System and method for radioactive waste destruction

Information

  • Patent Grant
  • 6738446
  • Patent Number
    6,738,446
  • Date Filed
    Friday, October 25, 2002
    22 years ago
  • Date Issued
    Tuesday, May 18, 2004
    20 years ago
Abstract
A method for transmuting spent fuel from a nuclear reactor includes the step of separating the waste into components including a driver fuel component and a transmutation fuel component. The driver fuel, which includes fissile materials such as Plutonium239, is used to initiate a critical, fission reaction in a reactor. The transmutation fuel, which includes non-fissile transuranic isotopes, is transmuted by thermal neutrons generated during fission of the driver fuel. The system is designed to promote fission of the driver fuel and reduce neutron capture by the driver fuel. Reacted driver fuel is separated into transuranics and fission products using a dry cleanup process and the resulting transuranics are mixed with transmutation fuel and re-introduced into the reactor. Transmutation fuel from the reactor is introduced into a second reactor for further transmutation by neutrons generated using a proton beam and spallation target.
Description




FIELD OF THE INVENTION




The present invention pertains generally to systems and methods for the destruction of high-level radioactive waste. More particularly, the present invention pertains to methods for converting the spent fuel from a nuclear reactor into a form which is suitable for long term storage at a repository. The present invention is particularly, but not exclusively, useful for transmuting Plutonium


239


and other transuranics found in spent nuclear fuel into more stable, less radiotoxic materials.




BACKGROUND OF THE INVENTION




It is well known that spent nuclear fuel is highly radiotoxic and poses several challenging threats to mankind, including nuclear proliferation, radiation exposure and environmental contamination. To date, approximately 90,000 spent fuel assemblies containing about 25,000 tons of spent radioactive fuel are stored in the United States. Furthermore, with additional spent fuel assemblies being generated each year, it is estimated there will be about 70,000 tons of spent fuel waste by the year 2015. At the rate waste is produced by the existing nuclear reactors in the United States, new repository capacity would be needed every 20-30 years equal to the statutory capacity of the yet-to-open Geological Repository at Yucca Mountain. Currently, about 95% of this radiotoxic material is temporarily stored at the point of generation (i.e. at the power plant) in water pools, with a small amount being stored in dry storage (casks).




A typical spent fuel assembly removed from a commercial nuclear power plant, such as a Light Water Reactor, contains four major constituents: Uranium (about 95%), fissile transuranics including Plutonium


239


(0.9%), non-fissile transuranics including certain isotopes of Americium, Plutonium, Curium and Neptunium (0.1%), and fission products (balance). After a relatively short time, the Uranium and a portion of the fission products are generally no more radiotoxic than natural Uranium ore. Consequently, these components of the spent fuel do not require transmutation or special disposal. The remaining fission products can be used as a burnable poison in a commercial reactor followed by disposal at a repository.




The fissile and non-fissile transuranics, however, require special isolation from the environment or transmutation to non-fissile, shorter lived forms. Destroying at least 95% of these transuranics followed by disposal in advanced containers (i.e. containers better than simple steel containers) represents a much better solution than merely stockpiling the waste in the form of fuel rods. In one transmutation scheme, the transuranics are transmuted in a reactor, followed by a separation step to concentrate the remaining transuranics, followed by further transmutation. Unfortunately, this cycle must be repeated 10-20 times to achieve a desirable destruction level of 95%, and consequently, is very time consuming and expensive.




In another transmutation scheme, fast neutrons are used to transmute the non-fissile transuranics. For example, fast neutrons generated by bombarding a spallation target with protons are used. Although these fast spectrum systems generate a large number of neutrons, many of the neutrons are wasted, especially in subcritical systems. Further, these fast neutrons can cause serious damage to fuel and structures, limiting the useful life of the transmutation devices.




In light of the above, it is an object of the present invention to provide devices suitable for transmuting fissile and non-fissile transuranics to achieve relatively high destruction levels without requiring multiple reprocessing steps. It is another object of the present invention to provide systems and methods for efficiently transmuting fissile and non-fissile transuranics with thermal neutrons. It is yet another object of the present invention to provide systems and methods for efficiently transmuting fissile and non-fissile transuranics which use neutrons released during the fission of fissile transuranics to transmute the non-fissile transuranics.




