WO2009139899A1 - Heat pipe fission fuel element - Google Patents

Heat pipe fission fuel element Download PDF

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Publication number
WO2009139899A1
WO2009139899A1 PCT/US2009/003028 US2009003028W WO2009139899A1 WO 2009139899 A1 WO2009139899 A1 WO 2009139899A1 US 2009003028 W US2009003028 W US 2009003028W WO 2009139899 A1 WO2009139899 A1 WO 2009139899A1
Authority
WO
WIPO (PCT)
Prior art keywords
nuclear fission
heat pipe
fission fuel
cavity
fuel element
Prior art date
Application number
PCT/US2009/003028
Other languages
French (fr)
Inventor
Charles E. Ahlfeld
John Rogers Gilleland
Roderick A . Hyde
Muriel Y . Ishikawa
David G. Mcalees
Nathan P. Myhrvold
Thomas Allan Weaver
Charles Whitmer
Jr. Lowell L. Wood
Original Assignee
Searete Llc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Searete Llc filed Critical Searete Llc
Priority to CN200980122734.4A priority Critical patent/CN102067241B/en
Priority to JP2011509489A priority patent/JP2011523045A/en
Priority to EP09746986.0A priority patent/EP2291850B1/en
Priority to RU2010147880/07A priority patent/RU2492533C2/en
Publication of WO2009139899A1 publication Critical patent/WO2009139899A1/en

Links

Classifications

    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21C—NUCLEAR REACTORS
    • G21C15/00—Cooling arrangements within the pressure vessel containing the core; Selection of specific coolants
    • G21C15/02—Arrangements or disposition of passages in which heat is transferred to the coolant; Coolant flow control devices
    • G21C15/04—Arrangements or disposition of passages in which heat is transferred to the coolant; Coolant flow control devices from fissile or breeder material
    • G21C15/06—Arrangements or disposition of passages in which heat is transferred to the coolant; Coolant flow control devices from fissile or breeder material in fuel elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D15/00—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies
    • F28D15/02—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes
    • F28D15/04—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure
    • F28D15/046—Heat-exchange apparatus with the intermediate heat-transfer medium in closed tubes passing into or through the conduit walls ; Heat-exchange apparatus employing intermediate heat-transfer medium or bodies in which the medium condenses and evaporates, e.g. heat pipes with tubes having a capillary structure characterised by the material or the construction of the capillary structure
    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21C—NUCLEAR REACTORS
    • G21C1/00—Reactor types
    • G21C1/02—Fast fission reactors, i.e. reactors not using a moderator ; Metal cooled reactors; Fast breeders
    • G21C1/022—Fast fission reactors, i.e. reactors not using a moderator ; Metal cooled reactors; Fast breeders characterised by the design or properties of the core
    • G21C1/026—Reactors not needing refueling, i.e. reactors of the type breed-and-burn, e.g. travelling or deflagration wave reactors or seed-blanket reactors
    • G—PHYSICS
    • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21C—NUCLEAR REACTORS
    • G21C3/00—Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
    • G21C3/02—Fuel elements
    • G21C3/04—Constructional details
    • G21C3/044—Fuel elements with porous or capillary structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0054—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for nuclear applications
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00—Energy generation of nuclear origin
    • Y02E30/30—Nuclear fission reactors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Definitions

  • the present application relates to nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto.
  • Illustrative embodiments provide nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto.
  • Illustrative embodiments and aspects include, without limitation, nuclear fission fuel elements, heat pipe assemblies, heat pipes, methods of fabricating a nuclear fission fuel element, methods of fabricating a heat pipe assembly, and the like.
  • FIG. IA is a perspective view in schematic form of an illustrative nuclear fission fuel element.
  • FIG. IB is a perspective view in schematic form of details of the nuclear fission fuel element of FIG. IA.
  • FIG. 2A is a cutaway side plan view in schematic form of an illustrative nuclear fission fuel element.
  • FIG. 2B is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element.
  • FIG. 2C is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element.
  • FIG. 2D is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element.
  • FIG. 3A is a cutaway end plan view in schematic form of a portion of embodiments of the illustrative nuclear fission fuel elements of FIGS. 2A-2D.
  • FIG. 3B illustrates details of the portion shown in FIG. 3 A.
  • FIG. 4A is a cutaway side plan view in schematic form of an illustrative heat pipe.
  • FIG. 4B is a cutaway side plan view in schematic form of another illustrative heat pipe.
  • FIG. 4C is a cutaway side plan view in schematic form of another illustrative heat pipe.
  • FIG. 4D is a cutaway side plan view in schematic form of another illustrative heat pipe.
  • FIG. 5A is a cutaway end plan view in schematic form of a portion of embodiments of the illustrative heat pipes of FIGS. 4A-4D.
  • FIG. 5B illustrates details of the portion shown in FIG. 5 A.
  • FIG. 5C is a cutaway end plan view in schematic form of a portion of other embodiments of the illustrative heat pipes of FIGS. 4A-4D.
  • FIG. 6 is a cutaway side plan view in schematic form of a portion of other embodiments of the illustrative heat pipes of FIGS. 4A-4D.
  • FIG. 7A is a flow chart of an illustrative method of fabricating a nuclear fission fuel element.
  • FIGS. 7B-7I are flow charts of details of portions of the flow chart of FIG. 7A.
  • FIG. 8A is a flow chart of an illustrative method of fabricating a heat pipe assembly.
  • FIGS. 8B-8H are flow charts of details of portions of the flow chart of FIG. 8A.
  • illustrative embodiments provide nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto.
  • Illustrative embodiments and aspects include, without limitation, nuclear fission fuel elements, heat pipe assemblies, heat pipes, methods of fabricating a nuclear fission fuel element, methods of fabricating a heat pipe assembly, and the like.
  • some embodiments may be provided as nuclear fission fuel elements that include at least one heat pipe disposed therein while some other embodiments may be provided as heat pipes with nuclear fission fuel material disposed therein.
  • the illustrative nuclear fission fuel element 10 suitably includes nuclear fission fuel material 12. At least a portion 14 (shown in phantom) of a heat pipe 16 is disposed within the nuclear fission fuel material 12.
  • the nuclear fission fuel material 12 suitably may be any type of nuclear fission fuel material as desired for a particular application.
  • the nuclear fission fuel material 12 may be provided in the form of a metal, a compound, an alloy, or any combination thereof as desired.
  • the nuclear fission fuel material 12 may be usable in any type of nuclear fission reactor whatsoever with any neutron spectrum whatsoever.
  • the nuclear fission fuel material 12 may be usable in nuclear fission reactors having a thermal neutron spectrum.
  • the nuclear fission fuel material 12 may be usable in nuclear fission reactors having a fast neutron spectrum.
  • the nuclear fission fuel material 12 may be usable in breeder reactors, such as without limitation fast breeder reactors like nuclear fission deflagration wave fast breeder reactors.
  • breeder reactors such as without limitation fast breeder reactors like nuclear fission deflagration wave fast breeder reactors.
  • Nuclear fission deflagration wave fast breeder reactors are discussed in United States Patent Application No. 11/605,943, entitled AUTOMATED NUCLEAR POWER REACTOR FOR LONG-TERM OPERATION, naming RODERICK A. HYDE, MURIEL Y. ISHIKAWA, NATHAN P. MYHRVOLD, AND LOWELL L. WOOD, JR.
  • the nuclear fission fuel material 12 may include fissile material and/or fertile material.
  • the fissile material may include any one or more of 233 U, 235 U, and/or 239 Pu
  • the fertile material may include any one or more Of 232 Th and/or 238 U.
  • geometry of the nuclear fission fuel element 10. The geometric configuration shown in the drawing herein is used for illustrative purposes only.
  • a cavity 18 may be defined in the nuclear fission fuel material 12.
  • the cavity 18 may be a passageway that is defined through at least the portion 14 of the nuclear fission fuel material 12.
  • a surface 20 of the cavity 18 maybe a wall of the portion 14 (FIGURE IA) of the heat pipe 16 (FIGURE IA).
  • the cavity 18 may be defined in any suitable manner.
  • the cavity 18 may be defined by machining the cavity from the nuclear fission fuel material 12 in any manner as desired, such as by drilling, milling, stamping, or the like.
