HIGH-DENSITY SUBTERRANEAN STORAGE SYSTEM FOR NUCLEAR FUEL AND RADIOACTIVE WASTE

Abstract

A passively cooled stackable nuclear waste storage system includes an at least partially below grade cavity enclosure container (CEC) and above grade cask. Each vessel includes a cavity holding a nuclear waste canister containing spent nuclear fuel or other high-level radioactive wastes. The CEC is founded on a below grade concrete base pad and cask is mounted on an above-grade concrete top pad in a vertically stacked arrangement. The upper cask comprises a perforated baseplate which establishes fluid communication between cavities of both casks and is configured to prevent radiation shine. One or both vessels include air inlets which draw ambient cooling air into their respective cavities for cooling the nuclear waste. Air heated in the lower CEC rises into the upper cask through the baseplate where it mixes with air drawn into the cask and is returned to atmosphere. The system increases storage capacity of new or existing facilities.

Claims

1. A passively ventilated nuclear waste storage system comprising: a lower cavity enclosure container configured for mounting at least partially below grade, the cavity enclosure container comprising at least one first air inlet and a first internal cavity configured for holding a first canister which contains radioactive nuclear waste; and an upper cask comprising a second internal cavity configured for holding a second canister which contains radioactive nuclear waste, the cask being located above grade; at least one air outlet configured to allow heated air in a top portion of the second internal cavity to exit the second internal cavity of the cask; the cask stacked atop the lower cavity enclosure container in a vertically stacked arrangement so that a cask-to-cask interface is formed between the cavity enclosure container and the cask; wherein the first and second internal cavities are fluidly interconnected so that heated air in a top portion of the first internal cavity can flow into a bottom portion of the second internal cavity.

2. The system according to claim 1, wherein the upper cask is coaxially aligned with a vertical centerline axis of the cavity enclosure container.

3. The system according to claim 1, wherein the upper cask is mounted on an above grade concrete top pad surrounding an upper portion of the cavity enclosure container.

4. The system according to claim 3, wherein the upper cask is bolted to the top pad and the lower cavity enclosure container is mounted on a below grade concrete base pad.

5. The system according to claim 2, further comprising an engineered fill disposed between the top pad and base pad.

6. The system according to claim 2, wherein the cavity enclosure container comprises a vertically elongated cylindrical shell body of which a majority portion is disposed below grade, and the cask comprises a vertically-elongated cylindrical body all of which is above grade.

7. The system according to claim 6, wherein the body of the cask comprises a radiation shielding material including concrete and a body of the cavity enclosure container comprises an all metallic body.

8. The system according to claim 7, wherein the body of the cask includes a vertical sidewall comprising cylindrical metallic inner shell, a cylindrical metallic outer shell, and the radiation shielding material disposed between the shells.

9. The system according to claim 8, wherein the concrete of the radiation-shielding material contains hematite for enhancing heat transfer through the sidewall to ambient atmosphere.

10. The system according to claim 1, wherein a top end of the cavity enclosure container is open and the cask comprises a perforated baseplate configured to fluidly interconnect the internal cavity of the cask with the internal cavity of the cavity enclosure container.

11. The system according to claim 10, wherein the perforated baseplate is configured to engage and support the second canister.

12. The system according to claim 10, wherein the perforated baseplate includes a plurality of axial through holes configured to transfer cooling air from the internal cavity of the cavity enclosure container upwards into the internal cavity of the cask.

13. The system according to claim 12, wherein the through holes have a height to diameter ratio of at least 2:1.

14. The system according to claim 12, wherein the perforated baseplate comprises a solid metallic circular plate affixed to a bottom end of the cask, the plurality of axial through holes being formed and extending vertically completely through the plate.

15. The system according to claim 10, wherein the perforated baseplate is spaced vertically apart from the first canister in the cavity enclosure container such that the perforated support structure does not contact the first canister.

16. The system according to claim 1, further comprising a radiation shielded closure lid detachably mounted on top of the cask.

17. The system according to claim 16, wherein the lid defines an air outlet duct configured to discharge cooling air received from the cask to ambient atmosphere.

18. The system according to claim 1, further comprising a vertically elongated first cooling air feeder shell in fluid communication with ambient atmosphere and operable to draw in ambient air, the first cooling air feeder shell being fluidly coupled directly to the first air inlet of the cavity enclosure container via a first flow conduit.

19. The system according to claim 18, wherein the first flow conduit comprises a horizontally-extending piping fluidly coupling a lower portion of the internal cavity of the cavity enclosure container to a lower portion of the first cooling air feeder shell.

20. The system according to claim 18, wherein the first cavity enclosure container is structurally coupled to the first cooling air feeder shell by a plurality of horizontally-extending cross-support members which act as lateral bracing.

21. The system according to claim 20, wherein the first cavity enclosure container and the first cooling air feeder shell are fixedly mounted on a metallic common support plate forming a self-supporting and transportable modular unit, the common support plate being configured for rigid anchoring onto a below grade concrete support structure.

22. The system according to claim 1, wherein the upper cask includes a plurality of second air inlet ducts configured to draw ambient ventilation air for cooling the nuclear waste into the second internal cavity of the upper cask.

23. The system according to claim 22, wherein at least the cavity enclosure container includes a plurality of first air inlets configured to draw ambient ventilation air for cooling the nuclear waste into the first internal cavity.

24. The system according to claim 22, wherein the second air inlet ducts of the upper cask are positioned to draw ambient ventilation air into a lower portion of the second internal cavity, and the at least one first air inlet of the lower cavity enclosure container is to draw ambient ventilation air into a lower portion of the first internal cavity.

25. The system according to claim 24, wherein the second air inlet ducts are configured to draw ambient ventilation air radially inwards into the second internal cavity in a circuitous path such that no straight line of sight exists between an external entrance opening and an internal exit opening of each air inlet duct in the upper cask.

26. The system according to claim 22, wherein the second air inlet ducts of the upper cask each have a vertically elongated slit-like shape.

27. The system according to claim 1, wherein the second internal cavity of the upper cask has a second diameter which is larger than a first diameter of the lower cavity enclosure container.

28. The system according to claim 1, wherein the first and second nuclear waste canisters each comprise cylindrical metallic bodies which do not contain a radiation shielding material.

29. The system according to claim 28, wherein the first and second cavities of the lower and upper casks each have a height and transverse cross-sectional area configured to hold no more than a single respective first or second nuclear waste canister.

30. The system according to claim 1, further comprising a first ventilation annulus formed in the first internal cavity between the shell body of the lower cavity enclosure container and the first nuclear waste canister, and a second ventilation annulus formed in the second internal cavity between an inner shell of the upper cask and the second nuclear waste canister, the second ventilation annulus having a greater radial width than the first ventilation annulus.

31. The system according to claim 10, wherein a peripheral portion of the perforated baseplate of the upper cask defines an annular radially protruding mounting flange which is detachably coupled to a concrete top pad surrounding an upper portion of the cavity enclosure container.

32. The system according to claim 31, wherein the mounting flange of the upper cask is coupled to the top pad by a plurality of bolts.

33. The system according to claim 10, wherein a ventilation air flow path is defined by the lower cavity enclosure container and the upper cask in which ventilation air flows through the at least one air inlet of the cavity enclosure container into the first internal cavity, is heated and rises upwards therefrom through the perforated baseplate and into the second internal cavity of the upper cask, and is discharged back to ambient atmosphere via the closure lid on the upper cask.

34. The system according to claim 10, wherein the perforated baseplate further comprises a plurality of spacer plates attached to a top surface thereof, the spacer plates configured to engage and elevate a bottom of the second nuclear waste canister above the perforated baseplate so that ventilation can flow beneath the second nuclear waste canister.