SUMMARY OF THE INVENTION




In accordance with the present invention, a system and method for transmuting spent fuel (i.e. radioactive waste) from a nuclear reactor, such as a Light Water Reactor, includes the step of separating the waste into components. For the present invention, a conventional UREX process can be used to separate the spent fuel into components that include a Uranium component, a fission products component, a driver fuel component and a transmutation fuel component. After the separation, the driver fuel and transmutation fuel components are placed in a reactor with a thermal neutron spectrum for transmutation into less hazardous materials. On the other hand, the Uranium component is relatively non-radioactive and can be disposed of without transmutation. Also, the fission products may be transmuted into short-lived, non-toxic forms in commercial thermal reactors.




The driver fuel, which includes fissile materials such as Plutonium


239


, is used to initiate a critical, self-sustaining, thermal-neutron fission reaction in the first reactor. The transmutation fuel, which includes non-fissile materials, such as certain isotopes of Americium, Plutonium, Neptunium and Curium, is transmuted by the neutrons released during fission of the driver fuel. The transmutation fuel also provides stable reactivity feedback and makes an important contribution to ensure that the reactor is passively safe. The system is designed to promote fission of the driver fuel and reduce excessive neutron capture by the driver fuel. More specifically, the system is designed to minimize exposure of the driver fuel to thermal neutrons within an energy band wherein the driver fuel has a relatively high neutron capture cross-section and a relatively low fission cross-section. In one implementation, the driver fuel is formed into spherical particles having a relatively large diameter (e.g. approximately 300 μm) to minimize neutron capture by the so called self-shielding effect.




The transmutation fuel is formed into relatively small, substantially spherical particles having a diameter of approximately 150 μm in diameter (or diluted 250 μm particles) to maximize exposure of the small amount of the transmutation fuel to epithermal neutrons (i.e. thermal neutrons at the high energy end of the thermal neutron energy spectrum). These neutrons interact with the transmutation fuel atoms in the so-called resonance epithermal region and destroy them in a capture-followed-by-fission sequence. Additionally, the particles are placed in graphite blocks which moderate neutrons from the fission reaction. A relatively high ratio of graphite mass to driver fuel mass is used in the first reactor to slow down neutrons to the desired energy levels that promote fission over capture in the driver fuel.




The driver fuel and transmutation fuel remain in the first reactor for approximately three years, with one third of the reacted driver fuel and transmutation fuel removed each year and replaced with fresh fuel. Upon removal from the first reactor, the reacted driver fuel consists of approximately one-third transuranics and two-thirds fission products. The transuranics in the reacted driver fuel are then separated from the fission products using a baking process to heat up and evaporate volatile elements. The resulting fission products can be sent to a repository and the transuranics left over can be mixed with transmutation fuel from the UREX separation and re-introduced into the first reactor for further transmutation.




Transmutation fuel that has been removed from the first reactor after a three year residence time is then introduced into a second reactor for further transmutation. The second reactor includes a sealable, cylindrical housing having a window to allow a beam of protons to pass through the window and into the housing. A spallation target is positioned inside the housing and along the proton beam path. Fast neutrons are thereby released when the beam of protons enters the housing and strikes the spallation target.




Graphite blocks containing the transmutation fuel are positioned inside the housing at a distance from the spallation target. A relatively low ratio of graphite mass to transmutation fuel mass is used in the second reactor to allow epithermal neutrons to reach the transmutation fuel. However, enough graphite is used to achieve the desired moderation for transmutation, with the attendant effect that fast neutron damage to reactor structures and equipment is limited. After a residence time in the second reactor of approximately four years, the reacted transmutation fuel is removed from the second reactor and sent directly to a repository. The spherical particles of transmutation fuel are coated with an impervious, ceramic material which provides for long-term containment of the reacted transmutation fuel in the repository.