  • the cavity 18 may be defined by forming at least a portion 22 of the nuclear fission fuel material 12 around a shape, such as without limitation a mandrel (not shown). The forming may be performed in any manner as desired, such as without limitation by welding, casting, electroplating, pressing, molding, or the like.
  • a wall 24 of the heat pipe 16 extends from the cavity 18 in the nuclear fission fuel material 12, thereby substantially acting as an extension of the surface 20.
  • the cavity 18 can be considered to be substantially sealed.
  • the wall 24 may be made of any suitable material as desired for high-temperature operations and/or, if desired, a neutron flux environment.
  • the wall 24 may be made of any one or more of materials such as steel, niobium, vanadium, titanium, a refractory metal, and/or a refractory alloy.
  • the refractory metal may be niobium, tantalum, tungsten, hafnium, rhenium, or molybdenum.
  • refractory alloys include, rhenium-tantalum alloys as disclosed in U.S. patent 6902809, tantalum alloy T-111, molybdenum alloy TZM, tungsten alloy MT-185, or niobium alloy Nb-IZr.
  • a capillary structure 26 of the heat pipe 16 is defined within at least a portion of the cavity 18. That is, the surface 20 is a wall that surrounds a portion of the capillary structure 26. In some embodiments, the capillary structure 26 may also be defined in an interior of the heat pipe 16 that is outside the nuclear fission fuel material 12 and enclosed by the wall 24. In some embodiments, the capillary structure may be a wick. The wick may be made of any suitable material as desired, such as thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
  • the capillary structure 26 may be provided as axial grooves 28.
  • the grooves 28 are separated by lands 30.
  • additional grooves 32 within the groove 28 are defined additional grooves 32.
  • the grooves 32 may be separated from each other by two lands 34 or by one of the lands 30 and one of the lands 34.
  • the grooves 28 and 32 may be defined by any suitable method as desired, such as without limitation machining, etching, casting, stamping, or the like.
  • a working fluid 36 (FIGURE 3B) is provided within the heat pipe 16.
  • the working fluid 36 suitably is evaporable and condensable.
  • the working fluid 36 may include any suitable working fluid as desired, such as without limitation 7Li, sodium, potassium, or the like.
  • the heat pipe 16 includes an evaporator section 38 and a condenser section 40.
  • the evaporator section 38 may be disposed entirely or substantially within the nuclear fission fuel material 12. However, it will be appreciated that the evaporator section 38 need not be disposed entirely or substantially within the nuclear fission fuel material 12. To that end, in some other embodiments and as shown in FIGURES 2B and 2D, at least a portion of the evaporator section 38 is not within the nuclear fission fuel material 12.
  • the condenser section 40 may be disposed entirely external to the nuclear fission fuel material 12. However, in some other embodiments (not shown) a portion of the condenser section 40 may be disposed within the nuclear fission fuel material 12 and at least a portion of the condenser section 40 is not within the nuclear fission fuel material 12.
  • the heat pipe 16 may also include an adiabatic section 42.
  • the adiabatic section 42 may be disposed entirely external to the nuclear fission fuel material 12. However, in some other embodiments (not shown) a portion of the adiabatic section 42 may be disposed within the nuclear fission fuel material 12 and at least a portion a portion of the adiabatic section 42 is not within the nuclear fission fuel material 12.
  • heat from the nuclear fission fuel material 12 is transferred to the evaporator section 40 as indicated by arrows 44.
  • the working fluid 36 in the evaporator section 38 evaporates, as indicated by arrows 46, thereby undergoing phase transformation from a liquid to a gas.
  • the working fluid 36 in gaseous form moves through the heat pipe 16, as indicated by arrows 48, from the evaporator section 38, when applicable (in some embodiments) through the adiabatic section 42 (FIGURES 2C and 2D), and to the condenser section 40.
  • heat from the working fluid 36 is transferred out of the heat pipe 16, as indicated by arrows 50.
  • the working fluid 36 in the condenser section 40 condenses, as indicated by arrows 52, thereby undergoing phase transformation from a gas to a liquid.
  • the working fluid 36 in liquid form returns from the condenser section 40 to the evaporator section 38, as indicated by arrows 54, via capillary action in the capillary structure 26.
  • the working fluid 36 in liquid form returns from the condenser section 40 through the adiabatic section 42 (FIGURES 2C and 2D) to the evaporator section 38.
  • the assembly shown in FIGURES IA, IB, and 2A-2D can be a heat pipe assembly that includes the heat pipe 16 and the nuclear fission fuel material 12.
  • the nuclear fission fuel material 12 is integral with the heat pipe 16 and is disposed in thermal communication with the heat pipe 16. That is, the nuclear fission fuel material 12 defines the cavity 18 therein and at least the portion 14 of the heat pipe 16 is disposed within the cavity 18.
  • a heat pipe assembly 60 includes a heat pipe device 62.
  • the heat pipe device 62 includes a wall section 63.
  • nuclear fission fuel material 64 is integral with the heat pipe device 62 and is disposed in thermal communication with the heat pipe device 62.
  • the nuclear fission fuel material 64 suitably is similar to the nuclear fission fuel material 12 (FIGURES IA, IB, and 2A-2D) described above, and details need not be repeated.
  • Embodiments of the heat pipe assembly 60 share some features in common with the nuclear fission fuel element 10 (FIGURES IA, IB, 2A-2D, 3 A, and 3B). Common reference numbers will be used to refer to common features, and details need not be repeated for an understanding.
  • the heat pipe device 62 defines a cavity 66 therein.
  • a surface 65 of the wall section 63 defines a surface of the cavity 66.
  • the nuclear fission fuel material 64 is disposed within at least a portion of the cavity 66.
  • the nuclear fission fuel material 64 may be disposed within the capillary structure 26.
  • the nuclear fission fuel material 64 need not be disposed within the capillary structure 26 and may be disposed anywhere whatsoever within the cavity 66 as desired. As another illustrative example given without limitation and referring additionally to FIGURE 5C, in some embodiments the nuclear fission fuel material 64 may be disposed within the cavity 64 on one or more support structures 67 that hold the nuclear fission fuel material 64 in place. Additional capillary structure 26A is disposed about the exterior of the nuclear fission fuel material 64.
  • At least one of the support structures 67 is a liquid transport structure, such as a channel, capillary structure, or the like, that can transport the working fluid in its liquid phase via capillary action between the capillary structure 26A disposed about the exterior of the nuclear fission fuel material 64 and the capillary structure 26 disposed about the surface of the cavity 66.
  • a liquid transport structure such as a channel, capillary structure, or the like
  • the heat pipe device 62 includes the evaporator section 38 and the condenser section 40.
  • the nuclear fission fuel material 64 may be disposed entirely or substantially within the evaporator section 38.
  • the nuclear fission fuel material 64 need not be disposed entirely or substantially within the evaporator section 38.
  • at least a portion of the nuclear fission fuel material 64 is not within the evaporator section 38.
  • the nuclear fission fuel material 64 may have a capillary structure. If desired, in some other embodiments the nuclear fission fuel material 64 may have a sintered powdered fuel microstructure, or a foam microstructure, or a high density microstructure, or the like.
  • the heat pipe device 62 includes the capillary structure 26.
  • the capillary structure 26 may include the grooves 28 defined in the surface 65 as described above between the lands 30.
  • the capillary structure 26 may include the grooves 32 defined in the surface 65 as described above between the lands 30 and 34.
  • the capillary structure may include a wick as described above.
  • the heat pipe assembly 60 also includes the working fluid 36 as described above. Also, in some embodiments, the heat pipe device 62 may include the adiabatic section 42 (FIGURES 4C and 4D).
  • heat from the nuclear fission fuel material 64 is transferred to the evaporator section 40.
  • the working fluid 36 in the evaporator section 38 evaporates, as indicated by arrows 46, thereby undergoing phase transformation from a liquid to a gas.
  • the working fluid 36 in gaseous form moves through the heat pipe device 62, as indicated by arrows 48, from the evaporator section 38, when applicable (in some embodiments) through the adiabatic section 42 (FIGURES 4C and 4D), and to the condenser section 40.
  • heat from the working fluid 36 is transferred out of the heat pipe device 62, as indicated by arrows 50.