35-59. (canceled)

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0036] The features of the exemplary embodiments of the present invention will be described with reference to the following drawings, where like elements are labeled similarly, and in which:

[0037] FIG. 1 is a perspective view of an ISFSI facility comprising a first embodiment of a nuclear waste storage system according to the present disclosure for consolidated interim storage of spent nuclear fuel and other high level radioactive nuclear waste materials;

[0038] FIG. 2 is a top plan view thereof;

[0039] FIG. 3 is a perspective view of one of the nuclear waste storage rows of the ISFSI facility of FIGS. 1 and 2;

[0040] FIG. 4 is a first cross sectional view of a second embodiment of a nuclear waste storage system showing a cavity enclosure container (CEC) and cooling air feeder shell thereof;

[0041] FIG. 5 is a second cross sectional view thereof of the CEC alone;

[0042] FIG. 6 is a top plan view of an arrangement of multiple CECs of the second embodiment;

[0043] FIG. 7 is a perspective view of one nuclear waste storage row according to the second embodiment;

[0044] FIG. 8 is a top perspective view of the first embodiment of a nuclear waste storage system of FIGS. 1-3 showing one of the modular nuclear waste storage units including a CEC; pair of directly fluidly coupled cooling air feeder shells all mounted on a common support plate;

[0045] FIG. 9 is a bottom perspective view thereof;

[0046] FIG. 10 is a first lateral side view thereof;

[0047] FIG. 11 is a second lateral side view thereof;

[0048] FIG. 12 is a front view thereof;

[0049] FIG. 13 is a top view thereof with the top lid in place on the CEC;

[0050] FIG. 14 is a top view thereof with the top lid removed to show the internal cavity of the CEC;

[0051] FIG. 15 is a top view thereof with the top air intake housing removed from the pair of cooling air feeder shells to reveal the array of radiation attenuator plates therein;

[0052] FIG. 16 is a top perspective view thereof;

[0053] FIG. 17 is a cross-sectional perspective view thereof showing the modular nuclear waste storage unit installed on a concrete base pad below grade, a concrete top pad, and engineered fill therebetween;

[0054] FIG. 18 is a cross-sectional side view thereof;

[0055] FIG. 19 is a cross-sectional side view thereof showing multiple CECs and cooling air feeder shells; in part of the nuclear waste storage row of FIG. 3;

[0056] FIG. 20 is a top view of a third embodiment of a nuclear waste storage system according to the present disclosure showing a pair of CECs and cooling air feeder shells;

[0057] FIG. 21 is a side cross sectional view of a stackable nuclear waste storage system for storing high level nuclear radioactive waste material including the below grade lower CEC of FIGS. 4-5 and an above grade upper cask mounted over and atop the CEC;

[0058] FIG. 22 is a first perspective view thereof;

[0059] FIG. 23 is a second perspective view thereof;

[0060] FIG. 24 is a first side view thereof;

[0061] FIG. 25 is a second side view thereof;

[0062] FIG. 26 is a first top view of the storage system;

[0063] FIG. 27 is a second top view of the storage system;

[0064] FIG. 28 is a transverse cross sectional view through the lower CEC showing the air inlet ducts and air inlet of the CEC;

[0065] FIG. 29 is a first vertical cross sectional view of the storage system including the lower CEC and upper cask;

[0066] FIG. 30 is a second vertical cross sectional view thereof;

[0067] FIG. 31 is a third vertical cross sectional view thereof;

[0068] FIG. 32 is a fourth vertical cross sectional view thereof;

[0069] FIG. 33 is a fifth vertical cross sectional view thereof;

[0070] FIG. 34 is a perspective view of a first embodiment of a central portion of a perforated baseplate of the upper cask;

[0071] FIG. 35 is a perspective view of a second embodiment of a central portion of the perforated baseplate showing the entire structure of the baseplate;

[0072] FIG. 36A is an enlarged partial transverse cross sectional view of storage system showing the cask-to-CEC interface area;

[0073] FIG. 36B is a detail taken from FIG. 36A;

[0074] FIG. 37 is a partial transverse cross sectional view of the upper portion of the upper cask and cask lid;

[0075] FIG. 38 is a first perspective view of the CEC and cask assembly;

[0076] FIG. 39 is a second perspective view thereof;

[0077] FIG. 40 is first side view thereof;

[0078] FIG. 41 is a second side view thereof;

[0079] FIG. 42 is a first exploded perspective view thereof;

[0080] FIG. 43 is a second exploded perspective view thereof; and

[0081] FIG. 44 is a transverse cross sectional view taken through the air inlet ducts of the upper cask.

[0082] All drawings are schematic and not necessarily to scale. Parts given a reference numerical designation in one figure may be considered to be the same parts where they appear in other figures without a numerical designation for brevity unless specifically labeled with a different part number and described herein. References herein to a whole figure number herein which may comprise multiple figures with the same whole number but different alphabetical suffixes shall be construed to be a general reference to all those figures sharing the same whole number, unless otherwise indicated.

DETAILED DESCRIPTION OF THE EMBODIMENTS

[0083] The features and benefits of the invention are illustrated and described herein by reference to exemplary (“example”) embodiments. This description of exemplary embodiments is intended to be read in connection with the accompanying drawings, which are to be considered part of the entire written description. Accordingly, the disclosure expressly should not be limited to such exemplary embodiments illustrating some possible non-limiting combination of features that may exist alone or in other combinations of features.

[0084] In the description of embodiments disclosed herein, any reference to direction or orientation is merely intended for convenience of description and is not intended in any way to limit the scope of the present invention. Relative terms such as “lower,” “upper,” “horizontal,” “vertical,”, “above,” “below,” “up,” “down,” “top” and “bottom” as well as derivative thereof (e.g., “horizontally,” “downwardly,” “upwardly,” etc.) should be construed to refer to the orientation as then described or as shown in the drawing under discussion. These relative terms are for convenience of description only and do not require that the apparatus be constructed or operated in a particular orientation. Terms such as “attached,” “affixed,” “connected,” “coupled,” “interconnected,” and similar refer to a relationship wherein structures are secured or attached to one another either directly or indirectly through intervening structures, as well as both movable or rigid attachments or relationships, unless expressly described otherwise.

[0085] As used throughout, any ranges disclosed herein are used as shorthand for describing each and every value that is within the range. Any value within the range can be selected as the terminus of the range. In addition, all references cited herein to prior patents or patent applications are hereby incorporated by reference in their entireties. In the event of a conflict in a definition in the present disclosure and that of a cited reference, the present disclosure controls.

[0086] FIGS. 1 and 2 depict a top views of an ISFSI facility comprising a passively cooled subterranean consolidated interim storage (CIS) system 100 according to the present disclosure. System 100 comprises an array of underground vertical ventilated cavity enclosure containers (CECs) 110 each holding a single nuclear waste canister 150 containing the radioactive nuclear waste, and vertically elongated cooling air feeder shells 130 interspersed between and fluidly coupled to the CECs according to the present disclosure. The CECs and air feeder shells are configured to form integral parts of an unpowered natural convective ventilation system which operates via the thermo-siphon effect to cool the nuclear waste fuel stored in each CEC, as further described herein.

[0087] FIGS. 4 and 5 depict one embodiment of a CEC 110 and cooling air feeder shell 110 of a nuclear waste storage system according to the present disclosure in greater detail. The CECs 110 and cooling air feeder shells 130 are founded on and supported by a thick and horizontally extending subterranean bottom base pad 101 located below a cleared top surface or grade “G” of the native soil “S” at the CIS system site. Base pad 101 may be made of reinforced concrete in one embodiment; however, in other embodiments other materials may be used such as compacted gravel so long a stable and firm base is provided to support the CECs and air feeder shells. In the case of concrete as shown in the illustrated embodiment, the CECs and air feeder shells may be rigidly anchored to the base pad via multiple anchor members 103 such as robust J-shaped fasteners (threaded or otherwise), or other suitable types of anchors commonly used for fastening structural objects to concrete. Preferably, base pad 101 has a suitable thickness and construction robust enough to withstand postulated seismic events and maintain safe support the CECs 110 and containment of their nuclear waste contents.