BRIEF DESCRIPTION OF THE DRAWINGS




The novel features of this invention, as well as the invention itself, both as to its structure and its operation, will be best understood from the accompanying drawings, taken in conjunction with the accompanying description, in which similar reference characters refer to similar parts, and in which:





FIG. 1

is a functional block diagram of a method for treating spent fuel from a Light Water Reactor;





FIG. 2

is a sectional view through the center of a coated driver particle;





FIG. 3

is a sectional view through the center of a coated transmutation particle;





FIG. 4

is a process diagram for fabricating fuel elements;





FIG. 5

is a sectional view of a fuel element as seen along line


5





5


in

FIG. 4

;





FIG. 6

is a Modular Helium Reactor (MHR) for hosting a critical, self-sustaining fission reaction;





FIG. 7

is a sectional view as seen along line


7





7


in

FIG. 6

;





FIG. 8

is a graph showing the net neutron production from 95% destruction of 100 atoms of transuranic waste as a function of neutron energy;





FIG. 9

is a Modular Helium Reactor (MHR) for hosting a subcritical, accelerator driven, transmutation reaction; and





FIG. 10

is a sectional view as seen along line


10





10


in FIG.


9


.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




Referring initially to

FIG. 1

, a method


11


is shown for treating a spent fuel


12


, such as the spent fuel assemblies from a Light Water Reactor (LWR), to achieve a high level of destruction of transuranic elements in the spent fuel


12


via transmutation with thermal neutrons. As shown, a conventional UREX process


14


can be used to separate the spent fuel


12


into components that include a Uranium component


16


, a fission products component


18


, a driver fuel component


20


and a transmutation fuel component


22


. In greater detail, the Uranium component


16


, which constitutes approximately 95% of the spent fuel


12


, is relatively non-radioactive and can be disposed of without transmutation.




As further shown in

FIG. 1

, the fission products component


18


, which constitutes approximately 4% of the spent fuel


12


, includes toxic fission products


24


, such as technicium


+


(constituting approximately 0.1% of the spent fuel


12


) which can be irradiated (see box


26


) to produce Ruthenium


28


, which can then be packaged (box


30


) and sent to a repository


32


. If desired, the irradiation step (box


26


) can be accomplished by using the technicium


+


as a burnable poison in a commercial reactor. As further shown, other fission products including Iodine


34


(which constitute approximately 3.9% of the spent fuel


12


) can be packaged (box


30


) and sent to repository


32


.




Continuing with

FIG. 1

, it can be seen that after the UREX process


14


, the driver fuel component


20


, which constitutes approximately 0.9% of the spent fuel


12


and includes fissile isotopes, such as Plutonium


239


and Neptunium


237


, is fabricated into coated driver particles (box


36


) and then used to initiate a critical, self-sustaining, thermal-neutron fission reaction in the first reactor


38


. Typically, the driver fuel component


20


is approximately 95% Plutonium and 5% Neptunium. Similarly, the transmutation fuel component, which constitutes approximately 0.1% of the spent fuel


12


and includes non-fissile materials, such as Americium, Curium and certain isotopes of Pu and Neptunium coming from the driver fuel, is fabricated into coated transmutation particles (box


40


) and introduced into the first reactor


38


for transmutation with neutrons generated during fission of the driver fuel component


20


. Typically, the transmutation fuel component


22


is approximately 42% Plutonium, 39% Americium, 16% Curium and 3% Neptunium. The transmutation fuel component


22


also provides stable reactivity feedback to control the nuclear reactor.




Referring now to

FIG. 2

, a coated driver particle is shown and generally designated


42


. As shown, the coated driver particle


42


has a driver fuel kernel


44


having a kernel diameter d


1


, that is fabricated from the driver fuel component


20


. As further shown, the driver fuel kernel


44


is coated with a coating having a buffer layer


46


, which can be a porous carbon layer. Functionally, the buffer layer


46


attenuates fission recoils and accommodates kernel swelling. Further, the pores provide a void volume for fission gases. The coating also includes an inner pyrocarbon layer


48


, a silicon carbide (SiC) layer


50


and an outer pyrocarbon layer


52


. The inner pyrocarbon layer


48


provides support for the silicon carbide layer


50


during irradiation, prevents the attachment of CI to driver fuel kernel


44


during manufacture, provides protection for SiC from fission products and CO, and retains gaseous fission products. The silicon carbide layer


50


constitutes the primary load bearing member and retains gas and metal fission products during long term storage. The outer pyrocarbon layer


52


, provides structural support for the silicon carbide layer


50


, provides a bonding surface for compacting, and provides a fission product barrier in particles having a defective silicon carbide layer


50


.