  • the working fluid 36 in the condenser section 40 condenses, as indicated by arrows 52, thereby undergoing phase transformation from a gas to a liquid.
  • the working fluid 36 in liquid form returns from the condenser section 40 to the evaporator section 38, as indicated by arrows 54, via capillary action in the capillary structure 26.
  • the working fluid 36 in liquid form returns from the condenser section 40 through the adiabatic section 42 (FIGURES 4C and 4D) to the evaporator section 38.
  • a heat pipe device 62A has a wall section 63 A that includes at least one layer of structural material 68 and at least one layer of nuclear fission fuel material 64A.
  • the nuclear fission fuel material 64A can be disposed outside of the cavity 66.
  • only one layer of the nuclear fission fuel material 64A and the structural material 68 are shown. However, it will be appreciated that, in some embodiments, any number of layers of the nuclear fission fuel material 64 A and the structural material 68 may be provided as desired.
  • the structural material 68 may include any one or more of materials such as steel, niobium, vanadium, titanium, a refractory metal, and/or a refractory alloy.
  • the refractory metal may be niobium, tantalum, tungsten, hafnium, rhenium, or molybdenum.
  • Non-limiting examples of refractory alloys include, rhenium-tantalum alloys as disclosed in U.S. patent 6902809, tantalum alloy T-111, molybdenum alloy TZM, tungsten alloy MT-185, or niobium alloy Nb-IZr.
  • a layer of the nuclear fission fuel material 64 A can be disposed entirely or substantially within the evaporator section 38.
  • one or more layers of the nuclear fission fuel material 64A maybe disposed in at least a portion of the adiabatic section (if provided) and/or the condenser section.
  • an illustrative method 80 is provided for fabricating a nuclear fission fuel element.
  • the method 80 starts at a block 82.
  • nuclear fission fuel material is provided.
  • At a block 86 at least a portion of at least one heat pipe is disposed within the nuclear fission fuel material.
  • the method 80 stops at a block 88.
  • disposing at least a portion of at least one heat pipe within the nuclear fission fuel material at the block 86 may include further processes.
  • a cavity may be defined within at least a portion of the nuclear fission fuel material.
  • a capillary structure may be disposed within at least a portion of the cavity.
  • a working fluid may be disposed within the cavity.
  • defining a cavity within at least a portion of the nuclear fission fuel material at the block 90 can include machining the cavity at a block 96.
  • machining the cavity at the block 96 can be performed by a machining operation such as drilling, milling, stamping, or the like.
  • defining a cavity within at least a portion of the nuclear fission fuel material at the block 90 can include forming at least a portion of the nuclear fission fuel material around a shape, such as without limitation a mandrel, at a block 98.
  • forming can be performed by an operation such as welding, casting, electroplating, pressing, molding, or the like.
  • disposing a capillary structure within at least a portion of the cavity at the block 92 can include defining a plurality of grooves in a surface of the cavity at a block 100.
  • defining a plurality of grooves in a surface of the cavity at the block 100 can be performed by an operation such as machining, etching, casting, stamping, or the like.
  • disposing a capillary structure within at least a portion of the cavity at the block 92 can include disposing a wick within at least a portion of the cavity at a block 102.
  • a size of the cavity can be determined based upon accommodating predetermined power production properties of the nuclear fission fuel element.
  • the cross-sectional area of the cavity may be chosen by dividing a predetermined power production value of the nuclear fission fuel element by a specified axial heat flux value of the working fluid.
  • a size of the cavity can be determined based upon accommodating predetermined heat transfer properties of the working fluid.
  • the cross-sectional area of the cavity may be chosen in order to achieve a desirable axial heat transport capability from the heat pipe working fluid. In some embodiments, this selection suitably may take into account the operational vapor density of the working fluid, its latent heat of vaporization, and a desirable flow velocity or mach number. In another example, a lateral dimension of the cavity can be chosen in order to provide a desirable Reynold's number for vapor flow.
  • a size of the cavity can be determined based upon accommodating volatile fission products.
  • the cavity volume may be selected based upon the pressure developed by a specified amount of gaseous fission products within the volume.
  • the cavity volume may be selected based upon the effects of the inertia of a specified amount of gaseous fission products within the volume on the heat transfer properties of the heat pipe.
  • an illustrative method 110 is provided for fabricating a heat pipe assembly.
  • the method 110 starts at a block 112.
  • a heat pipe device is provided.
  • nuclear fission fuel material is disposed integral with the heat pipe device and in thermal communication with the heat pipe device.
  • the method 110 stops at a block 118.
  • providing a heat pipe device at the block 114 may include further processes.
  • a heat pipe body having a wall section may be provided.
  • a cavity may be defined within at least a portion of the wall section.
  • a capillary structure may be disposed within at least a portion of the cavity.
  • a working fluid may be disposed within the cavity.
  • disposing nuclear fission fuel material in thermal communication with the heat pipe device at the block 116 may include disposing nuclear fission fuel material within at least a portion of the wall section at a block 128.
  • disposing nuclear fission fuel material in thermal communication with the heat pipe device at the block 116 may include disposing nuclear fission fuel material within at least a portion of the cavity at a block 130.
  • defining a cavity within the wall section at the block 122 may include machining the cavity.
  • machining the cavity at the block 122 can be performed by a machining operation such as drilling, milling, stamping, or the like.
  • defining a cavity within at least a portion of the wall section at the block 122 may include forming the at least a portion of the wall section around a shape, such as without limitation a mandrel, at a block 134.
  • forming can be performed by an operation such as welding, casting, electroplating, pressing, molding, or the like.
  • disposing a capillary structure within at least a portion of the cavity at the block 124 may include defining a plurality of grooves in a surface of the cavity at a block 136.
  • defining a plurality of grooves in a surface of the cavity at the block 136 can be performed by an operation such as machining, etching, casting, stamping, or the like.
  • disposing a capillary structure within at least a portion of the cavity at the block 124 may include disposing a wick within at least a portion of the cavity at a block 138.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Monitoring And Testing Of Nuclear Reactors (AREA)
  • Fuel Cell (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

Illustrative embodiments provide nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto. Illustrative embodiments and aspects include, without limitation, nuclear fission fuel elements, heat pipe assemblies, heat pipes, methods of fabricating a nuclear fission fuel element, methods of fabricating a heat pipe assembly, and the like.

Description

Heat Pipe Fission Fuel Element
Inventors: Charles E. Ahlfeld; John Rogers Gilleland;
Roderick A. Hyde; Muriel Y. Ishikawa; David G. McAlees; Nathan P. Myhrvold; Thomas Allan Weaver; Charles Whitmer; Lowell L. Wood, Jr.
BACKGROUND
The present application relates to nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto.
SUMMARY
Illustrative embodiments provide nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto. Illustrative embodiments and aspects include, without limitation, nuclear fission fuel elements, heat pipe assemblies, heat pipes, methods of fabricating a nuclear fission fuel element, methods of fabricating a heat pipe assembly, and the like.
The foregoing summary is illustrative only and is not intended to be in any way limiting. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features will become apparent by reference to the drawings and the following detailed description.
BRIEF DESCRIPTION OF THE FIGURES
FIG. IA is a perspective view in schematic form of an illustrative nuclear fission fuel element.
FIG. IB is a perspective view in schematic form of details of the nuclear fission fuel element of FIG. IA. FIG. 2A is a cutaway side plan view in schematic form of an illustrative nuclear fission fuel element.
FIG. 2B is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element. FIG. 2C is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element.
FIG. 2D is a cutaway side plan view in schematic form of another illustrative nuclear fission fuel element.
FIG. 3A is a cutaway end plan view in schematic form of a portion of embodiments of the illustrative nuclear fission fuel elements of FIGS. 2A-2D. FIG. 3B illustrates details of the portion shown in FIG. 3 A. FIG. 4A is a cutaway side plan view in schematic form of an illustrative heat pipe.
FIG. 4B is a cutaway side plan view in schematic form of another illustrative heat pipe.
FIG. 4C is a cutaway side plan view in schematic form of another illustrative heat pipe.
FIG. 4D is a cutaway side plan view in schematic form of another illustrative heat pipe. FIG. 5A is a cutaway end plan view in schematic form of a portion of embodiments of the illustrative heat pipes of FIGS. 4A-4D.
