includes an inner sidewall 14 that is spaced apart from an outer sidewall 16 to form a cooling channel 18 therebetween. The inner and outer sidewalls 14, 16 are hexagonal in the illustrated embodiment, primarily because a hexagon is mathematically optimum for enclosing an area with a repeating lattice structure and is infinitely repeatable. However, other constructions are possible in other embodiments, including cylindrical tubes, rectangular tubes, or any other construction including those that are axially and/or radially asymmetric. The cladding structure 10 also includes an integral base 20 and a separate lid 22 (visible in FIG. 4), the lid 22 being welded to the upper periphery of the inner sidewall 14.

[0019] The inner sidewall 14, the base 20, and the lid 22 define an internal fuel cavity for the nuclear fuel 100. In addition, the cladding structure 10 includes a plurality of first structures that interconnect the inner sidewall 14 and the outer wall 16. The plurality of first structures comprise a plurality of fins 24 that sub-divide the cooling channel 18 into multiple sub-channels 18a, 18b, 18c, etc., such that n number of fins creates n number of sub-channels. The illustrated embodiment includes fifteen fins and fifteen sub-channels, however greater or fewer number of fins and sub-channels can be used in other embodiments. The fins 24 extend from the lower periphery of the double-walled cladding structure 10 to the upper periphery of the double-walled cladding structure 10. The cooling channel 18 extends entirely through the cladding structure 10, being open at upper and lower ends of the cladding structure 10 for circulation of the coolant therethrough. The fins 24 are non-linear or curvilinear and are oriented at a non-zero angle relative to vertical to direct the cooling gas through the sub-channels at a non-zero angle relative to vertical, thereby promoting radial and axial movement of the coolant.

[0020] The cladding structure 10 also includes a plurality of second structures that extend radially inward, toward the nuclear fuel 12. The plurality of second structures can include essentially any geometry that enhances heat transfer from the nuclear fuel 12 and that accommodates a wide range of as-fabricated fuel dimensions as well as thermal expansion and irradiation-induced swelling of the nuclear fuel 12. As show in FIG. 2, for example, each inward-facing surface of the inner sidewall 14 includes four vertical fins 26. Along their major axis, the vertical fins 26 extend along a substantial portion of the height of the inner sidewall 14. Along their minor axis, the vertical fins 26 are angled at a non-zero angle (e.g., 12 degrees) relative to the inner sidewall 14. As the nuclear fuel 100 expands, the fins 26 flex toward the inner sidewall 14, reducing to a lesser angle (e.g., 6 degrees). The vertical fins 26 remain in contact with the nuclear fuel 100 at all times, thus providing improved thermal conductivity (and a lesser thermal gradient) across the gas-filled gap between the nuclear fuel 100 and the inner sidewall 14. The fins 26 are oriented vertically in the illustrated embodiment, but can be oriented horizontally or at a non-zero angle relative to horizontal in other embodiments.

[0021] The plurality of second structures can alternatively include knobs or resiliently deformable fingers. As shown in FIG. 3 for example, each inward-facing surface of the inner sidewall 14 can include five vertical knobs 28 or eight horizontal rows of resiliently deformable fingers 30. Akin to the angled fins 26 illustrated in FIG. 2, the vertical knobs 28 and the resiliently deformable fingers 30 remain in contact with the nuclear fuel 100 at all times, thus providing improved thermal conductivity (and a lesser thermal gradient) across the gap between the nuclear fuel 100 and the inner sidewall 14.

[0022] In the illustrated embodiment, each cladding structure 10 comprises a fuel can 12 that is 4 cm wide (flat-to-flat width) and 10 cm in length. The fuel cans 12 are oriented side-by-side and are stacked upon one another to form a core module. As illustrated in FIG. 5, for example, the core module 40 is approximately 80 cm in diameter with an active fuel length of about 100 cm and is surrounded by a barrel 42. The thickness of the inner sidewall 14 and the outer sidewall 16 is 0.5 mm, and the thickness of the flow channel 18 is 0.4 cm. The core module 40 can include a moderator material, for example yttrium hydride or zirconium hydride.