As shown in

FIG. 3

, a coated transmutation particle is shown and generally designated


54


. As shown, the coated transmutation particle


54


has a transmutation fuel kernel


56


having a kernel diameter d


2


, that is fabricated from the transmutation fuel component


22


. As further shown, the transmutation fuel kernel


56


is coated with a coating having a buffer layer


58


, inner pyrocarbon layer


60


, a silicon carbide layer


62


and an outer pyrocarbon layer


64


. These layers are similar to corresponding layers for the coated driver particle


42


described above (i.e. buffer layer


46


, inner pyrocarbon layer


48


, silicon carbide layer


50


and outer pyrocarbon layer


52


) in composition and function.





FIG. 4

illustrates a manufacturing process for fabricating coated driver particles


42


and coated transmutation particles


54


. In greater detail, for fabrication of coated driver particles


42


, a concentrated Pu nitrate solution (e.g. 600-1100 g Pu/I) is first prepared as a broth by adding H


2


O and NH


3


to neutralize free nitric acid. Urea is added and the solution chilled to 10° C. at which point Hexamethylene-tetra-amine (HMTA) is added to form the broth


66


having a concentration of approximately 240-260 g Pu/I. Liquid droplets are generated by pulsing the broth


66


through needle orifices at drop column


68


and the droplets are gelled (creating gelled spheres


70


) by heating the droplets in a bath at 80° C. to release NH


3


from the decomposition of HMTA and cause gelation.




Continuing with

FIG. 4

, after gelation, wash columns


72




a,b


are used to wash the gelled spheres


70


in dilute NH


4


OH to stabilize structure and remove residual reaction products and organics. From wash column


72




b


, rotary dryer


74


is used to dry the spheres in saturated air at 200° C. Next, the spheres are calcinated in a calcinating furnace


76


using dry air at 750° C. From the calcinating furnace


76


, the spheres are sintered in pure H


2


at 1500-1600° C. in sintering furnace


78


. A table


80


and screen


82


are used to discard unacceptable spheres. In one implementation, non-sphericity (i.e. the ratio of maximum to minimum diameter) is controlled to be less than 1.05. Acceptable spheres constitute the driver fuel kernels


44


which are then coated using fluidized bed coaters


84


,


86


,


88


.




Cross-referencing

FIGS. 2 and 4

, it can be seen that fluidized bed coater


84


using hydrocarbon gas can be used to deposit the inner pyrocarbon layer


48


. Similarly, fluidized bed coater


86


using methyltrichlorosilane can be used to deposit the silicon carbide layer


50


, and fluidized bed coater


88


using hydrocarbon gas can be used to deposit the outer pyrocarbon layer


52


. The coatings may also be applied in a continuous process using only one coater. Table


90


, screen


92


and elutriation columns


94


are used to separate coated driver particles


42


of acceptable size, density and shape. Acceptable coated driver particles


42


are then used to prepare cylindrical driver fuel compacts


96


. In greater detail, the coated driver particles


42


are placed in a compact press


98


with a thermoplastic or thermosetting matrix material wherein the combination is pressed into cylinders. The cylinders are then placed in a carburizing furnace


100


, followed by a heat treatment furnace


102


to produce the driver fuel compacts


96


. Compacts may also be treated with dry hydrochloric acid gas between carburizing furnace


100


and heat treatment furnace


102


to remove transuranics and other impurities from the compacts.