FIG. 5B illustrates details of the portion shown in FIG. 5 A. FIG. 5C is a cutaway end plan view in schematic form of a portion of other embodiments of the illustrative heat pipes of FIGS. 4A-4D. FIG. 6 is a cutaway side plan view in schematic form of a portion of other embodiments of the illustrative heat pipes of FIGS. 4A-4D.
FIG. 7A is a flow chart of an illustrative method of fabricating a nuclear fission fuel element.
FIGS. 7B-7I are flow charts of details of portions of the flow chart of FIG. 7A. FIG. 8A is a flow chart of an illustrative method of fabricating a heat pipe assembly.
FIGS. 8B-8H are flow charts of details of portions of the flow chart of FIG. 8A.
DETAILED DESCRIPTION
In the following detailed description, reference is made to the accompanying drawings, which form a part hereof. In the drawings, similar symbols typically identify similar components, unless context dictates otherwise. The illustrative embodiments described in the detailed description, drawings, and claims are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented here.
By way of overview, illustrative embodiments provide nuclear fission fuel elements, and systems, applications, apparatuses, and methods related thereto. Illustrative embodiments and aspects include, without limitation, nuclear fission fuel elements, heat pipe assemblies, heat pipes, methods of fabricating a nuclear fission fuel element, methods of fabricating a heat pipe assembly, and the like.
Still byway of overview and given by way of non-limiting examples, some embodiments may be provided as nuclear fission fuel elements that include at least one heat pipe disposed therein while some other embodiments may be provided as heat pipes with nuclear fission fuel material disposed therein.
Still by way of overview and referring to FIGURE IA, an illustrative nuclear fission fuel element 10 will be discussed by way of illustration and not limitation. The illustrative nuclear fission fuel element 10 suitably includes nuclear fission fuel material 12. At least a portion 14 (shown in phantom) of a heat pipe 16 is disposed within the nuclear fission fuel material 12.
No limitations whatsoever are intended regarding the nuclear fission fuel material 12. To that end, the nuclear fission fuel material 12 suitably may be any type of nuclear fission fuel material as desired for a particular application. As such, the nuclear fission fuel material 12 may be provided in the form of a metal, a compound, an alloy, or any combination thereof as desired. The nuclear fission fuel material 12 may be usable in any type of nuclear fission reactor whatsoever with any neutron spectrum whatsoever. For example, in some embodiments the nuclear fission fuel material 12 may be usable in nuclear fission reactors having a thermal neutron spectrum. In some other embodiments the nuclear fission fuel material 12 may be usable in nuclear fission reactors having a fast neutron spectrum.
Moreover, in some embodiments the nuclear fission fuel material 12 may be usable in breeder reactors, such as without limitation fast breeder reactors like nuclear fission deflagration wave fast breeder reactors. Nuclear fission deflagration wave fast breeder reactors are discussed in United States Patent Application No. 11/605,943, entitled AUTOMATED NUCLEAR POWER REACTOR FOR LONG-TERM OPERATION, naming RODERICK A. HYDE, MURIEL Y. ISHIKAWA, NATHAN P. MYHRVOLD, AND LOWELL L. WOOD, JR. as inventors, filed 28 November 2006, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date, the entire contents of which are hereby incorporated by reference. To that end, in some embodiments the nuclear fission fuel material 12 may include fissile material and/or fertile material. In such cases, the fissile material may include any one or more of 233U, 235U, and/or 239Pu, and the fertile material may include any one or more Of232Th and/or 238U. Furthermore, no limitation whatsoever is intended regarding geometry of the nuclear fission fuel element 10. The geometric configuration shown in the drawing herein is used for illustrative purposes only. No limitation to any particular geometric configuration of the nuclear fission fuel element 10 is intended to be implied and, accordingly, none should be inferred. Referring additionally to FIGURE IB, in some embodiments a cavity 18 may be defined in the nuclear fission fuel material 12. In some embodiments, the cavity 18 may be a passageway that is defined through at least the portion 14 of the nuclear fission fuel material 12. Thus, in some embodiments, a surface 20 of the cavity 18 maybe a wall of the portion 14 (FIGURE IA) of the heat pipe 16 (FIGURE IA). The cavity 18 may be defined in any suitable manner. For example, in some embodiments the cavity 18 may be defined by machining the cavity from the nuclear fission fuel material 12 in any manner as desired, such as by drilling, milling, stamping, or the like. In some other embodiments the cavity 18 may be defined by forming at least a portion 22 of the nuclear fission fuel material 12 around a shape, such as without limitation a mandrel (not shown). The forming may be performed in any manner as desired, such as without limitation by welding, casting, electroplating, pressing, molding, or the like.
Referring now to FIGURES 2A-2D, a wall 24 of the heat pipe 16 extends from the cavity 18 in the nuclear fission fuel material 12, thereby substantially acting as an extension of the surface 20. As such, the cavity 18 can be considered to be substantially sealed. The wall 24 may be made of any suitable material as desired for high-temperature operations and/or, if desired, a neutron flux environment. Given by way of non-limiting example, in some embodiments the wall 24 may be made of any one or more of materials such as steel, niobium, vanadium, titanium, a refractory metal, and/or a refractory alloy. Given by way of non-limiting example, in some embodiments the refractory metal may be niobium, tantalum, tungsten, hafnium, rhenium, or molybdenum. Non-limiting examples of refractory alloys include, rhenium-tantalum alloys as disclosed in U.S. patent 6902809, tantalum alloy T-111, molybdenum alloy TZM, tungsten alloy MT-185, or niobium alloy Nb-IZr.
A capillary structure 26 of the heat pipe 16 is defined within at least a portion of the cavity 18. That is, the surface 20 is a wall that surrounds a portion of the capillary structure 26. In some embodiments, the capillary structure 26 may also be defined in an interior of the heat pipe 16 that is outside the nuclear fission fuel material 12 and enclosed by the wall 24. In some embodiments, the capillary structure may be a wick. The wick may be made of any suitable material as desired, such as thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
In some other embodiments and referring briefly to FIGURES 3 A and 3B, the capillary structure 26 may be provided as axial grooves 28. The grooves 28 are separated by lands 30. hi some embodiments, within the groove 28 are defined additional grooves 32. The grooves 32 may be separated from each other by two lands 34 or by one of the lands 30 and one of the lands 34. The grooves 28 and 32 may be defined by any suitable method as desired, such as without limitation machining, etching, casting, stamping, or the like.
Referring back to FIGURES 2A-2D and to FIGURE 3B, a working fluid 36 (FIGURE 3B) is provided within the heat pipe 16. The working fluid 36 suitably is evaporable and condensable. Given by way of non-limiting examples, the working fluid 36 may include any suitable working fluid as desired, such as without limitation 7Li, sodium, potassium, or the like.
Referring to FIGURES 2A-2D, the heat pipe 16 includes an evaporator section 38 and a condenser section 40. In some embodiments and as shown in FIGURES 2 A and 2C, the evaporator section 38 may be disposed entirely or substantially within the nuclear fission fuel material 12. However, it will be appreciated that the evaporator section 38 need not be disposed entirely or substantially within the nuclear fission fuel material 12. To that end, in some other embodiments and as shown in FIGURES 2B and 2D, at least a portion of the evaporator section 38 is not within the nuclear fission fuel material 12. As shown in FIGURES 2A-2D, in some embodiments the condenser section 40 may be disposed entirely external to the nuclear fission fuel material 12. However, in some other embodiments (not shown) a portion of the condenser section 40 may be disposed within the nuclear fission fuel material 12 and at least a portion of the condenser section 40 is not within the nuclear fission fuel material 12.
In some embodiments and referring now to FIGURES 2C and 2D, the heat pipe 16 may also include an adiabatic section 42. As shown in FIGURES 2C and 2D, in some embodiments the adiabatic section 42 may be disposed entirely external to the nuclear fission fuel material 12. However, in some other embodiments (not shown) a portion of the adiabatic section 42 may be disposed within the nuclear fission fuel material 12 and at least a portion a portion of the adiabatic section 42 is not within the nuclear fission fuel material 12.
