High costs with nuclear waste disposal at the Yucca Mountain repository are typically attributed to the large number of disposal containers. Additionally, the risks associated with early container failure typically increase with as the number of containers increases. The current (also referred to as “License Application” or LA) containers (also referred to as “waste packages”) are typically designed with free spaces between individual nuclear material sub-containers (also referred to herein as assemblies, units, or canisters). The loosely packed container design, i.e. the LA design, often leads to significantly more containers.
Certain embodiments provide container designs that allow for more efficient storage of nuclear wastes. Some embodiments allow for the disposal of a plurality of different types of nuclear waste within the same container. In at least one embodiment, a waste container includes a central nuclear material sub-container of a first type surrounded, such as concentrically, by one or more nuclear material sub-containers of a second type. In a further embodiment, a nuclear material container includes a plurality of nuclear material sub-containers of a first type formed in a central nucleus and surrounded by one or more nuclear material sub-containers of a second type. By increasing the amount of nuclear material that may be stored in each container, the number of containers needed may be reduced. In addition, proper selection of the amount of each type of nuclear sub-container in the container can be used to adjust the amount of heat generated by each container, for example, to comply with regulatory guidelines.
For example, certain embodiments of the invention provide alternative container designs that would utilize the free space in the LA spent nuclear fuel (SNF) containers for holding additional nuclear wastes. At least some designs may reduce disposal costs and use the additional heat, due to more waste per container, for favorably engineering the emplacement drift thermal-hydrology.
Modification of the SNF, i.e. the pressurized water reactor (PWR) and the boiling water reactor (BWR), containers are proposed in order to accommodate additional wastes making more effective utilization of the waste package space. The additional wastes are the Department of Energy High Level Waste (DOE-HLW) canisters that are planned in the LA design for disposal within the 6 canister over-pack containers (referred to as 5 DOE-HLW/1 DOE-SNF containers). Due to the similar characteristics in the commercial waste (BWR and PWR assemblies) and the DOE-HLW forms, both may be placed together into one waste container.
Two new designs are proposed for both the PWR and the BWR waste packages. The proposed design configurations would make more effective use of the available waste package volume, at least substantially eliminating the gap in the waste packages to accommodate colder DOE-HLW canisters. At least certain embodiments incorporate DOE-HLW canisters within the BWR and PWR containers. The proposed new designs are also subsequently referred to as co-disposal waste package designs. The designs adhere to the current federal regulatory standards.
The new designs may decrease the number of DOE-HLW packages and may eliminate the necessity of, or the number of, current DOE-HLW containers. As a result there may be a decrease in the waste disposal cost and due better engineering of the emplacement drift. Incorporations of these new designs may eliminate the necessity of, or reduce the number of, the 5 DOE-HLW/1 SNF waste packages by implementation of one design and may decrease the number of the DOE-HLW canisters to be disposed by more than half of the current number of canisters by implementation of the other design.
The present disclosure also provides method for using the disclosed containers. For example, the disclosed containers can be used in an emplacement drift.
There are additional features and advantages of the various embodiments of the present invention. They will become evident as this specification proceeds.
In this regard, it is to be understood that this is a brief summary of the various embodiments described herein. Any given embodiment of the present invention need not provide all features noted above, nor must it solve all problems or address all issues in the prior art noted above.
In order to facilitate review of the various embodiments of the disclosure, the following explanations of specific abbreviations and terms are provided:
BWR—boiling water reactor
DOE—United States Department of Energy
PWR—pressurized water reactor
HLW—high1 level waste
SNF—spent nuclear fuel
LA—license application
SS—stainless steel
NRC—Nuclear Regulatory Commission
The disclosure proceeds with reference to certain specific embodiments of nuclear material containers according to the present disclosure. It to be understood that these embodiments are only exemplary and do not limit the scope of the disclosure. The containers contain a number of sub-containers, the exact number, nature, and position of which can be varied.
44 BWR/1 DOE-HLW and 24 PWR/1 DOE-HLW Waste Containers
This design accommodates the commercial SNF assemblies and a DOE-HLW in the packages together in one waste package. The design is modification of the License Application design (cross-sectional schematic shown in
The co-disposal 24 PWR/1 DOE-HLW package (
The DOE-HLW/SNF canisters in the co-disposal BWR packages are confined by 4 cm thick stainless steel (SS) layers and those in the co-disposal PWR packages are confined by a 2 cm thick SS layer. The assemblies surround the cylinders in a radial manner enclosed in basket made of partly Neutronit for neutron shielding and partly Aluminum for structural strength and effective heat transport.