Continuing with

FIG. 4

, it can be seen that the driver fuel compacts


96


can then be placed in graphite blocks


104


to prepare fuel elements


106


. With cross-reference to

FIGS. 4 and 5

, it can be seen that cylindrical holes


108


are machined in hexagonally shaped graphite blocks


104


to contain the cylindrical shaped fuel compacts


96


. As best seen in

FIG. 5

, an exemplary fuel element


106


is shown having one-hundred-forty-four holes containing driver fuel compacts


96


that are uniformly distributed across the fuel element


106


. Further, the exemplary fuel element


106


includes seventy-two holes for containing transmutation fuel compacts


110


uniformly distributed across the fuel element


106


, and one-hundred-and-eight coolant channels


112


for passing a coolant such as Helium through the fuel element


106


. It is to be appreciated that other similar hole configurations can be used in the fuel elements


106


. It is to be appreciated by skilled artisans that the transmutation fuel compacts


110


can be prepared in a manner similar to the above described manufacturing process for preparing driver fuel compacts


96


.




A plurality of fuel elements


106


containing driver fuel compacts


96


and transmutation fuel compacts


110


are then placed in first reactor


38


as shown in

FIG. 1

for transmutation. As used herein, the term transmutation and derivatives thereof is herein intended to mean any process(es) which modify the nucleus of an atom such that the product nucleus has either a different mass number or a different atomic number than the reactant nucleus, and includes but is not limited to the fission, capture and decay processes. For example, non-fissile isotopes in the transmutation fuel component can generally be destroyed with thermal neutrons by first transmuting via one or more capture and/or decay processes to a fissile isotope, followed by fission.




Referring now to

FIG. 6

, an exemplary first reactor


38


is shown. For the method


11


, a Modular Helium Reactor (MHR) can be used as the first reactor


38


. In an MHR, Helium is circulated through the reactor vessel to regulate temperature and extract heat from the vessel. The extracted heat can then be used, for example, to produce electricity. The use of Helium as a coolant is advantageous because of Helium's transparency to neutrons. Additionally, Helium is chemically inert, and consequently, nuclear and chemical coolant-fuel interactions are minimized. Further, the Helium remains in the gaseous state providing reliable cooling that is easy to calculate and predict.




Referring now to

FIG. 7

, it can be seen that fuel elements


106


are arranged in the first reactor


38


in a substantially annular arrangement surrounding a central reflector


114


. More specifically, as shown the fuel elements


106


are arranged in three substantially annular rings


116


,


118


,


120


, with each ring


116


,


118


,


120


containing thirty-six columns of fuel elements


106


with each column having a stack of ten fuel elements


106


.




A sufficient quantity of fissile material is included in the reactor


38


to initiate a self-sustaining critical, fission reaction. For the method


11


, materials in the first reactor


38


are configured to promote fission of the driver fuel component


20


(See

FIG. 1

) and reduce neutron capture by the driver fuel component


20


. More specifically, the first reactor


38


is configured to minimize any exposure of the driver fuel component


20


to thermal neutrons within an energy band wherein the Pu


239


in the driver fuel component


20


has a relatively high neutron capture cross-section and a relatively low fission cross-section. As best seen in

FIG. 8

, this energy band extends from approximately 0.2 eV to approximately 1.0 eV.




In one implementation of the method


11


, materials in the reactor


38


are configured to maximize exposure of the driver fuel component


20


to thermal neutrons within an energy band extending from approximately 0.1 eV to approximately 0.2 eV. To achieve this, the driver fuel component


20


is formed into spherical particles having a relatively large driver fuel kernel diameter, d


1


, (see

FIG. 2

) that is between approximately 270 μm and approximately 320 μm) to minimize neutron capture. Neutrons in the problematic energy band (i.e. neutrons between approximately 0.2 eV to approximately 1.0 eV) are limited to the surface of the relatively large driver fuel kernel


44


, leaving the remainder of the relatively large driver fuel kernel


44


available for fission with neutrons having energies in the range of approximately 0.1 eV to approximately 0.2 eV.