[0088] A horizontally and longitudinally extending concrete top pad 102 is formed on top of the engineered fill 140 described below which is placed after pouring base pad 101. Top pad 102 therefore protrudes upwards from and is raised above the cleared grade G of the surrounding native soil S. The top pad is vertically spaced apart from the below grade base pad 101. The top pad defines an upward facing top surface 102a elevated above grade to prevent the ingress of standing water from the surrounding native soil S into the CECs 110 originating from rain events. Top surface 102a is substantially parallel to an upward facing top surface 101a of base pad 101 (the term “substantially” accounting for small variations in the level of surfaces 101a, 102a and recesses and/or contours formed therein for various purposes). The top pad 102 preferably extends at least one CEC outer diameter beyond the peripheral CECs 110. A gradually sloping terrain of native soil S around the top pad is preferred to facilitate rainwater drainage away from the CECs.

[0089] The vertical gap or space formed between base and top pads 101, 102 including the open horizontal/lateral space between adjacent CECs 110 and cooling air feeder shells 130 is filled with a suitable “engineered fill” 104 to provide both lateral radiation shielding for the nuclear waste stored inside the CECs 110, and full lateral structural support to the CECs and the cooling air feeder shells 130. Any suitable engineered fill may be used, such as without limitation flowable CLSM (controlled low-strength material) which is a self-compacting cementitious fill material often used in the industry as a backfill in lieu of ordinary compacted soil fill. Plain concrete may also be used as the inter-CEC and base pad to top pad gap filler material if it is desired to further increase the CIS system's radiation dose blockage capabilities. Other types of fill material which can provide radiation shielding and lateral support of the CECs and air feeder shells may be used.

[0090] With continuing general reference to FIGS. 4 and 5, each CEC 110 comprises a vertically elongated metallic shell body 111 defining a vertical centerline axis VC1 and which extends between a top end 112 and bottom end 113 of the body. The upper portion 111a of the shell body which defines top end 112 may be embedded in in concrete top pad 102 including between the top surface 102a and bottom surface 102b of the top pad 102 as shown. In some embodiments shown in FIGS. 4-5 and 17-19. the top end 112 of the CEC shell body 111 may terminate at the top surface 102a of the top pad. In either case, body 111 of CEC 110 may be cylindrical with a circular transverse cross-sectional shape in preferred non-limiting embodiments; however, other non-polygonal and polygonal shaped bodies may be used in certain other acceptable embodiments. The shell body 111 of each CEC 110 defines a vertically extending internal cavity 120 extending between ends 112, 113 which is configured for holding a cylindrical nuclear waste canister 150. As previously described herein, the waste canister 150 defines an interior space which holds spent fuel assemblies and/or other high level radioactive waste from the nuclear reactor.

[0091] The nuclear waste canister 150 stored in CEC 110 includes a vertically-elongated hollow cylindrical shell 151, top closure plate 152, and bottom closure plate 153. The top and bottom closure plates are hermetically seal welded to the top and bottom ends of shell 151 to form a gas-tight containment boundary for the nuclear waste stored in the canister. Canister 150 (i.e. shell and closure plates) may be formed of stainless steel in preferred embodiments for corrosion resistance. Canister 150 has a height H3 smaller than the height H2 of the CEC shell body 111 such that the top of the canister is spaced vertically apart and downwards from the bottom of the concrete top pad 102 (see, e.g., FIG. 3). This helps to both ensure that there is no lateral radiation streaming outwards from the CEC 110 at the top, and provides impact protection from incident projectiles (e.g., missiles, etc.). Canister 150 may be any type of nuclear waste/SNF canister, including without limitation Multi-Purpose Canisters (MPCs) available from Holtec International of Camden, N.J.

[0092] CEC 110 further includes a baseplate 114 hermetically seal welded to the bottom end 113 of shell body 111. A plurality of metallic radial support lugs 124 are welded to baseplate 114 and/or inside surface of the CEC shell body 111 in a circumferentially spaced apart manner at the bottom of cavity 120. The lugs are formed of suitable metal (e.g., stainless steel or other) and act to support and elevate the canister 150 above the baseplate. This creates open space between the top of the baseplate 114 and bottom closure plate 153 of the canister 150 to allow cooling ventilation air to circulate beneath the canister for removing heat emitted from the bottom of the canister by the nuclear waste material stored therein.

[0093] In one embodiment, the support lugs 124 may be generally L-shaped having a horizontal portion 124a welded to baseplate 114 and an integral adjoining vertical portion 124b welded to the inner surface of the CEC shell body 111. Vertical portions 124b each define radially-extending lower seismic restraint members which engage the sides of the canister 150 to keep it centered in the cavity 120 of the CEC 110 particularly during a seismic event (e.g., earthquake). A plurality of radially-extending upper seismic restraint members 123b project inwards from the shell body 111 in cavity 120 to keep the upper portion of the canister 150 centered. Restraint members 123b may be formed by circumferentially spaced apart metal plates or lugs welded to the inner surface of the CEC shell body 111.

[0094] When the canister 150 is positioned in the cavity 120 of the CEC 110, a ventilation annulus 121 is formed therebetween which extends for the full height of the canister. The ventilation annulus is fluid communication with the cooling air feeder shells 130 at the bottom via flow conduits 160 and an air outlet plenum 152 formed inside the CEC cavity 120 above the canister.

[0095] The shell body 111 and baseplate 114 of each CEC 110 may be formed of a suitable metal such as stainless steel for corrosion resistance.

[0096] The top end 112 of CEC 110 is enclosed by a removable thick radiation shielded lid 115 detachably mounted on top of the CEC shell body 111. The lid may have a composite metal and concrete construction including an outer shell 115a formed of steel such as stainless steel, and interior concrete lining 115b. This robust construction not only provides radiation shielding, but also offers added protection against projectile impacts. In one configuration, lid 115 includes a cylindrical circular upper portion 116a and adjoining cylindrical circular lower portion 116b having an outer diameter D4 smaller than an outer diameter D3 of the upper portion. An annular stepped shoulder 116c is formed between the upper and lower portions of the lid. Diameters D3 and/or D4 in some embodiments may be larger than an outer diameter D2 of the CEC shell body 111.

[0097] Lower portion of 116b of lid 115 is insertably positioned inside a corresponding upwardly open circular recess 117 formed into the top surface 102a of the top pad 102 around the top end 112 of each CEC 110 as shown (see, e.g., FIGS. 4-5). Recess 117 is larger in diameter D5 that the outer diameter D2 of the CEC shell body 111. In one embodiment, the upper portion 111a of CEC 110 (i.e. shell body 111) may include a diametrically enlarged top cylindrical section 111b which has the same diameter D5 as recess 117 and in fact defines the recess in this embodiment shown in FIGS. 14 and 16). The lid is slightly elevated and ajar from top pad 102 in its recess to create an air outlet 118 thereby forming an exit pathway between the lid and CEC 110 for the rising ventilation air from the cavity 120 of the CEC to return to ambient atmosphere. The air outlet 118 is configured to form a circuitous multi-angled pathway such that there is no direct line of sight from cavity 120 to atmosphere for radiation to escape (i.e. radiation streaming) Outlet 118 may have a double L-shaped configuration in one embodiment for this purpose as shown in FIG. 2; however other circuitous shaped pathways may be used.

[0098] In some embodiments as shown in FIGS. 16-18, the top section 111b of the CEC shell body 111 may further include a flat radially projecting annular seating flange 111c. The seating flange is configured for engaging and resting on top surface 102a of the concrete top pad 102.