55 BWR/3 DOE-HLW and 18 PWR/3 DOE-HLW Waste Packages
This new design accommodates the commercial SNF assemblies and the DOE-HLW canisters in single packages. This design is generally similar in concept to the design mentioned above (i.e. in part 1.), however, with at least one difference. The at least one difference is made towards accommodating more waste per package at an overall increase in the waste volume.
The co-disposal 55 BWR/3 DOE-HLW waste packages, as shown in
Confirmation of the Co-Disposal Containers to Safety Requirements
The radionuclides containment in the co-disposal packages are as safe as those of the license application (LA) design. The SNF assemblies are contained in the neutron shield basket, though the geometry of the same is being varied to make more effective utilization of the available waste package interior volume. The current Nuclear Regulatory Commission (NRC) safety criterion requires the HLW and the SNF temperatures to be below 350° C. Additionally, according to present NRC criteria, the HLW waste temperatures must not go beyond 400° C., which is nearly the glass transition temperature of the HLW waste glass. Based on the waste package internal geometry, effective heat transport can be achieved from the waste package interior to it exterior by using aluminum shunts that would maintain the waste form in safe thermal limits.
Advantages of the Co-Disposal Containers
The proposed designs may yield lesser number of waste packages. The primary design advantages are potential cost savings in terms of the associated packaging materials, fabrication, transportation, and handling costs. The effective utilization of the waste package space would keep the waste package wall (or outer shell) hot which would delay condensation of water on the surface and may significantly reduce the required number waste packages.
The 44 BWR/1 DOE-HLW waste package design and the 24 PWR/1 DOE-HLW waste package designs may eliminate the need for half of the 5 DOE-HLW/1 DOE-SNF, as shown in Table 1. A feature of this design is the potential generation of waste disposal cost savings and the possibility of more favorable drift thermal-hydrology without significantly changing the waste package dimensions and the associated materials, fabrication, transportation and handling costs.
The 55 BWR/3 DOE-HLW and 18 PWR/3 DOE-HLW waste package dimensions are suggested, taking into the DOE-HLW inventory, for eliminating or reducing the necessity of the 5 DOE-HLW/1 DOE-SNF packages. A drift arrangement corresponding to the proposed waste package design is shown in
Thermal Design of an 52 BWR Waste Package
A 52 BWR waste package thermal modeling methodology is described below, demonstrating that the additional heat, due to the more waste in the container, can be effectively transported out of the container. The effective heat transport sustains the spent fuel in safe temperature range. A similar methodology can be applied for modeling the proposed co-disposal containers.
Description of the 52 BWR Waste Package Design
The cross-sectional geometry of the BWR spent fuel cask is shown in
The aluminum shunts are the other part of the basket tube. These are shown in
Thermal Model of 52 BWR Waste Package
The three dimensional heat transfer mechanism in the waste package is complex. The heat flow problem in the radial direction (i.e. in one cross-section) of the waste package is modeled on the millimeter scale from the heat generating fuel-rods to the outer surface of the waste package. The axial heat flow is modeled as a separate task, incorporated in the three-dimensional emplacement drift-scale thermal model, providing outer surface temperature distribution as boundary condition for the radial flow waste package model. This axial heat flow model is a centimeter-scale emplacement drift thermal model accounting for the neighboring-effects of the various waste containers with different heat dissipation, the ultimate reason for having axial temperature variation and heat flow along the drift. The procedure adapted is the heat flow network method that can be implemented using MULTIFLUX [Danko (2000), incorporated by reference herein].
The waste package cross-section is descretized as shown in
The heat flow network allows connections between a node to other desired nodes. MULTIFLUX calculates the thermal admittance of each connection. The admittances for the connections for all the nodes are processed as coefficients in a network matrix representing heat balance equations for the entire model domain. The solution of the model provides the temperature distribution. The model outputs the steady state temperature distribution at a given boundary condition. The boundary condition in this case is the time-dependent waste package surface temperature from the thermal and moisture flow model constituted for an entire emplacement drift in an emplacement tunnel at Yucca Mountain. The description of this waste package exterior thermal and moisture flow model is described in detail in another paper [Barhami & Danko, (2005), incorporated by reference herein]. The thermal model within the waste package is described with the following constitutive equations (1) to (3) for all connections:
For conduction,
For radiation,
qij=AijBεijφij(Ti4−Tj4) (2)
For convection,
qij=Aijhij(Ti−Tj) (3)
The heat balance equation for a node is given by:
Σq=0 (4)
Calculation of Assembly Thermal Conductivity with Helium
The interior heat transfer in the assembly is a complex phenomenon because of its anisotropic structure. The BWR assembly is a square enclosure having a 14 cm×14 cm cross-section and 4.5 meter (m) length. Within its cross-section there is an 8×8 fuel rod matrix consisting of 62 fuel rods and 2 moderator rods. The fuel rods consist of the UO2 fuel pellets, a very thin gap (in between the pellet and the cladding) filled with pressurized helium and fission product gases, and the zircaloy-2 cladding.