Referring now to FIGURES 2A-2D, heat from the nuclear fission fuel material 12 is transferred to the evaporator section 40 as indicated by arrows 44. The working fluid 36 in the evaporator section 38 evaporates, as indicated by arrows 46, thereby undergoing phase transformation from a liquid to a gas. The working fluid 36 in gaseous form moves through the heat pipe 16, as indicated by arrows 48, from the evaporator section 38, when applicable (in some embodiments) through the adiabatic section 42 (FIGURES 2C and 2D), and to the condenser section 40. At the condenser section 40, heat from the working fluid 36 is transferred out of the heat pipe 16, as indicated by arrows 50. The working fluid 36 in the condenser section 40 condenses, as indicated by arrows 52, thereby undergoing phase transformation from a gas to a liquid. The working fluid 36 in liquid form returns from the condenser section 40 to the evaporator section 38, as indicated by arrows 54, via capillary action in the capillary structure 26. When applicable, in some embodiments the working fluid 36 in liquid form returns from the condenser section 40 through the adiabatic section 42 (FIGURES 2C and 2D) to the evaporator section 38.
Thus, referring back to FIGURES IA, IB, and 2A-2D, it will be appreciated that in some embodiments the assembly shown in FIGURES IA, IB, and 2A-2D can be a heat pipe assembly that includes the heat pipe 16 and the nuclear fission fuel material 12. As described above, the nuclear fission fuel material 12 is integral with the heat pipe 16 and is disposed in thermal communication with the heat pipe 16. That is, the nuclear fission fuel material 12 defines the cavity 18 therein and at least the portion 14 of the heat pipe 16 is disposed within the cavity 18.
Referring now to FIGURES 4A-4D, in some other embodiments a heat pipe assembly 60 includes a heat pipe device 62. The heat pipe device 62 includes a wall section 63. As will be discussed below, nuclear fission fuel material 64 is integral with the heat pipe device 62 and is disposed in thermal communication with the heat pipe device 62. The nuclear fission fuel material 64 suitably is similar to the nuclear fission fuel material 12 (FIGURES IA, IB, and 2A-2D) described above, and details need not be repeated.
Embodiments of the heat pipe assembly 60 share some features in common with the nuclear fission fuel element 10 (FIGURES IA, IB, 2A-2D, 3 A, and 3B). Common reference numbers will be used to refer to common features, and details need not be repeated for an understanding. The heat pipe device 62 defines a cavity 66 therein. A surface 65 of the wall section 63 defines a surface of the cavity 66. In some embodiments, the nuclear fission fuel material 64 is disposed within at least a portion of the cavity 66. For example, referring additionally to FIGURES 5A and 5B, in some embodiments the nuclear fission fuel material 64 may be disposed within the capillary structure 26.
However, it will be appreciated that the nuclear fission fuel material 64 need not be disposed within the capillary structure 26 and may be disposed anywhere whatsoever within the cavity 66 as desired. As another illustrative example given without limitation and referring additionally to FIGURE 5C, in some embodiments the nuclear fission fuel material 64 may be disposed within the cavity 64 on one or more support structures 67 that hold the nuclear fission fuel material 64 in place. Additional capillary structure 26A is disposed about the exterior of the nuclear fission fuel material 64. At least one of the support structures 67 is a liquid transport structure, such as a channel, capillary structure, or the like, that can transport the working fluid in its liquid phase via capillary action between the capillary structure 26A disposed about the exterior of the nuclear fission fuel material 64 and the capillary structure 26 disposed about the surface of the cavity 66.
The heat pipe device 62 includes the evaporator section 38 and the condenser section 40. In some embodiments and as shown in FIGURES 4A and 4C, the nuclear fission fuel material 64 may be disposed entirely or substantially within the evaporator section 38. However, it will be appreciated that the nuclear fission fuel material 64 need not be disposed entirely or substantially within the evaporator section 38. To that end, in some other embodiments and as shown in FIGURES 4B and 4D, at least a portion of the nuclear fission fuel material 64 is not within the evaporator section 38.
In some embodiments, given by way of non-limiting example the nuclear fission fuel material 64 may have a capillary structure. If desired, in some other embodiments the nuclear fission fuel material 64 may have a sintered powdered fuel microstructure, or a foam microstructure, or a high density microstructure, or the like.
The heat pipe device 62 includes the capillary structure 26. In some embodiments, the capillary structure 26 may include the grooves 28 defined in the surface 65 as described above between the lands 30. In some other embodiments, the capillary structure 26 may include the grooves 32 defined in the surface 65 as described above between the lands 30 and 34. In some other embodiments, the capillary structure may include a wick as described above.
The heat pipe assembly 60 also includes the working fluid 36 as described above. Also, in some embodiments, the heat pipe device 62 may include the adiabatic section 42 (FIGURES 4C and 4D).
Referring now to FIGURES 4A-4D, heat from the nuclear fission fuel material 64 is transferred to the evaporator section 40. The working fluid 36 in the evaporator section 38 evaporates, as indicated by arrows 46, thereby undergoing phase transformation from a liquid to a gas. The working fluid 36 in gaseous form moves through the heat pipe device 62, as indicated by arrows 48, from the evaporator section 38, when applicable (in some embodiments) through the adiabatic section 42 (FIGURES 4C and 4D), and to the condenser section 40. At the condenser section 40, heat from the working fluid 36 is transferred out of the heat pipe device 62, as indicated by arrows 50. The working fluid 36 in the condenser section 40 condenses, as indicated by arrows 52, thereby undergoing phase transformation from a gas to a liquid. The working fluid 36 in liquid form returns from the condenser section 40 to the evaporator section 38, as indicated by arrows 54, via capillary action in the capillary structure 26. When applicable, in some embodiments the working fluid 36 in liquid form returns from the condenser section 40 through the adiabatic section 42 (FIGURES 4C and 4D) to the evaporator section 38.
Referring additionally to FIGURE 6, in some other embodiments a heat pipe device 62A has a wall section 63 A that includes at least one layer of structural material 68 and at least one layer of nuclear fission fuel material 64A. As such, the nuclear fission fuel material 64A can be disposed outside of the cavity 66. For sake of brevity and clarity, only one layer of the nuclear fission fuel material 64A and the structural material 68 are shown. However, it will be appreciated that, in some embodiments, any number of layers of the nuclear fission fuel material 64 A and the structural material 68 may be provided as desired. Given by way of non-limiting example, in some embodiments the structural material 68 may include any one or more of materials such as steel, niobium, vanadium, titanium, a refractory metal, and/or a refractory alloy. Given by way of non-limiting example, in some embodiments the refractory metal may be niobium, tantalum, tungsten, hafnium, rhenium, or molybdenum. Non-limiting examples of refractory alloys include, rhenium-tantalum alloys as disclosed in U.S. patent 6902809, tantalum alloy T-111, molybdenum alloy TZM, tungsten alloy MT-185, or niobium alloy Nb-IZr. In some embodiments, a layer of the nuclear fission fuel material 64 A can be disposed entirely or substantially within the evaporator section 38. However, in other embodiments (not shown) one or more layers of the nuclear fission fuel material 64A maybe disposed in at least a portion of the adiabatic section (if provided) and/or the condenser section. Now that illustrative embodiments of nuclear fission fuel elements and heat pipes have been discussed, illustrative methods associated therewith will now be discussed.