[0099] Each cooling air feeder shell 130 is a tubular hollow structure comprising a metallic vertically-elongated body 131 defining a vertical centerline axis VC2 and bottom closure plate 132 welded to the bottom end 134 of the shell. The vertical centerlines VC2 and VC1 of the CECs 110 are parallel to each other. The body 131 may be cylindrical with a circular transverse cross-sectional shape in preferred non-limiting embodiments; however, other non-polygonal and polygonal shaped bodies may be used in certain other acceptable embodiments. The body 131 of each feeder shell defines an open vertical air passage 133 extending between the bottom end 134 and top end 135 of the shell 130 for drawing ambient cooling air downwards through the shell. The top end of shell 130 may terminate at the top surface 102a of the concrete top pad 102 in some embodiments. A perforated air intake housing 136 is coupled to the top end 135 of the shell 130 which projects vertically upwards from the top pad 102 as shown. In one embodiment, housing 136 may be formed of a cylindrical shell which is perforated to form a plurality of lateral openings extending 360 degrees circumferentially around for drawing air laterally into the feeder shell 130. A circular cap 137 encloses the top of the air inlet housing 136 to prevent the ingress of rain. The air feeder shell 130, bottom closure plate 132, air intake housing 136, and cap 137 may be formed of metal such as stainless steel for corrosion protection. Other shaped caps and intake housings may be used in other embodiments.

[0100] To minimize rising air leaving the top of the cavities 120 of the CECs 110 which has been heated by the canisters 150 from being drawn back into the intake housings 136 of the cooling air feeder shells 130, each feeder shell is preferably spaced apart from the shell bodies 101 of adjacent CECs by a sufficient lateral/horizontal distance such as at least one outer diameter D1 of feeder shell in some embodiments.

[0101] With continuing reference to FIGS. 4 and 5, cooling air feeder shells 130 have a height H1 which is at least coextensive as height H2 of CEC shell bodies 111. As one non-limiting example, H2 and H1 may be about 227 inches (576.6 cm). In one embodiment, shells 130 may have a slightly greater height H1 (measured between bottom and top ends 134, 135) than height H2 of the CEC shell bodies 111 (measured between bottom and top ends 113, 112 of the bodies in including upper portion 111a).

[0102] The canister 150 has a total height H3 (inclusive of the top and bottom closure plates 152, 153) less than height H2 of the CEC shell bodies 111 so that an air outlet plenum 154 is formed between the bottom of CEC lid 115 and the top closure plate 152 of the canister. The top of the canister defined by top closure plate 152 terminates beneath the concrete top pad 102 of the CIS system at an elevation that may fall within the vertical extent of the engineered fill 140. This helps prevent “sky shine” radiation streaming to the ambient environment.

[0103] Referring to FIGS. 1 and 2, the cavity enclosure containers 110 and cooling air feeder shells 130 in one embodiment may be arranged in a tightly packed array to minimize spatial site requirements at the CIS facility. The array comprises a plurality of longitudinally-extending and parallel linear nuclear waste storage rows R each including a plurality of CECs 110 and cooling air feeder shells 130. For convenience of illustration, the array in FIGS. 1-2 shows only five rows R; however, it is recognized that more or less rows of CECs and air feeder shells may of course be provided as needed. Each row defines a respective horizontally-extending longitudinal axis LA. The geometric centers of each CEC which intersect their vertical centerline axes VC1 intersect the respective longitudinal axis LA in each row such that the CECs 110 may be considered to be located on the longitudinal axis. For convenience of reference, a transverse axis TA may be defined as oriented perpendicularly to the longitudinal axis LA in each row extending front to back between rows R in the array (see, e.g., FIG. 2).

[0104] The nuclear waste storage rows R of CECs 110 are spaced apart and parallel to each other to form longitudinally-extending access aisles AI which provide access for commercially-available motorized wheeled or track driven lifting equipment such as without limitation cask crawlers or other equipment which transport, maneuver, and raise/lower the canisters 150 for insertion into and removal from the CECs 110. The equipment may straddle the row of CECs 110 and the wheels or tracks run in aisles AI on each side of the row. Such equipment is well known to those skilled in the art without further elaboration. The low exposed vertical profile of the CECs 110 (as further described herein) allows the equipment to move over the CECs modules in a single row to the desired CEC for inserting or removing canisters.

[0105] FIGS. 4-7 show a possible first embodiment and arrangement of CECs 110 and cooling air feeder shells 130. In this embodiment, each CEC 110 in each row R is fluidly coupled directly to a pair of cooling air feeder shells 130 by horizontally/laterally extending flow conduits 160; one each of feeder shells 130 being on opposite lateral sides of the CECs along the longitudinal axis LA as shown. Viewed the other way, each air feeder shell 130 may be considered centrally located between a pair of CECs. Each CEC therefore comprises a pair of air inlets 125 on opposite sides forming openings which extend through the shell body 111 of the CEC 110 to the internal cavity 120. The air inlets 125 are therefore formed in and through the lower portion 111d of the CECs (i.e. shell body 111) to introduce cooling air into the bottom of the CEC cavity 120 and ventilation annulus 121. In a preferred but non-limiting embodiment, the air inlets 125 are each configured and arranged to introduce cooling ventilation air tangentially into the cavity 120 of each CEC 110 as shown. Introduction of cooling air in this tangential manner which flows circumferentially around the inner surface of the CEC to quickly fill the CEC cavity and ventilation advantageously results in less pressure drop than introducing the air radially and perpendicularly at the canister shell 151.

[0106] The flow conduits 160 comprise sections of horizontally-extending metal piping spanning between the cooling air feeder shells 130 and their respective CECs 110. The flow conduits fluidly couple each CEC air inlet 125 “directly” to a respective air feeder shell 130 meaning that the cooling air passes from the feeder shell to the respective CEC without passing through any other CEC or feeder shell on the way. As previously described herein, this arrangement advantageously maximizes the amount of cooing air received by each CEC 110 commensurate with the level of heat emitted by the canisters in each CEC which may differ. Accordingly, no CEC is starved of its required cooling air flow by any upstream CEC. Because the CECs and their nuclear waste material contents are passively and convectively cooled via the natural thermo-siphon effect as previously described herein, pressure imbalances in the cooling air ventilation system which can adversely affect proper cooling of each CEC are avoided by the present cooling equipment arrangement. The provision of two air inlets 125 for each CEC 110 and separate sources of cooling air (i.e. feeder shells 130) for each inlet further ensures each CEC is cooled to remove the heat generated in its cavity to the maximum extent possible.

[0107] For the same foregoing reasons to ensure each CEC 110 receives the needed amount of cooling air based on its particular heat load generated by the nuclear waste canister 150 therein, it further bears noting that there is no interconnecting flow conduits between any CECs or cooling air feeder shells 130 in one row and any other rows R. Accordingly, each nuclear waste storage row R is fluidly isolated from every other row.

[0108] Although perhaps not readily apparent from the figures, it also bears noting that each CEC 110 in a single row R is fluidly isolated from adjacent CECs and every other CEC in the same row when the ambient air cooling ventilation system is in operation (i.e. nuclear waste canisters 150 disposed in the CECs thereby creating active air flow through the ventilation system via the thermo-siphon effect previously described herein). For example, referring to FIG. 4, ambient cooling air will be drawn downwards in the centrally located air feeder shell 130 and then flow laterally outwards to each of the two CECs 110 pictured via flow conduits 160 (see directional air flow arrows). The cool air enters the bottoms of the CECs and flows vertically upwards as the air in the CEC cavities 120 is heated by the canisters 150 (see, e.g., FIG. 2). Accordingly, given the direction of flow through these nuclear waste storage system components, air cannot possibly flow from one CEC 110 backwards through the centrally located air feeder shell 130 and into the remaining CEC. The CECs are therefore effectively fluidly isolated from each other.

[0109] As previously noted, the flow conduits 160 may comprise sections of metal piping such as stainless steel of suitable diameter. In preferred but non-limiting embodiments, the flow conduits are configured such that there is no straight line of sight between each cooling air feeder shell 130 and either of its respective pair of cavity enclosure containers 110 fluidly coupled thereto to prevent radiation streaming. This concomitantly also ensures there is no straight line of sight between any of the CECs 110 in the row R through the feeder shells 130. In one configuration, flow conduits 160 may each comprise an angled transverse section 162 oriented transversely to the longitudinal axis LA, and an adjoining longitudinal section 161 oriented parallel to the longitudinal axis. A welded mitered joint 163 may be formed between the transverse and longitudinal sections (see, e.g., FIG. 6). An oblique angle is formed between these two sections of the flow conduit. In other possible embodiments, curved piping elbows may be used instead of mitered sections of straight piping to prevent the straight line of sight.