The fuel rods are arranged inside the assembly as non-touching-cylinders, kept in place by distant-keepers. Outside the fuel rods is the backfill media (pressurized helium in case of the BWR assemblies). More than one mode of heat transfer is usually prevalent. The kind of backfill media and the backfill pressure markedly affects the heat transfer mode and the fuel-assembly wall temperature difference [Manteufel & Todreas (1993) and Canaan & Klein (1996)].
Experimental and modeling results have consistently demonstrated that very little or no natural convection occurs within the assemblies with helium as backfill gas. Natural convection occurs due to buoyancy driven fluid flow when the Raleigh Number exceeds its critical value. Experimental studies [Keyhani et al (1987), Gotovsky et al (1986) and Vdovets et al (1986)] have concluded that the critical Raleigh Number cannot be reached in the applicable transportation and storage conditions (i.e. temperature and pressures) for the assemblies with helium backfill. The dominant modes of heat transfer with helium backfill under pressurization in the range of 0-5 atmospheres are conduction and radiation [Manteufel and Todreas (1993), Canaan & Klein (1996)].
The effective thermal conductivity of the waste package assemblies includes temperature-dependent thermal radiation and therefore it requires numerical modeling. The assembly heat transfer phenomena has been studied [Canaan & Klein (1996), Manteufel and Todreas (1992) & (1993), Keyhani & Luo (1994) and Kelkar & Patankar (1990)] for an accurate estimation of the effective thermal conductivity. Manteufel and Todreas (1993) developed analytical formulae for their continuum and lumped Keff/Hedge models for determination of assembly effective thermal conductivity. Both of these models predict very nearly equal values for the BWR assembly thermal conductivity, and therefore they confirm each other's validity. The continuum Keff/Hedge model is used in this Example for calculating the BWR assembly effective thermal conductivity.
Description of the Continuum Keff/Hedge Model for Determination of the BWR Assemblies' Effective Thermal Conductivities
The assembly is assumed to have two distinct regions, i.e. an interior region containing all the fuel rods and an exterior region surrounding and encapsulating the interior region, called the wall (
The assembly interior effective conductivity, Kai, is given by equation (5) [Manteuffel & Todreas (1993)]. The first term to the right of the equation expresses the interior conduction in the fuel rods comprising the weighted average of the UO2 pellets, zircaloy cladding and helium fill. The second term on the right represents thermal radiation.
Kai=FcondKgas+CradBπd4T3 (5)
The assembly edge heat transfer coefficient is given in equation (6). The first term in the right hand side is the wall conductive heat transfer coefficient and the second term is the wall radiative heat transfer coefficient. The values, Fcond,w (the wall conduction factor) and f (the edge to interior heat transfer ratio), are determined in the manner defined by Manteuffel & Todreas (1993), incorporated by reference herein:
The overall assembly effective conductivity can be determined from the resultant sum, R, of the thermal resistances, R1 and R2, representing the interior and edge regions respectively. The total resistance, R, is given by equation (7) and the effective thermal conductivity of the assembly, Kassembly is given by equation (8).
Convective-Radiative Heat Transfer Across the Gap Between the Basket and the Waste Package Inner Cylinder
Heat transfer in the gap between the waste package and inner cylindrical walls of the waste containers is convective and radiative. The convective heat transfer is typical to that occurring in horizontal and vertical enclosures depending on the location of the gap. MULTIFLUX allows for modeling natural convection in enclosures. However, due to the low temperature differences in the gap, a simple heat conduction model is selected for the helium filled gap in the present study. The radiative heat transfer is modeled either as a rectangular-type or as wedge-type domain shown in FIGS. 12 (a) and (b). The geometry of the gap in most places (e.g. node 185 to 208 in
The radiative view factor is calculated using the formula [Handbook of Essential Formulae and Data on Heat Transfer for Engineers] given by equation (9) for radiation from plate 1 to 2 and that from plate 1 to 3 are determined by using view factor arithmetic, as given by equation (10).