Following are a series of flowcharts depicting implementations of processes. For ease of understanding, the flowcharts are organized such that the initial flowcharts present implementations via an overall "big picture" viewpoint and thereafter the following flowcharts present alternate implementations and/or expansions of the "big picture" flowcharts as either sub-steps or additional steps building on one or more earlier-presented flowcharts. Those having skill in the art will appreciate that the style of presentation utilized herein (e.g., beginning with a presentation of a flowchart(s) presenting an overall view and thereafter providing additions to and/or further details in subsequent flowcharts) generally allows for a rapid and easy understanding of the various process implementations. In addition, those skilled in the art will further appreciate that the style of presentation used herein also lends itself well to modular design paradigms. Referring now to FIGURE 7A, an illustrative method 80 is provided for fabricating a nuclear fission fuel element. The method 80 starts at a block 82. At a block 84 nuclear fission fuel material is provided. At a block 86 at least a portion of at least one heat pipe is disposed within the nuclear fission fuel material. The method 80 stops at a block 88. Referring now to FIGURE 7B5 in some embodiments disposing at least a portion of at least one heat pipe within the nuclear fission fuel material at the block 86 may include further processes. For example, at a block 90 a cavity may be defined within at least a portion of the nuclear fission fuel material. Also, at a block 92 a capillary structure may be disposed within at least a portion of the cavity. Further, at a block 94 a working fluid may be disposed within the cavity. Referring now to FIGURE 7C, in some embodiments, defining a cavity within at least a portion of the nuclear fission fuel material at the block 90 can include machining the cavity at a block 96. Given by way of non-limiting example, in some embodiments machining the cavity at the block 96 can be performed by a machining operation such as drilling, milling, stamping, or the like. Referring now to FIGURE 7D, in some other embodiments, defining a cavity within at least a portion of the nuclear fission fuel material at the block 90 can include forming at least a portion of the nuclear fission fuel material around a shape, such as without limitation a mandrel, at a block 98. Given by way of non-limiting example, in some embodiments forming can be performed by an operation such as welding, casting, electroplating, pressing, molding, or the like.
Referring now to FIGURE 7E, in some embodiments disposing a capillary structure within at least a portion of the cavity at the block 92 can include defining a plurality of grooves in a surface of the cavity at a block 100. Given by way of non- limiting example, in some embodiments defining a plurality of grooves in a surface of the cavity at the block 100 can be performed by an operation such as machining, etching, casting, stamping, or the like.
Referring now to FIGURE 7F, in some other embodiments disposing a capillary structure within at least a portion of the cavity at the block 92 can include disposing a wick within at least a portion of the cavity at a block 102. Referring now to FIGURE 7G, in some embodiments, before at least a portion of at least one heat pipe is disposed within the nuclear fission fuel material at the block 86, at a block 104 a size of the cavity can be determined based upon accommodating predetermined power production properties of the nuclear fission fuel element. In one example, the cross-sectional area of the cavity may be chosen by dividing a predetermined power production value of the nuclear fission fuel element by a specified axial heat flux value of the working fluid. Referring now to FIGURE 7H, in some other embodiments, before at least a portion of at least one heat pipe is disposed within the nuclear fission fuel material at the block 86, at a block 106 a size of the cavity can be determined based upon accommodating predetermined heat transfer properties of the working fluid. In one example, the cross-sectional area of the cavity may be chosen in order to achieve a desirable axial heat transport capability from the heat pipe working fluid. In some embodiments, this selection suitably may take into account the operational vapor density of the working fluid, its latent heat of vaporization, and a desirable flow velocity or mach number. In another example, a lateral dimension of the cavity can be chosen in order to provide a desirable Reynold's number for vapor flow.
Referring now to FIGURE 71, in some other embodiments, before at least a portion of at least one heat pipe is disposed within the nuclear fission fuel material at the block 86, at a block 108 a size of the cavity can be determined based upon accommodating volatile fission products. In one example, the cavity volume may be selected based upon the pressure developed by a specified amount of gaseous fission products within the volume. In another example, the cavity volume may be selected based upon the effects of the inertia of a specified amount of gaseous fission products within the volume on the heat transfer properties of the heat pipe.
Referring now to FIGURE 8 A, an illustrative method 110 is provided for fabricating a heat pipe assembly. The method 110 starts at a block 112. At a block 114 a heat pipe device is provided. At a block 116 nuclear fission fuel material is disposed integral with the heat pipe device and in thermal communication with the heat pipe device. The method 110 stops at a block 118.
Referring now to FIGURE 8B, in some embodiments providing a heat pipe device at the block 114 may include further processes. For example, at a block 120 a heat pipe body having a wall section may be provided. At a block 122 a cavity may be defined within at least a portion of the wall section. Also, at a block 124 a capillary structure may be disposed within at least a portion of the cavity. Further, at a block 126 a working fluid may be disposed within the cavity. Referring now to FIGURE 8C, in some embodiments disposing nuclear fission fuel material in thermal communication with the heat pipe device at the block 116 may include disposing nuclear fission fuel material within at least a portion of the wall section at a block 128. Referring now to FIGURE 8D, in some other embodiments disposing nuclear fission fuel material in thermal communication with the heat pipe device at the block 116 may include disposing nuclear fission fuel material within at least a portion of the cavity at a block 130.
Referring now to FIGURE 8E, in some embodiments defining a cavity within the wall section at the block 122 may include machining the cavity. Given by way of non-limiting example, in some embodiments machining the cavity at the block 122 can be performed by a machining operation such as drilling, milling, stamping, or the like.
Referring now to FIGURE 8F, in some other embodiments defining a cavity within at least a portion of the wall section at the block 122 may include forming the at least a portion of the wall section around a shape, such as without limitation a mandrel, at a block 134. Given by way of non-limiting example, in some embodiments forming can be performed by an operation such as welding, casting, electroplating, pressing, molding, or the like.
Referring now to FIGURE 8 G, in some embodiments disposing a capillary structure within at least a portion of the cavity at the block 124 may include defining a plurality of grooves in a surface of the cavity at a block 136. Given by way of non- limiting example, in some embodiments defining a plurality of grooves in a surface of the cavity at the block 136 can be performed by an operation such as machining, etching, casting, stamping, or the like.
Referring now to FIGURE 8H, in some other embodiments disposing a capillary structure within at least a portion of the cavity at the block 124 may include disposing a wick within at least a portion of the cavity at a block 138.
One skilled in the art will recognize that the herein described components (e.g., blocks), devices, and objects and the discussion accompanying them are used as examples for the sake of conceptual clarity and that various configuration modifications are within the skill of those in the art. Consequently, as used herein, the specific exemplars set forth and the accompanying discussion are intended to be representative of their more general classes. In general, use of any specific exemplar herein is also intended to be representative of its class, and the non-inclusion of such specific components (e.g., blocks), devices, and objects herein should not be taken as indicating that limitation is desired.
With respect to the use of substantially any plural and/or singular terms herein, those having skill in the art can translate from the plural to the singular and/or from the singular to the plural as is appropriate to the context and/or application. The various singular/plural permutations are not expressly set forth herein for sake of clarity.
While particular aspects of the present subject matter described herein have been shown and described, it will be apparent to those skilled in the art that, based upon the teachings herein, changes and modifications may be made without departing from the subject matter described herein and its broader aspects and, therefore, the appended claims are to encompass within their scope all such changes and modifications as are within the true spirit and scope of the subject matter described herein. Furthermore, it is to be understood that the invention is defined by the appended claims. It will be understood by those within the art that, in general, terms used herein, and especially in the appended claims (e.g., bodies of the appended claims) are generally intended as "open" terms (e.g., the term "including" should be interpreted as "including but not limited to," the term "having" should be interpreted as "having at least," the term "includes" should be interpreted as "includes but is not limited to," etc.). It will be further understood by those within the art that if a specific number of an introduced claim recitation is intended, such an intent will be explicitly recited in the claim, and in the absence of such recitation no such intent is present. For example, as an aid to understanding, the following appended claims may contain usage of the introductory phrases "at least one" and "one or more" to introduce claim recitations. However, the use of such phrases should not be construed to imply that the introduction of a claim recitation by the indefinite articles "a" or "an" limits any particular claim containing such introduced claim recitation to inventions containing only one such recitation, even when the same claim includes the introductory phrases "one or more" or "at least one" and indefinite articles such as "a" or "an" (e.g., "a" and/or "an" should typically be interpreted to mean "at least one" or "one or more"); the same holds true for the use of definite articles used to introduce claim recitations. In addition, even if a specific number of an introduced claim recitation is explicitly recited, those skilled in the art will recognize that such recitation should typically be interpreted to mean at least the recited number (e.g., the bare recitation of "two recitations," without other modifiers, typically means at least two recitations, or two or more recitations). Furthermore, in those instances where a convention analogous to "at least one of A, B, and C, etc." is used, in general such a construction is intended in the sense one having skill in the art would understand the convention (e.g., " a system having at least one of A, B, and C" would include but not be limited to systems that have A alone, B alone, C alone, A and B together, A and C together, B and C together, and/or A, B, and C together, etc.). In those instances where a convention analogous to "at least one of A, B, or C, etc." is used, in general such a construction is intended in the sense one having skill in the art would understand the convention (e.g., " a system having at least one of A, B, or C" would include but not be limited to systems that have A alone, B alone, C alone, A and B together, A and C together, B and C together, and/or A, B, and C together, etc.). It will be further understood by those within the art that virtually any disjunctive word and/or phrase presenting two or more alternative terms, whether in the description, claims, or drawings, should be understood to contemplate the possibilities of including one of the terms, either of the terms, or both terms. For example, the phrase "A or B" will be understood to include the possibilities of "A" or "B" or "A and B."