[0110] Because each cooling air feeder shell 130 need only be sized in diameter to supply cooling air to a pair of CECs 110, the diameter of the feeder shells can be minimized to allow CECs in each row to be closely spaced. This advantageously allows more CECs and nuclear waste to be packed into each row R. Accordingly, in preferred but non-limiting embodiments, the outer diameter D1 of the feeder shells 130 may be smaller than the outer diameter D2 of the CECs 110. As one non-limiting example, D1 may be about 30 inches (76.2 cm) and D2 may be about 84 inches (213.4 cm). For size comparison, the flow conduits 60 may have a smaller diameter than D1 or D2; such as for example without limitation about 24 inches (61 cm) in one embodiment. Other diametrical sizes may be used in other embodiments and does not limit the invention.

[0111] To summarize operation of the nuclear waste storage system and ambient cooling air ventilation system, nuclear waste canisters 150 containing radioactive waste materials (e.g. SNF fuel assembly and/or other high level radioactive waste materials removed from the reactor) are loaded into the CECs 110. The lids 115 are then placed onto the CECs to enclose the CECs and their internal cavities.

[0112] With the canisters positioned inside the CECs and lids in place, air in the ventilation annulus 121 between the canister and shell body 111 of each CEC 110 becomes heated by the canister. The heated air rises, collects in the air outlet plenum 154 above the canister in cavity 120 of the CEC, and exits the CEC back to atmosphere through the air outlet 118 formed through the lid 115 of the CEC (see directional air flow arrows in FIGS. 4-5 and 18).

[0113] The upward convective flow of air inside cavity 120 of each CEC 110 creates a negative pressure which draws ambient air down into the cooling air feeder shell 130 via the known thermo-siphon effect or mechanism. The CEC draws the air from the bottom of the air feeder shell into the lower portion of its internal cavity 120 and ventilation annulus 121 through the flow conduits 160 to complete the ventilation air flow circuit. It bears noting that this natural air flow is unassisted by powered fans or blowers, thereby avoiding operating costs associated with electric power consumption, but importantly ensuring continued cooling of the CECs 110 in the event of power disruption to prevent overheating the CECs and protect the containment of the nuclear waste materials.

[0114] FIG. 20 depicts an alternative second embodiment and arrangement of a nuclear waste storage system and corresponding air ventilation system. In this embodiment, each CEC 110 is fluidly coupled to only a single cooling air feeder shell 130 by a pair of angled/curved flow conduits 160 to prevent radiation streaming as previously described herein. The CEC includes two air inlets 125 also arranged to introduce ventilation air tangentially into the internal cavity of the CEC. The bifurcated ventilation air supply effectively creates a curtain of cooling air around the nuclear waste canister 150 inside the CEC with minimal flow resistance to maximize the air flow for cooling the radioactive waste material. This alternative embodiment may be appropriate where certain canisters 150 are still emitting extremely high levels of thermal energy (heat) which must be dissipated in order to protect the structural integrity of the canister and nuclear waste therein. Multiple pairs of the fluidly isolated CECs 110 and cooling air feeder shells 130 in FIG. 20 may be arranged in a row R of the CIS facility. The CECs 110 and air feeder shells 130 are arranged on the longitudinal axis LA of each row R that may be provided in the array of CECs.

[0115] It bears noting that certain CIS facilities may combine some rows of CECs 110 and air feeder shells 130 according to the arrangement shown in FIG. 20 for high thermal energy emitting nuclear waste canisters, and some other rows of CECs and air feeder shells according to the arrangement shown in FIGS. 4-7 for lower thermal energy emitting nuclear waste canisters. In yet other embodiments, the two different arrangements of CECs and air feeder shells may be mixed in a single row R. Accordingly, numerous variations are possible depending on particular nuclear waste material storage needs and level of thermal energy emitted by the canisters 150.

[0116] FIGS. 1-3 and 8-19 depict yet another third alternative embodiment and arrangement of a nuclear waste storage system and corresponding air ventilation system. This a high airflow capacity configuration of the passively cooled nuclear waste storage system with thermo-siphon driven ventilation system suitable for radioactive nuclear waste emitting extremely high levels of heat that must be dissipated by ambient cooling air to protect the radioactive waste (e.g. SNF fuel assemblies, etc.) inside the nuclear waste canisters 150. The cooling air requirements of these high heat load CECs may exceed even the higher airflow capacity provided by the CECs in FIG. 20 with a dedicated separate pair of cooling air feeder shells 130 as shown.

[0117] Accordingly, CECs 110 in this high airflow capacity third embodiment may each be fluidly coupled to two pairs (i.e. four) cooling air feeder shells 130 by air flow conduits 160 (see, e.g., FIGS. 1-3 and 14). With continuing reference to FIGS. 1-3 and 8-19 generally, one pair of feeder shells 130 may be located on one lateral side of the CEC, and the remaining pair of feeder shells may be located on the opposite other lateral side as shown. The CEC includes four air inlets 125; each of which is fluidly coupled by a flow conduit 160 to one of the four cooling air feeder shells 130. The flow conduits 160 may be similarly configured and arranged to the prior embodiments of the ambient air ventilation system previously described herein to introduce ventilation air tangentially into the lower/bottom portion of internal cavity 120 of the CEC 110 in order to achieve the same airflow benefits noted above.

[0118] It bears noting that each CEC 110 in a single row R need not necessarily be coupled to four cooling air feeder shells 130 as seen in FIGS. 1-3. For example, one CEC 110 located at one end of row R is shown fluidly coupled to only a pair of cooling air feeder shells 130 as this CEC may not have a heat load as high as the heat loads of the remaining other CECs in the depicted row which require a higher ambient ventilation air flow volume or rate (e.g. CFM—cubic feet per minute) to dissipate the higher heat emissions from the canisters 150 stored therein. Accordingly, the present passively cooled nuclear waste storage and ventilation system offers considerable flexibility in configuration which can be customized in order to accommodate the particular heat load dissipation needs of the CECs which may differ.

[0119] With continuing general reference to FIGS. 1-3 and 8-19, the construction and structural details of the CECs 110 in this third embodiment and arrangement of passively-cooled nuclear waste storage system may be similar to the previously described embodiments with exception of the additional cooling air inlets 125 to accommodate the two pairs of cooling air feeder shells 130. The description of the CEC structure including lid 115 will therefore not be repeated here for sake of brevity. The features or parts of the CEC in the presently illustrated third embodiment of the nuclear waste storage system are therefore numbered the same as in the figures for the first and second embodiments.

[0120] In the present high air flow embodiment shown in FIGS. 1-3 and 8-19, the CECs 110 and cooling air feeder shells 130 however have been structurally integrated into a readily transportable and mountable modular nuclear waste storage unit 200 (best seen in FIGS. 8-16). The modular unit 200 is a self-supported and transportable assemblage or structure which includes a common or shared support plate 202 formed of a suitably strong and appropriate metallic material (e.g., stainless steel or other). The support plate 202 has a horizontally broadened and flat body 201 configured for mounting and anchoring onto the top surface of the subterranean concrete base pad 101 such as via anchors 103 which may be threaded fasteners or other type anchoring/mounting devices. One CEC 110 and a single pair of cooling air feeder shells 130 on one lateral side of the CEC are fixedly attached to the common or shared support plate 202 such as via welding. The support plate 202 may have any suitable configuration, such as a U-shaped mixed polygonal-non-polygonal configuration in one non-limiting embodiment as shown.