[0023] A manufacturing method according to one embodiment includes laser powder bed printing the cladding structure, wherein the cladding structure is formed from Type 304 or Type 316 stainless steel. Specifically, a powder feedstock is deposited in sequential layers, one on top of the other. Following the deposit of each layer of powder feedstock, a fiber optic laser fuses the powder feedstock together in accordance with a computer model (e.g., CAD model) of the cladding structure. The laser powder bed printing process allows geometrical complexity, particularly for the first and second structures of the cladding structure, that are not possible using conventional manufacturing techniques. Once the cladding structure is fully printed, the unbound powder is removed, yielding for example the near net-shaped cladding structure shown in FIG. 4. Post processing steps can include heat treatments, machining steps, and polish processes.

[0024] Alternative manufacturing methods include direct metal deposition and binder jet printing to allow the use of different metal alloys. For example, two or more features of the cladding structure can be additively manufactured from different metal alloys according to a direct metal deposition method. As one example, the outer hexagonal wall, and optionally the inner hexagonal wall and the first structures, can be formed from stainless steel, while the second structures can be formed from a ductile but thermally conductive metal such as copper. As another example, the inner and outer hexagonal walls and the first structures can be formed from a first metal, for example stainless steel, and the second structures can be formed from a ductile but thermally conductive metal such as copper. Other combinations of metals and metal alloys can be used in other embodiments as desired.

[0025] Subsequent to the formation of the cladding structure, nuclear fuel is added to the internal fuel cavity. The nuclear fuel can include uranium, plutonium, thorium, or other fissile elements, and can be ceramic pellets, bare fuel kernels or coated particles, for example tri-structural isotropic (TRISO) particles, bi-structural isotropic (BISO) particles, and bare uranium-bearing (e.g., UO.sub.2, UC, UN, or there combinations) spheres (fuel kernels) containing fissile uranium. The internal fuel cavity is then sealed by welding the lid 22 to the inner sidewall 14. The resultant fuel can 12 includes a generally stackable construction. When arranged and stacked, the cooling channel(s) 18 of each fuel can 12 are in fluid communication with the cooling channel(s) 18 of a vertically adjacent fuel can 12. Further, the cooling channels 18 can be manufactured with surface features to improve cooling of the nuclear fuel therein, as the thermal energy is optimally transmitted to the cooling fluid.

[0026] The foregoing fuel cans 12 can be used with a wide variety of cooling fluids, nuclear fuels, moderators, and core designs. As one example, the fuel cans 12 can be used with a He coolant, which is favored because He is chemically inert and has the ability to adopt more simple heat rejection systems without additional intermediate heat transfer loops. The fuel form can include conventionally fabricated UO.sub.2 in hexagonal geometries to fit within the internal fuel cavity. The moderators can include a metal hydride moderator, for example yttrium hydride, which exhibits improved thermal stability over zirconium hydride. An optional core design is shown in FIG. 6. The reactor core 50 includes a core module 40, a coolant inlet 52, and a coolant outlet 54. The coolant inlet 52 and the coolant outlet 54 are located at the base of the reactor core 50. Coolant (e.g., He gas) moves along the exterior of the core module 40, passes through the cooling channels 18 of vertically stacked fuel cans 12, and is diverted to the outlet 54 by a baffle 56. Other core designs are also possible however, and the core design of FIG. 6 is merely presented for illustrative purposes.

[0027] The above description is that of current embodiments of the invention. Various alterations and changes can be made without departing from the spirit and broader aspects of the invention as defined in the appended claims, which are to be interpreted in accordance with the principles of patent law including the doctrine of equivalents. This disclosure is presented for illustrative purposes and should not be interpreted as an exhaustive description of all embodiments of the invention or to limit the scope of the claims to the specific elements illustrated or described in connection with these embodiments. For example, and without limitation, any individual element(s) of the described invention may be replaced by alternative elements that provide substantially similar functionality or otherwise provide adequate operation. This includes, for example, presently known alternative elements, such as those that might be currently known to one skilled in the art, and alternative elements that may be developed in the future, such as those that one skilled in the art might, upon development, recognize as an alternative. Further, the disclosed embodiments include a plurality of features that are described in concert and that might cooperatively provide a collection of benefits. The present invention is not limited to only those embodiments that include all of these features or that provide all of the stated benefits, except to the extent otherwise expressly set forth in the issued claims. Any reference to claim elements in the singular, for example, using the articles “a,” “an,” “the” or “said,” is not to be construed as limiting the element to the singular.