With respect to the appended claims, those skilled in the art will appreciate that recited operations therein may generally be performed in any order. Examples of such alternate orderings may include overlapping, interleaved, interrupted, reordered, incremental, preparatory, supplemental, simultaneous, reverse, or other variant orderings, unless context dictates otherwise. With respect to context, even terms like "responsive to," "related to," or other past-tense adjectives are generally not intended to exclude such variants, unless context dictates otherwise.
While various aspects and embodiments have been disclosed herein, other aspects and embodiments will be apparent to those skilled in the art. The various aspects and embodiments disclosed herein are for purposes of illustration and are not intended to be limiting, with the true scope and spirit being indicated by the following claims.
What is claimed is:

Claims

1. A nuclear fission fuel element comprising:
nuclear fission fuel material; and
at least one heat pipe, at least a portion of which is disposed within the nuclear fission fuel material.
2. The nuclear fission fuel element of Claim 1 , wherein the nuclear fission fuel material includes at least one material chosen from fissile material and fertile material.
3. The nuclear fission fuel element of Claim 2, wherein the fissile material includes at least one fissile material chosen from 233U, 235U, and 239Pu.
4. The nuclear fission fuel element of Claim 2, wherein the fertile material includes at least one fertile material chosen from 232Th and 238U.
5. The nuclear fission fuel element of Claim 1 , wherein:
the nuclear fission fuel material defines a cavity therein; and
the heat pipe includes a capillary structure defined within at least a portion of the cavity.
6. The nuclear fission fuel element of Claim 5, wherein the cavity includes a passageway defined through at least a portion of the nuclear fission fuel material.
7. The nuclear fission fuel element of Claim 6, wherein the passageway includes walls that substantially surround a portion of the capillary structure.
8. The nuclear fission fuel element of Claim 5, wherein, wherein the cavity is substantially sealed.
9. The nuclear fission fuel element of Claim 5, wherein a surface of the cavity defines a plurality of grooves therein, the plurality of grooves defining the capillary structure.
10. The nuclear fission fuel element of Claim 5, wherein the capillary structure includes a wick.
11. The nuclear fission fuel element of Claim 10, wherein the wick is made of material chosen from thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
12. The nuclear fission fuel element of Claim 5, further comprising a working fluid disposed within the cavity.
13. The nuclear fission fuel element of Claim 12, wherein the working fluid is evaporable and condensable.
14. The nuclear fission fuel element of Claim 13, wherein the working fluid includes a fluid chosen from 7Li, sodium, and potassium.
15. The nuclear fission fuel element of Claim 1 , wherein the heat pipe includes an evaporator section and a condenser section.
16. The nuclear fission fuel element of Claim 15, wherein the heat pipe further includes an adiabatic section.
17. The nuclear fission fuel element of Claim 15, wherein at least a portion of the condenser section is not within the nuclear fission fuel material.
18. The nuclear fission fuel element of Claim 15, wherein at least a portion of the evaporator section is not within the nuclear fission fuel material.
19. The nuclear fission fuel element of Claim 16, wherein at least a portion of the adiabatic section is not within the nuclear fission fuel material.
20. A heat pipe assembly comprising:
a heat pipe device; and
nuclear fission fuel material integral with the heat pipe device and disposed in thermal communication with the heat pipe device.
21. The heat pipe assembly of Claim 20, wherein:
the nuclear fission fuel material defines a cavity therein; and
at least a portion of the heat pipe device is disposed within the cavity.
22. The heat pipe assembly of Claim 21 , wherein the cavity includes a passageway defined through at least a portion of the nuclear fission fuel material.
23. The heat pipe assembly of Claim 22, wherein the passageway includes walls that substantially surround a portion of the capillary structure.
24. The heat pipe assembly of Claim 21 , wherein, wherein the cavity is substantially sealed.
25. The heat pipe assembly of Claim 20, wherein:
the heat pipe device defines a cavity therein; and
the nuclear fission fuel material is disposed within at least a portion of the cavity.
26. The heat pipe assembly of Claim 25, wherein the nuclear fission fαel material includes a microstructure chosen from sintered powdered fuel microstructure, a foam microstructure, and a high density microstructure.
27. The heat pipe assembly of Claim 25, wherein the nuclear fission fuel material includes a capillary structure.
28. The heat pipe assembly of Claim 20, wherein the heat pipe device includes a capillary structure.
29. The heat pipe assembly of Claim 28, a plurality of grooves defines the capillary structure.
30. The heat pipe assembly of Claim 28, wherein the capillary structure includes a wick.
31. The heat pipe assembly of Claim 30, wherein the wick is made of material chosen from thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
32. The heat pipe assembly of Claim 28, further comprising a working fluid disposed within the heat pipe device.
33. The heat pipe assembly of Claim 32, wherein the working fluid is evaporable and condensable.
34. The heat pipe assembly of Claim 33, wherein the working fluid includes a fluid chosen from 7Li, sodium, and potassium.
35. The heat pipe assembly of Claim 20, wherein the heat pipe device includes an evaporator section and a condenser section.
36. The heat pipe assembly of Claim 35, wherein the heat pipe device further includes an adiabatic section.
37. The heat pipe assembly of Claim 20, wherein the nuclear fission fuel material includes at least one material chosen from fissile material and fertile material.
38. The heat pipe assembly of Claim 37, wherein the fissile material includes at least one fissile material chosen from 233U, 235U, and 239Pu.
39. The heat pipe assembly of Claim 37, wherein the fertile material includes at least one fertile material chosen from 232Th and 238U.
40. A nuclear fission fuel element comprising:
nuclear fission fuel material defining a cavity therein;
a capillary structure disposed within at least a portion of the cavity; and
a working fluid disposed within the cavity.
41. The nuclear fission fuel element of Claim 40, wherein the cavity includes a passageway defined through at least a portion of the nuclear fission fuel material.
42. The nuclear fission fuel element of Claim 41 , wherein the passageway includes walls that substantially surround a portion of the capillary structure.
43. The nuclear fission fuel element of Claim 40, wherein, wherein the cavity is substantially sealed.
44. The nuclear fission fuel element of Claim 40, wherein the nuclear fission fuel material includes at least one material chosen from fissile material and fertile material.
45. The nuclear fission fuel element of Claim 44, wherein the fissile material includes at least one fissile material chosen from 233U, 235U, and 239Pu.
46. The nuclear fission fuel element of Claim 44, wherein the fertile material includes at least one fertile material chosen from 232Th and 238U.
47. The nuclear fission fuel element of Claim 40, wherein wall surfaces of the cavity define wall surfaces of a heat pipe.
48. The nuclear fission fuel element of Claim 47, wherein the wall surfaces define a plurality of grooves therein, the plurality of grooves defining the capillary structure.
49. The nuclear fission fuel element of Claim 40, wherein the capillary structure includes a wick.
50. The nuclear fission fuel element of Claim 49, wherein the wick is made of a material chosen from thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
51. The nuclear fission fuel element of Claim 40, wherein the working fluid is evaporable and condensable.
52. The nuclear fission fuel element of Claim 51 , wherein the working fluid includes a fluid chosen from 7Li, sodium, and potassium.
53. The nuclear fission fuel element of Claim 47, wherein the heat pipe includes an evaporator section and a condenser section.
54. The nuclear fission fuel element of Claim 53, wherein the heat pipe further includes an adiabatic section.
55. The nuclear fission fuel element of Claim 53, wherein at least a portion of the condenser section is not within the nuclear fission fuel material.
56. The nuclear fission fuel element of Claim 53, wherein at least a portion of the evaporator section is not within the nuclear fission fuel material.
7. The nuclear fission fuel element of Claim 54, wherein at least a portion of the adiabatic section is not within the nuclear fission fuel material.