Continuing with

FIG. 7

, it can be seen that the fuel elements


106


(which include graphite blocks


104


shown in

FIG. 5

) are placed in annular arrangement interposed between a central reflector


114


and an outer reflector


122


. The graphite moderates fast neutrons from the fission reaction. Functionally, the graphite decreases fast neutron damage to fuel, reactor structures and equipment. A relatively high ratio (i.e. greater than 100:1) of graphite mass to fuel mass is used in the first reactor


38


to slow down neutrons within the problematic energy band (i.e. neutrons between approximately 0.2 eV to approximately 1.0 eV) before these neutrons reach the driver fuel component


20


. Additionally, non-fissile transuranics, including but not limited to Np


237


, Am


241


and Pu


240


in the driver fuel component


20


and transmutation fuel component


22


(see

FIG. 1

) can be used to assure negative reactivity feedbacks in the first reactor


38


and act as a burnable poison/fertile material to allow for extended burnups—replacing Er


167


or other similar parasitic poisons.




With cross reference now to

FIGS. 1 and 7

, the driver fuel component


20


and transmutation fuel component


22


remain in the first reactor


38


for approximately three years. Each year, 36 columns, 10 blocks high, of fresh (unreacted) fuel elements


106


are added to ring


118


and the partially reacted fuel elements


106


that have resided in ring


118


for one year are moved to ring


120


. Also, partially reacted fuel elements


106


that have resided in ring


120


for one year are moved to ring


116


and reacted fuel elements


106


that have resided in ring


116


for one year are removed from the first reactor


38


. During movement from ring


118


to ring


120


and movement from ring


120


to ring


116


, the fuel elements are axially shuffled. More specifically, the fuel elements


106


in each column


0


-


1


-


2


-


3


-


4


-


5


-


6


-


7


-


8


-


9


are axially shuffled into the new column


4


-


3


-


2


-


1


-


0


-


9


-


8


-


7


-


6


-


5


.




Continuing with cross-reference to

FIGS. 1 and 7

, it can be seen that reacted driver fuel


124


from the reacted fuel elements


106


that were removed from ring


116


of the first reactor


38


is then separated (box


126


) into transuranics


128


and fission products


130


using a baking process to heat up and evaporate volatile elements. It is calculated that the reacted driver fuel


124


will generally consist of approximately one-third transuranics


128


and two-thirds fission products


130


. As further shown, the fission products


130


can then be packaged (box


30


) and sent to the repository


32


. The transuranics


128


can be mixed with transmutation fuel component


22


(see box


40


) to make coated transmutation particles


54


(see

FIG. 3

) that are then introduced into the first reactor


38


for a three year residence time.




Continuing with

FIG. 1

, reacted transmutation fuel


132


that has been removed from the first reactor


38


after a three year residence time is then introduced into a second reactor


134


for further transmutation. It is calculated that approximately ⅝ of the reacted transmutation fuel


132


will be transuranics with the remainder being fission products.




As shown in

FIG. 9

, the second reactor


134


includes a sealable, cylindrical housing


136


having a window


138


that allows a beam of protons


140


to pass through the window


138


and into the housing


136


. In one implementation, the housing


136


is formed with a large length to diameter ratio to allow for adequate heat removal. A proton source


142


, such as a particle accelerator, is provided to generate the beam of protons


140


. A 10 MW proton source


142


capable of emitting a beam of protons


140


having energies of approximately 800 MeV and a current of approximately 10 mA can be used. A typical beam shape for the beam of protons


140


has a conical shape and a diameter of about 50 cm at the window


138


perpendicular to proton motion. The housing


136


is preferably sealable, air-tight and constructed primarily from high temperature steel alloys. A spallation target


144


is positioned inside the housing


136


for interaction with the beam of protons


140


. The spallation target


144


can be made of any material known in the pertinent art, such as Tungsten, which will emit fast neutrons in response to collisions between the beam of protons


140


and the spallation target


144


.




Like the first reactor


38


(see FIG.


6


), the second reactor


134


(shown in

FIG. 9

) can be a Modular Helium Reactor (MHR) wherein Helium is circulated through the reactor vessel to regulate temperature and extract heat from the vessel. The extracted heat can then be used, for example, to produce electricity. In addition to the advantages cited above, Helium is particularly suitable for use in the second reactor


134


because protons at the expected energies can travel with essentially no energy loss through Helium gas for several kilometers.