[0121] To ensure that the vertically tall shell body 111 of the CEC 110 and pair of cooling air feeder shells 130 are structurally stabilized and braced for lifting and transport as a single self-supporting unit, a plurality of horizontally-extending cross-support members 204 (e.g., structural beams of suitable shape) are provided which structurally ties the CEC shell body and feeder shells together in a rigid manner. In one embodiment (as variously appearing in FIGS. 8-16), the CEC 110 in each modular nuclear waste storage unit 200 is structurally tied and laterally braced to each of the pair of cooling air feeder shells 130 by a plurality of vertically spaced apart cross-support members 204. In the non-limiting illustrated embodiment, three cross-support members are shown to tie each of the lower portion 111d, middle portion 111e, and upper portion 111a of the CEC to each of the two feeder shells 130. More or less cross-support members 204 may be used. The pair of cooling air feeder shells 130 are similarly structurally tied together and laterally braced by vertically spaced apart cross-support members 204 which may be of the same type or different than the cross-support structural members tying the CEC 110 to each of the cooling air feeder shells 130. In one non-limiting embodiment, a W-beam may be used for cross-support structural members 204; however, other suitable type/shape structural members may be used.

[0122] The modular nuclear waste storage unit 200 advantageously allows the units to be fabricated under controlled shop conditions in the fabrication facility, and then shipped to the installation site (e.g., Consolidated Interim Storage facility). Since the CEC 110 and pair of cooling air feeder shells 130 are already palletized so to speak on the common support plate 201, installation requires only making the piping connections with the flow conduits 160 at the installation site. This results in rapid installation and deployment of the modular nuclear waste storage units.

[0123] To install the modular nuclear waste storage units 200 in the manner shown in FIG. 3 such as at a CIS site or facility, the installation process or method includes pouring the concrete base pad 101 and then positioning and mounting a first storage unit 200 on the pad when cured and hardened. A second storage unit 200 is next positioned and mounted on the base pad adjacent to the first storage unit in a longitudinally spaced apart manner along the row R. The piping connections can now be made for the first storage unit. Each of the four cooling air feeder shells 130 are then fluidly coupled directly to the CEC 110 of the first storage unit by a separate flow conduit 160. The piping connections between the CEC and feeder shells 160 may be welded or preferably bolted piping flange type connections which can be made more expediently than welded connections. Since the air flowing inside the flow conduits 160 is at most at air a slight negative (sub-atmospheric) pressure when the ventilation system is in operation, flanged type connections are suitable for these service conditions. The next additional third, fourth, so on nuclear waste storage units 200 may then be added and installed in a similar manner. Once all units have been mounted to the base pad 101 and fluidly coupled to their respective cooling air feeder shells 130, the flowable engineered fill 140 may be installed on top of the base pad and around the CECs and feeders shells of the CIS facility to fill the voids between this equipment for lateral support and radiation attenuation/blocking as shown in FIGS. 17-19 (note engineered fill not shown in FIG. 3 for clarity).

[0124] Next, the concrete top pad 102 may be formed on top of the engineered fill. The modular nuclear waste storage units 200 are now ready for receiving a nuclear waste canister 150 in each cavity 120. In some embodiments as disclosed in U.S. Pat. No. 9,852,822 which is incorporated herein by reference, a pair of canisters 150 may be vertically stacked in each CEC 110 and supported therein in the manner described. It bears noting that the CEC 110 whether holding a single or two vertically stacked canisters 150 has a cross-sectional area sufficient for holding only a single canister at a single elevation (i.e. no side-by-side canister placement).

[0125] It bears noting that in the preferred but non-limiting embodiment, the foregoing CECs 110 of the multiple modular nuclear waste storage units 200 are preferably positioned on the longitudinal axis LA of the storage row R (i.e. vertical centerline axis VC1 intersects longitudinal axis LA). This is similar to the previous two embodiments of the nuclear waste storage system 100 shown in FIGS. 4-7 and 20 described above. In the present embodiment shown in FIGS. 1-3, the first and second cooling air feeder shells 130 of the first pair of feeder shells may be transversely spaced apart perpendicularly to and on opposite sides of longitudinal axis LA). The first and second feeder shells are located on a first lateral side of a first CEC 110. The third and fourth cooling air feeder shells of the second pair of feeder shells may similarly be transversely spaced apart in the same manner and located on a second lateral side of the first CEC 110 opposite the first lateral side.

[0126] The first, second, third, and fourth cooling air feeder shells 130 are preferably fluidly coupled directly to the first CECs by separate metallic flow conduits 160 as shown in FIG. 3 (see also variously FIGS. 8-19). Accordingly, there are no intervening CECs or cooling air shells. Flow conduits 160 may be formed by sections of piping as previously described herein.

[0127] In the present third embodiment, the flow conduits 160 may each comprise a horizontally-extending straight piping section fluidly coupling a lower portion of the cavity 120 of the first CEC 110 to a lower portion of each of the cooling air feeder shells 130. Each straight piping section flow conduit 160 defines a horizontal centerline axis Hc which is acutely angled to longitudinal axis LA by angle A1 (see, e.g., FIG. 14). This angled arrangement of the cooling air feeder shells 130 to the longitudinal axis is sufficient to ensure there is no straight line of sight between the first CEC 110 and the next adjacent CEC which is mounted on a different support plate 201. In certain embodiments, angle A1 may be between about and including 10 to 20 degrees.

[0128] As also shown in FIG. 14, the cooling air feeder shells 130 in each pair on opposite lateral sides of the depicted CEC 110 are on opposite sides of longitudinal axis LA. The geometric vertical centerline VC2 of each of the feeder shells falls on a horizontal reference line R1 which is oriented at an acute angle A2 to the longitudinal axis LA of the nuclear waste storage row R. Angle A2 may be about 30 degrees (+/−5 degrees) in one embodiment as illustrated. It bears noting that the angular arrangement of the flow conduits 160 and cooling air feeder shells 130 to the longitudinal axis LA by angles A1 and A2 respectively advantageously contributes to allow closer spacing between the CECs 110 and feeder shells in each row. This allows more CECs to be tightly packed into each row R.

[0129] Referring to FIGS. 15-19, each cooling air feeder shell 130 in some embodiments may include an array 170 of vertically elongated radiation attenuator plates 171. The plates 171 may be flat, and are structurally coupled together (e.g. welded, via clips/brackets, etc.) and arranged in an orthogonal grid as shown. Plates 171 are disposed in the vertical air passage 133 of the cooling air feeder shells 130 and create vertically-extending grid openings between them through which the ventilation air is drawn downwards through the shells. Attenuator plates 171 may extend vertically for a majority of the H1 the cooling air feeder shells. In one embodiment, the attenuator plates extend vertically from top end 135 of the shells downwards towards bottom end 134 and terminate at a point just above and proximate to the top of the flow conduits 160 so as to not interfere with the ventilation air flow from the shells 130 to the CECs 110. In one embodiment, attenuator plates 171 may be formed of steel; however, other suitable materials including boron-containing materials and metals may be used. The attenuator plates 171 advantageously help prevent radiation streaming to the ambient environment surrounding the nuclear waste storage system.

[0130] In operation, the ambient cooling air ventilation system of the present high airflow capacity embodiment shown in FIGS. 1-3 and 8-19 functions and follows the same general path as the previously described embodiments. The air inlets 125 are each configured and arranged to introduce cooling ventilation air tangentially into the cavity 120 of each CEC 110 as shown. Ambient ventilation air is drawn downwards through and between the attenuator plates 171 inside each cooling air feeder shell 130, and then flows horizontal/laterally to the CEC 110 through flow conduits 160 to cool the canister 150 in each CEC via the convective natural thermo-siphon effect previously described herein.

[0131] In the present embodiment of FIGS. 1-3 and 8-19, an alternative air outlet 220 is shown which is formed directly through lid 215 rather than between the periphery of the lid and upper portion 111a of the CEC 110 and top pad 102 as with previous lid 115 in prior embodiments of FIGS. 4-7 described herein. In the present embodiment, the air outlet 220 forms a circuitous multi-angled passageway internally through the lid terminating in air discharge housing 216 mounted to the top surface of the lid (see, e.g., FIG. 18 and directional airflow arrows). To accommodate this internal air outlet 220 passage, lid 215 is configured slightly differently than lid 115 previously described herein.