58. A heat pipe comprising:
a wall section defining a cavity therein, the wall section including at least one portion including nuclear fission fuel material;
a capillary structure disposed within at least a portion of the cavity; and
a working fluid disposed within the cavity.
59. The heat pipe of Claim 58, wherein the heat pipe includes an evaporator section and a condenser section.
60. The heat pipe of Claim 59, wherein the heat pipe further includes an adiabatic section.
61. The heat pipe of Claim 59, wherein a portion of the wall section defining at least a portion of the condenser section does not include nuclear fission fuel material.
62. The heat pipe of Claim 59, wherein a portion of the wall section defining at least a portion of the evaporator section includes nuclear fission fuel material.
63. The heat pipe of Claim 60, wherein a portion of the wall section defining at least a portion of the adiabatic section does not include nuclear fission fuel material.
64. The heat pipe of Claim 58, wherein the wall section includes at least one layer including structural material and at least one other layer including nuclear fission fuel material.
65. The heat pipe of Claim 64, wherein the structural material includes a material chosen from steel, niobium, vanadium, titanium, a refractory metal, and a refractory alloy.
66. The heat pipe of Claim 58, wherein the nuclear fission fuel material includes at least one material chosen from fissile material and fertile material.
67. The heat pipe of Claim 66, wherein the fissile material includes at least one fissile material chosen from 233U, 235U, and 239Pu.
68. The heat pipe of Claim 66, wherein the fertile material includes at least one fertile material chosen from 232Th and 238U.
69. The heat pipe of Claim 58, wherein a surface of the cavity defines a plurality of grooves therein, the plurality of grooves defining the capillary structure.
70. The heat pipe of Claim 58, wherein the capillary structure includes a wick.
71. The heat pipe of Claim 70, wherein the wick is made of a material chosen from thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
72. The heat pipe of Claim 58, wherein the working fluid is evaporable and condensable.
73. The heat pipe of Claim 72, wherein the working fluid includes a fluid chosen from 7Li, sodium, and potassium.
74. A heat pipe comprising:
a wall section defining a cavity therein;
a capillary structure disposed within at least a portion of the cavity;
a working fluid disposed within the cavity; and
nuclear fission fuel material disposed within at least a portion of the cavity.
75. The heat pipe of Claim 74, wherein the heat pipe includes an evaporator section and a condenser section.
76. The heat pipe of Claim 75, wherein the heat pipe further includes an adiabatic section.
77. The heat pipe of Claim 75, wherein a portion of the cavity defining at least a portion of the condenser section does not include nuclear fission fuel material.
78. The heat pipe of Claim 75, wherein a portion of the cavity defining at least a portion of the evaporator section includes nuclear fission fuel material.
79. The heat pipe of Claim 76, wherein a portion of the cavity defining at least a portion of the adiabatic section does not include nuclear fission fuel material.
80. The heat pipe of Claim 74, wherein the nuclear fission fuel material includes a microstructure chosen from sintered powdered fuel microstructure, a foam microstructure, and a high density microstructure.
81. The heat pipe of Claim 74, wherein the nuclear fission fuel material includes a capillary structure.
82. The heat pipe of Claim 74, wherein the nuclear fission fuel material includes at least one material chosen from fissile material and fertile material.
83. The heat pipe of Claim 82, wherein the fissile material includes at least one fissile material chosen from 233U, 235U, and 239Pu.
84. The heat pipe of Claim 82, wherein the fertile material includes at least one fertile material chosen from Th and 238U.
85. The heat pipe of Claim 74, wherein a surface of the cavity defines a plurality of grooves therein, the plurality of grooves defining the capillary structure.
86. The heat pipe of Claim 74, wherein the capillary structure includes a wick.
87. The heat pipe of Claim 86, wherein the wick is made of a material chosen from thorium, molybdenum, tungsten, steel, tantalum, zirconium, carbon, and a refractory metal.
88. The heat pipe of Claim 74, wherein the working fluid is evaporable and condensable.
89. The heat pipe of Claim 88, wherein the working fluid includes a fluid chosen from 7Li, sodium, and potassium.
90. A method of fabricating a nuclear fission fuel element, the method comprising:
providing nuclear fission fuel material; and
disposing at least a portion of at least one heat pipe within the nuclear fission fuel material.
91. The method of Claim 90, wherein disposing at least a portion of at least one heat pipe within the nuclear fission fuel material includes:
defining a cavity within at least a portion of the nuclear fission fuel material;
disposing a capillary structure within at least a portion of the cavity; and
disposing a working fluid within the cavity.
92. The method of Claim 91 , wherein defining a cavity within at least a portion of the nuclear fission fuel material includes defining a passageway through at least a portion of the nuclear fission fuel material.
93. The method of Claim 91 , wherein defining a cavity within at least a portion of the nuclear fission fuel material includes machining the cavity.
94. The method of Claim 93, wherein machining includes performing a machining operation chosen from drilling, milling, and stamping.
95. The method of Claim 91 , wherein defining a cavity within at least a portion of the nuclear fission fuel material includes forming the at least a portion of the nuclear fission fuel material around a shape.
96. The method of Claim 95, wherein the shape includes a mandrel.
97. The method of Claim 95, wherein forming includes an operation chosen from welding, casting, electroplating, pressing, and molding.
98. The method of Claim 91 , wherein disposing a capillary structure within at least a portion of the cavity includes defining a plurality of grooves in a surface of the cavity.
99. The method of Claim 98, wherein defining includes performing an operation chosen from machining, etching, casting, and stamping.
100. The method of Claim 91 , wherein disposing a capillary structure within at least a portion of the cavity includes disposing a wick within at least a portion of the cavity.
101. The method of Claim 91 , further comprising determining a size of the cavity based upon accommodating predetermined power production properties of the nuclear fission fuel element.
102. The method of Claim 91 , further comprising determining a size of the cavity based upon accommodating predetermined heat transfer properties of the working fluid.
103. The method of Claim 91 , further comprising determining a size of the cavity based upon accommodating volatile fission products.
104. A method of fabricating a heat pipe assembly, the method comprising:
providing a heat pipe device; and
disposing nuclear fission fuel material integral with the heat pipe device and in thermal communication with the heat pipe device.
105. The method of Claim 104, wherein providing a heat pipe device includes:
providing a heat pipe body having a wall section;
defining a cavity within at least a portion of the wall section;
disposing a capillary structure within at least a portion of the cavity; and
disposing a working fluid within the cavity.
106. The method of Claim 105, wherein disposing nuclear fission fuel material in thermal communication with the heat pipe device includes disposing nuclear fission fuel material within at least a portion of the wall section.
107. The method of Claim 105, wherein disposing nuclear fission fuel material in thermal communication with the heat pipe device includes disposing nuclear fission fuel material within at least a portion of the cavity.
108. The method of Claim 105, wherein defining a cavity within the wall section includes machining the cavity.
109. The method of Claim 108, wherein machining includes performing a machining operation chosen from drilling, milling, and stamping.
1 10. The method of Claim 105, wherein defining a cavity within at least a portion of the wall section includes forming the at least a portion of the wall section around a shape.
11 1. The method of Claim 110, wherein the shape includes a mandrel.
112. The method of Claim 111, wherein forming includes an operation chosen from welding, casting, electroplating, pressing, and molding.
113. The method of Claim 105, wherein disposing a capillary structure within at least a portion of the cavity includes defining a plurality of grooves in a surface of the cavity.
114. The method of Claim 113, wherein defining includes performing an operation chosen from machining, etching, casting, and stamping.
115. The method of Claim 105, wherein disposing a capillary structure within at least a portion of the cavity includes disposing a wick within at least a portion of the cavity.
PCT/US2009/003028 2008-05-15 2009-05-15 Heat pipe fission fuel element WO2009139899A1 (en)

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EP2291850A1 (en) 2011-03-09
CN102067241A (en) 2011-05-18
US20090285348A1 (en) 2009-11-19
EP2291850A4 (en) 2012-03-28
CN102067241B (en) 2015-11-25
KR101568448B1 (en) 2015-11-11
JP2011523045A (en) 2011-08-04
KR20110013486A (en) 2011-02-09
EP2291850B1 (en) 2014-12-17
RU2010147880A (en) 2012-06-20

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