With cross reference now to

FIGS. 9 and 10

, it can be seen that hexagonally shaped fuel elements


146


containing reacted transmutation fuel


132


(see

FIG. 1

) are positioned in an annular arrangement surrounding the spallation target


144


. The fuel elements


146


used in the second reactor


134


are similar to the fuel elements


106


described above for use in the first reactor


38


. In greater detail, the fuel elements


146


consist of hexagonally shaped graphite blocks having machined holes for containing the reacted transmutation fuel


132


and channels to allow Helium coolant to be circulated through the blocks.




Referring now to

FIG. 10

, it can be seen that fuel elements


146


are arranged in the second reactor


134


in a substantially annular arrangement surrounding the spallation target


144


. A central reflector


148


is interposed between the spallation target


144


and the fuel elements


146


and a outer reflector


150


surrounds the fuel elements


146


. As further shown, the fuel elements


146


are arranged in three annular rings


152


,


154


,


156


, with each ring


152


,


154


,


156


containing thirty-six columns of fuel elements


146


with each column having a stack of ten fuel elements


146


.




The presence of fissile materials in the second reactor


134


are limited to ensure that the reaction remains subcritical. For the method


11


, materials in the second reactor


134


are configured to promote transmutation of the transmutation fuel component


22


(See

FIG. 1

) with neutrons within an energy band extending from approximately 1.0 eV to approximately 10.0 eV (see FIG.


8


). Thermal neutrons within this energy band (i.e. approximately 1.0 eV to approximately 10.0 eV) are referred to as epithermal neutrons herein.




To achieve this, the transmutation fuel component


22


is formed into substantially spherical particles having a relatively small transmutation fuel kernel diameter, d


2


, (see

FIG. 2

) that is between approximately 130 μm and approximately 170 μm, to maximize the surface area of the transmutation fuel component


22


and thereby increase transmutation using epithermal neutrons. Alternatively, diluted 250 μm transmutation fuel kernels


56


(having the same amount of transmutation fuel component


22


per kernel as the undiluted 150 μm kernels) can be used to achieve the same effect as 150 μm kernels while facilitating the manufacturability of the particles. The same coated transmutation particles


54


(see

FIG. 3

) are used in both the first reactor


38


and second reactor


134


.




Continuing with

FIG. 10

, it can be seen that the fuel elements


146


(which include graphite blocks) are placed in a substantially annular arrangement interposed between a central reflector


148


and an outer reflector


150


. The graphite in the second reactor


134


moderates fast neutrons from the spallation target


144


. One collateral benefit of the graphite is that it prevents fast neutron damage to reactor structures and equipment. A relatively low ratio (i.e. less than 10:1) of graphite mass to fuel mass can be used in the second reactor


134


to increase transmutation of the transmutation fuel component


22


with epithermal neutrons.




Continuing with

FIG. 10

, the reacted transmutation fuel


132


from the first reactor


38


remains in the second reactor


134


for approximately four years. Every one and one third years, thirty-six columns of fuel elements


146


with each column having a stack of ten fuel elements


146


containing reacted transmutation fuel


132


from one or more first reactors


38


are added to the second reactor


134


. In one implementation of the method


11


, the second reactor


134


is sized to receive reacted transmutation fuel


132


from four first reactors


38


, which in turn are sized to receive all the spent fuel from five large Light Water Reactors (i.e. each first reactor


38


is sized to receive approximately all the spent fuel from 1.25 large LWR's). The three hundred and sixty fuel elements


146


are initially introduced into ring


156


of the second reactor


134


. Fuel elements


146


that have resided in ring


156


for approximately one and one third years are moved to ring


154


with axial reshuffling as described above. Fuel elements


146


that have resided in ring


154


for approximately one and one third years are moved to ring


152


with axial reshuffling, and fuel elements


146


that have resided in ring


152


for approximately one and one third years are removed from the second reactor


134


. It is calculated that the fuel elements


146


removed from the second reactor


134


will contain approximately ⅛ transuranics and ⅞ fission products. This material is then sent directly to repository


32


. The spherical particles of transmutation fuel are coated with an impervious, ceramic material which provides for containment of the treated transmutation fuel in the repository


32


. Calculations indicate that the method


11


as described above can destroy all of the fissile transuranics, such as Pu


239


, and 95% or more of the remaining transuranics present in the LWR spent fuel.