Results
The thermal model with 224 nodes with convective, conductive and radiative thermal connections between them was configured in MULTIFLUX. The heat dissipation of the spent fuel was modeled as time-dependent heat source, directly applied to the fuel assembly nodes. The thermal model was solved for the hottest BWR package along the emplacement drift for 27 different time instants over the first 5000 years storage time period. For each time instant the solution was iterated until the temperature-dependent heat transport connections were calculated within 0.1° C. of the balanced temperature.
The feasibility of the design in terms of maintaining the maximum waste package temperature, that of the spent fuel cladding, below 350° C. (the regulated NRC limit [CRWMS M&O 1998a]), has been demonstrated in the results. As can be seen from FIGS. 15 (a) and 15 (b) the maximum attained cladding temperature is about 240° C. The maximum temperature difference between the cladding and waste package outer surface is less than 100° C., a favorably low value in spite of the enlarged design with about 20% or more waste and corresponding heat load in it.
The assembly thermal conductivity is slightly temperature dependent, and as a result each assembly has a unique thermal conductivity depending on its relative position in the waste package cross-section. These steady state cross-sectional temperature variations range from 5 to 20° C. More variations in the temperature are caused by the changing boundary temperature with time which is shown in
The temperature drop through the helium-filled gap is less than that occurring through the aluminum shunts. The effect of gap temperature drop can be observed in
It is to be understood that the foregoing is a detailed description of certain embodiments. The scope of the present invention is not to be limited thereby and is to be measured by the claims, which shall embrace appropriate equivalents.
Nomenclature
q—heat flux [W]
qij—net heat transfer between any two nodes, “i” and “j” [W]
Ti—temperature of the node, “i” [K or ° C.]
Tj—temperature of the node, “j” [K or ° C.]
δij—effective heat flow distance between any two nodes, “i” and “j” [m]
Aij—normal area between any two nodes, “i” and “j” [m2]
Kij—effective thermal conductivity between any two nodes, “i” and “j” [W/m-K]
B—Boltzmann's constant (5.67×10−8 W/m2-K4)
εij—emissivity of the radiating surface between any two nodes, “i” and “j”
φij—view factor between any two nodes, “i” and “j”
hij—convective heat transfer coefficient between any two nodes, “i” and “j” [W/m2-K]
Kai—assembly effective conductivity [W/m-K]
Kcond—assembly interior conductivity [W/m-K]
Kgas—thermal conductivity of helium in the range of the assembly temperature and pressure [Unterzuber et al (1980)] (determined as 0.2 W/m-K)
Fcond—conduction factor as experimentally determined for the given geometry and materials [Manteuffel & Todreas (1991)] (determined as 2.16)
Crad—radiative coefficient (determined as 0.4 for the BWR assembly under consideration as determined by Manteuffel & Todreas (1991))
d—fuel rod outer diameter (1.3 cm, or 0.013 m)
T—average fuel rod temperature (assumed to be 500° K as initial value)
Fcond,w—conduction factor for the wall
f—edge-to-interior heat transfer ratio (taken as 0.4518 for BWR assemblies, as calculated from (8))
w—distance from the centre of the outermost fuel rod to the wall exterior (taken as 0.01618 m for the BWR assemblies)
p—pitch, or the distance between the centers of two fuel rods (taken as 0.01352 m for the BWR assemblies)
Crad,w,2—second wall conduction factor [Manteuffel & Todreas (1991)] (determined as 0.085 for BWR assemblies)
L—assembly interior width [m]
A—assembly area in the inter-section of the interior and the exterior regions [m2]
Lassembly—length of the assembly cross-sectional edge (taken as 0.14 m)
F1-2—view factor from surface 1 to 2
F1-3—view factor from surface 1 to 3
17.) “Controlled Design Assumptions Document”, B00000000-01717-4600-00032 REV 05, ICN 0, Las Vegas, Nev., CRWMS M&O, ACC: MOL.19980804.0481
a—Enlargement of the DOE—HLW canisters' diameter to 0.8 m for accommodation in the co-disposal 44 BWR/1 DOE-HLW packages as shown in
The present application claims the benefit of U.S. Provisional Patent Application No. 60/654,214, filed Feb. 17, 2005, the disclosure of which is hereby incorporated by reference.
Number | Date | Country | |
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60654214 | Feb 2005 | US |