[0132] Air discharge housing 216 of present lid 215 comprises a perforated cylindrical metal shell which projects vertically upwards from the top surface of the lid 215 as shown. In one embodiment, housing 216 comprises a plurality of lateral openings extending 360 degrees circumferentially around for discharging air laterally outwards therefrom back to the ambient environment. A circular cap 217 encloses the top of the air discharge housing 216 to prevent the ingress of rain. The air discharge housing 216 and to cap 217 may be formed of metal such as stainless steel for corrosion protection. Other shaped caps and intake housings may be used in other embodiments.

[0133] The present lid 215 may have a composite metal and concrete construction and shape similar to previous lid 115 in FIGS. 4-7 including an outer shell 215a formed of steel such as stainless steel, and interior concrete lining 215b. This robust construction not only provides radiation shielding, but also offers protection against projectile impacts. In one configuration, lid 215 includes a circular upper portion 218a and adjoining circular lower portion 218b having an outer diameter smaller than an outer diameter of the upper portion similar to previous lid 115. The present lid 215 effectively seals off the upwardly open recess 117 formed into the top surface 102a of the top pad 102 around the top end 112 of each CEC 110 by the upper diametrically enlarged top cylindrical section 111b of the CEC.

[0134] In cooling operation, air rising upwards within ventilation annulus 121 between the heat-emitting canister 150 and shell body 111 of CEC 110 flows to the bottom of lid 215 (see, e.g., FIG. 18 and directional airflow arrows). The air then flows radially outwards and then turns upwards around the periphery of the smaller diameter lower portion 218b of the lid within air outlet 220. The air then flows radially inwards and turns 90 degrees upwards towards the discharge housing 216. The heated air is discharged laterally and radially from housing 216 through the perforations back to ambient atmosphere. The cooling cycle operates continuations via the thermo-siphon as long as the nuclear waste canister 150 continues to emit heat generated by the nuclear waste inside.

[0135] Stackable Nuclear Waste Storage System

[0136] To address the need described above to increase storage capacity at existing or new below grade ISFSI facilities as described above with respect to FIGS. 1-20 or other storage facility, FIGS. 21-44 depict various aspects of a passively cooled and stackable nuclear waste storage system which provides both below grade and above grade storage.

[0137] Referring to FIGS. 21-44, the system comprises a pair of vertically stacked nuclear waste storage vessels including a lower below grade module and an upper above grade module. The below grade module may be one or more of the embodiments of the vertically elongated CEC 110 (cavity enclosure containers) previously described herein which is mounted on the subterranean concrete base pad 101 of the ISFSI and situated below the storage site's final cleared grade of topsoil and/or engineered fill. CEC 110 is passively cooled via the natural thermo-siphon ventilation system described above via one or more cooling air feeder shells 130 fluidly coupled to the internal storage cavity 120 of the CEC by one or more horizontal/lateral flow conduits 160. The lid 115 on the CEC is omitted and instead an above grade module is mounted immediately above the CEC.

[0138] The above grade module may be a vertically-elongated radiation-shielded cask 300 positioned above the below grade CEC 110. The stacked casks and CEC may be concentrically arranged with respect to one another and coaxially aligned along a common vertical centerline collectively defined by vertical centerline axis VC1 of CEC 110 and vertical centerline cask axis CA1 of cask 300 (see, e.g., FIG. 41). In one embodiment, the cask 300 may be fixedly and detachably mounted to the ISFSI top pad 102 such as via bolting or other means. There may be no direct fixed coupling via bolting or other means of the cask to the below grade CEC. In other possible embodiments, the cask 300 may be directly coupled to top of the CEC (e.g., bolted or otherwise) either instead of or in addition to mounting to the concrete top pad.

[0139] Because cask 300 is an above grade nuclear waste storage module, it is a heavily radiation-shielded double-walled vessel. A suitable basic cask usable in the stacked storage system may be a HI-STORM cask available from Holtec International of Camden, N.J. when is modified to include the unique features described herein for a stacked installation above the below grade CEC including the special cooling air ventilation provisions disclosed to fluidly interconnect the internal nuclear waste canister cavities of the CEC 110 and cask 300 thereby forming a fluidly contiguous internal space of the cooling air ventilation system as further described herein.

[0140] Cask 300 in one embodiment includes a vertically orientated and elongated cask body 310 having a greater height than width. The cask body is formed by a cylindrical outer shell 311 and inner shell 312, and radiation shielding material 313 disposed in an annular space formed therebetween. The shells 311, 312 and shielding material 313 collectively define a cylindrical vertical sidewall 318 of the cask having the foregoing composite construction of different materials. The inner and outer shells are concentrically arranged and coaxial relative to each other as shown.

[0141] In one embodiment, the shielding material 313 may comprise a concrete mass or liner for neutron and gamma radiation blocking. A concrete aggregate comprising hematite or another type iron ore preferably may be used. This advantageously maximizes conductive heat transfer through the sidewalls 318 of the cask body to help dissipate and transmit a portion of the thermal energy (e.g., heat) emitted by the SNF (or other radioactive waste) stored inside the casks within the canister. The passive ventilation air system described herein dissipates the remainder of the decay heat to protect the structural integrity of the canister and SNF assemblies stored therein. Other radiation shielding materials may be used in addition to or instead of concrete including lead for gamma radiation shielding, boron containing materials for neutron blocking (e.g. Metamic® or others), steel, and/or others shielding material typically used for such purposes in the art.

[0142] Inner shell 312 of the cask 300 defines an inner or internal surface 312a and outer shell 311 defines an outer or external surface 311a of the casks. Surfaces 311a, 312a formed by the cylindrical shells 311, 312 may correspondingly be cylindrical and arcuately curved in one embodiment. The cask further defines a top end 319 defined by the upper end of the cask body 310 and bottom end 320 defined by the lower end.

[0143] The inner and outer shells 312, 311 may be formed of a suitable metallic material, such as without limitation steel (e.g. carbon or stainless steel). If carbon steel is used at least the external surface 311a of the cask may be epoxy painted/coated for corrosion protection. The metal shells 311, 312 may each have representative thickness of about ¾ inches as one non-limiting example; however, other suitable thicknesses may be used.

[0144] Above grade cask 300 comprises a vertically-extending internal cavity 321 which extends along the vertical cavity axis CA1 defined by the cask body 318. Cask 300 is concentrically and coaxially aligned with vertical centerline axis VC1 of the CEC 110. Cavity 321 extends vertically for substantially the entire height of the cask. Cavity 321 may be of cylindrical configuration in one embodiment with a circular cross-sectional shape to conform to the cylindrical shape of the nuclear waste canister 150; however, other shaped cavities with corresponding cross-sectional shapes may be used including polygonal shapes and other non-polygonal shapes (e.g. rectilinear, hexagon, octagonal, etc.) depending on configuration of the nuclear waste container stored therein. The cavity of cask 300 may have a height and transverse cross-sectional area configured to hold only a single nuclear waste canister 150 loaded with SNF assemblies (not shown) or other high level radioactive waste emitting radiation and substantial amounts of thermal energy in the form of decay heat.

[0145] Cask 300 further comprises a bottom baseplate 315 which may be seal welded to the inner and outer shells 312, 311 at the bottom end 320 of the cask body. Structurally, this forms a rigid self-supporting cask assemblage or structure which can be fabricated in the shop, and then transported to the desired nuclear waste storage site (e.g., nuclear generating plant and/or ISFSI) where it can be moved and handled by suitable lifting equipment such as track-driven cask crawlers (used and are well known in the art). The cask crawlers are also used for loading the nuclear waste canisters into the casks. Baseplate 315 may be structurally reinforced and stiffened by a plurality of circumferentially spaced apart angled gusset plates 315b welded to the peripheral portion of the baseplate which projects radially outward beyond outer shell 311 and the lower portion of external surface 311a of outer shell 311 as shown. The peripheral portion of baseplate 315 defines a user-accessible mounting flange 350 for anchoring the cask to the concrete top pad 102.