While the particular system and method for destroying radioactive waste as herein shown and disclosed in detail are fully capable of obtaining the objects and providing the advantages herein before stated, it is to be understood that they are merely illustrative of the presently preferred embodiments of the invention and that no limitations are intended to the details of construction or design herein shown other than as described in the appended claims.



Claims
  • 1. A method for transmuting spent fuel from a nuclear reactor, said method comprising the steps of:separating the spent fuel into components including a first component comprising at least one fissile isotope and a second component comprising at least one nonfissile, transuranic isotope; disposing said separated first and second components in a reactor; initiating a critical, self-sustaining fission reaction in said reactor to transmute at least a portion of said first component and produce a reacted first component and a reacted second component; separating said reacted first component into fractions including a transuranic fraction comprising at least one nonfissile, transuranic isotope; reintroducing said transuranic fraction into said reactor for further transmutation; positioning said reacted second component at a distance from a spallation target; and transmuting said reacted second component with neutrons from said spallation target.
  • 2. A method as recited in claim 1 wherein said first component comprises Plutonium239.
  • 3. A method as recited in claim 2 further comprising the step of forming said first component in substantially spherical kernels having a diameter between approximately 270 μm and 330 μm to minimize neutron capture by said Plutonium239 in the energy region between approximately 0.2 eV and approximately 1 eV.
  • 4. A method as recited in claim 3 further comprising the step of coating said kernels with a ceramic coating.
  • 5. A method as recited in claim 4 further comprising the steps of:providing a graphite block formed with at least one hole; disposing said coated kernels in said hole; and disposing said block and said coated kernels in said reactor.
  • 6. A method as recited in claim 4 further comprising the steps of:disposing a graphite central reflector in said reactor; providing a plurality of graphite blocks with each block formed with at least one hole; disposing said coated kernels in at least one said hole of each said block; and positioning said blocks in said reactor in a substantially annular arrangement to surround said graphite central reflector.
  • 7. A method as recited in claim 1 wherein said second component comprises a non-fissile isotope of a transuranic element to provide a stable, negative temperature coefficient of reactivity for safe control of the nuclear reaction, said element selected from the group consisting of Plutonium, Americium, Curium and Neptunium.
  • 8. A method as recited in claim 2 further comprising the steps of:providing an amount of said second component suitable to prepare an undiluted kernel of said second component having a diameter of approximately 1.50 μm; and diluting said amount of said second component to prepare a substantially spherical kernel having a diameter between approximately 220 μm and 350 μm.
  • 9. A method as recited in claim 2 further comprising the step of circulating Helium through said reactor to regulate the temperature inside said reactor.
  • 10. A method as recited in claim 1 wherein said step of transmuting said reacted second component with neutrons from said spallation target comprises the steps of:using a particle accelerator to generate a beam of protons; and directing said beam of protons to strike said spallation target with said protons and generate fast neutrons.
Parent Case Info

The present application is a continuation-in-part of U.S. patent application Ser. No. 09/511,749 filed Feb. 24, 2000 now U.S. Pat. No. 6,472,677, the contents of which are hereby incorporated by reference herein.

US Referenced Citations (7)
Number Name Date Kind
3649452 Chin et al. Mar 1972 A
4780682 Politzer Oct 1988 A
4987007 Wagal Jan 1991 A
5160696 Bowman Nov 1992 A
5513226 Baxter et al. Apr 1996 A
6233298 Bowman May 2001 B1
6472677 Rodriguez et al. Oct 2002 B1
Continuation in Parts (1)
Number Date Country
Parent 09/511749 Feb 2000 US
Child 10/281380 US