[0146] Baseplate 315 of upper cask 300 is configured for placement and seating on a top surface of a substantially flat horizontal support structure such as the ISFSI concrete top pad 102 to rigidly and detachably anchor the cask 100a thereto. This laterally stabilizes the stacked cask assemblage to withstand vibrational loads and moments during a seismic event. Cask 300 directly engages top pad 102, and in some embodiments abuttingly engages the annular seating flange 111c at the top of the CEC 110 (see, e.g., FIGS. 36A-B). This forms an annular cask-to-CEC interface 448. It bears noting that baseplate 315 of cask 300 is not fixedly coupled to the CEC seating flange 111c (e.g., bolted, welded, etc.) since the flange 111c is not accessible being located to abutting engage only the inner annular bottom surface portion of the cask baseplate (best shown in FIG. 36B). The peripheral portion of baseplate 315 which defines the mounting flange 350 abuttingly engages and is fixedly coupled to the top surface of the concrete top pad 102 as shown. In one non-limiting embodiment, a plurality of circumferentially spaced apart threaded mounting fasteners 324 such as anchor bolts may embedded in concrete pad and arranged in a bolt circle may be used to fixedly anchor the peripheral mounting flange 350 defined by baseplate 315 of cask 300 in place such as via threaded nuts. Other forms of mounting the baseplate to the concrete pad may be used.

[0147] Baseplate 315 may be made of a similar metallic material as the shells 111, 112 (e.g., steel or stainless steel). The bottom surface of baseplate 315 may be considered to define the bottom end 320 of the cask 300 for convenience of description purposes.

[0148] Baseplate 315 comprises peripheral portion which projects radially outward beyond outer shell 311 and defines the mounting flange 350 as previously described herein. The baseplate 315 may be structurally reinforced and stiffened by a plurality of circumferentially spaced apart angled gusset plates 315b welded to the mounting flange and the lower portion of the external surface 311a of outer shell 311 of cask 300 as shown.

[0149] In an important aspect of the invention, baseplate 315 of upper cask 300 is a perforated baseplate comprising a plurality of perforations in the form of axial through holes 315a. The through holes may have a circular cross-sectional shape in one embodiment; however, other suitably shaped through holes in cross section such as polygonal (e.g., square, rectangular etc.) and non-polygonal shapes may be used. The through holes 315a are vertically elongated and may be oriented parallel to each other and vertical cavity axis CA1 of the cask. Preferably, only the central portion of the perforated baseplate 315 which resides inside the internal cavity 321 of the cask 300 includes the perforations (i.e. through holes 315a).

[0150] Baseplate 315 of the above grade upper cask 300 is structured to support the entire weight of the nuclear waste canister 150 stored in the cask. The perforated baseplate 315 of cask 300 provides a structural purpose and in addition functions as an integral part of the cask and CEC ventilation air system described herein which removes decay heat (thermal energy) emitted by the nuclear waste canisters 150 in the stacked storage assembly. The through holes 315a of perforated baseplate 315 places the cavity 321 of the cask in fluid communication with the cavity 120 of the lower grade CEC 110. The fluid communication is established by the act of mounting the upper cask above the CEC, which in effect forms a common fluidly interconnected and contiguous ventilation riser extending in a vertical direction internally through the stack of cask 300 and CEC 110. Because the top end of the below grade CEC 110 and its cavity 120 are upwardly open (when lid 115 is removed to mount cask 300 above), the perforated baseplate 315 forms the only physical barrier between the cavities of the lower CEC and upper cask. The through holes 215a in perforated baseplate 215 defines an air transmissible barrier or structure which permits ventilation air in the lower cavity 120 of CEC 110 to be transferred and flow upwards into the upper cavity 321 of cask 300. Operation of the ventilation system will be further described herein.

[0151] Perforated baseplate 315 of upper cask 300 further plays an important role in preventing radiation streaming or shine therethrough during the process of mounting the upper cask above the embedded lower CEC 110. After a nuclear waste canister 150 is loaded into cavity 321 of upper cask 300 while positioned on the concrete top pad 102 (as further described herein), the upper cask must be lifted off of the pad by a commercially-available cask crawler to position the cask on top of the lower CEC already seated elsewhere on the pad. While the upper cask is suspended in mid air, the potential for radiation streaming or shine from the nuclear waste inside the cask cavity through the perforated baseplate to the ambient environment is created. To combat this issue, the axial through holes 315a in baseplate 315 therefore have a profile with height to diameter ratio of at least 2:1, and preferably more than 3:1. The baseplate 215 therefore is a vertically thick metallic structure which may be about 6 inches thick or more for this purpose in some non-limiting embodiments. The vertically elongated through holes 215a act to scatter the radiation to prevent radiation streaming to the environment through the baseplate. To further enhance radiation scattering effectiveness of the elongated through holes, some or all of the through holes may be obliquely oriented to the cavity axis CA1 of the upper cask 300 instead of being parallel thereto.

[0152] In some embodiments, instead of a single monolithic unitary structure which can be provided, the perforated baseplate 315 of upper cask 300 alternatively may have a two-piece construction (see, e.g., FIGS. 34-36). This includes a circular central portion 315e located inside the cavity 321 (which is perforated with the axial through holes 315a previously described herein) for supporting the upper canister 150, and an outer annular portion formed by a flat annular bottom closure plate 315f welded to the bottom ends of the upper cask cylindrical outer and inner shells 311, 312. Closure plate 315f defines a central opening 315h which allows rising air from the lower below grade CEC 110 to flow through the perforated central portion 315e of the baseplate 315 into the internal cavity 321 of upper above grade cask 300. The bottom closure plate 315f may be considered part of the entire structure of the baseplate 315. It bears noting that bottom closure plate 315f defines the peripheral portion of baseplate 315, which in turn defines the mounting flange 450 for coupling the upper cask 300 to lower CEC 110.

[0153] The perforated central portion 315e of baseplate 315 may be supported by an inner portion of bottom closure plate 315f located inside cavity 321 of above grade cask 300 via an annular stepped shoulder 315g formed by an inward radial extension or protrusion of closure plate 315f in one embodiment. Central portion 315e may loosely engage the stepped shoulder 315g of bottom closure plate 315f to be removable, or alternatively may be welded. to outer closure plate 315f for rigid fixation thereto. For the former loose coupling mounting, the circular perforated central portion 315e may be inserted through the top end of upper cask 300 after the annular bottom closure plate 315f is welded to outer and inner shells 311, 312 of the cask body.

[0154] In one embodiment, the central portion 315e may be thicker in construction than the bottom closure plate 315f of upper cask 300 as depicted herein because the central portion supports the weight of the canister 150 in the cask (see, e.g., FIG. 21). In other possible constructions, the entire baseplate 315 may have a uniform thickness.

[0155] The circular central portion 315e of baseplate 315 may have a variety of structures whether a monolithic one-piece or two-piece construction of the baseplate is used. FIG. 35 depicts one embodiment of central portion 315e formed by a plurality of orthogonally arranged and intersecting metallic flat plates 315m which define the plurality of axial through holes 315a. The outside perimeter of this embodiment defines an imaginary circle which conforms to and is complementary configured to the circular transverse cross-sectional area defined by internal cavity 321 of the above grade cask 300 which receives the central portion. FIG. 36 depicts an alternative and preferably embodiment in which central portion 315e of baseplate 315 of the cask 300 is formed by a solid circular metallic plate through which the plurality of through holes 315a previously described herein are formed. This central portion 315e formed by a thick steel plate allows formation of the through holes 315a which may offer greater protection against radiation streaming or shine through the perforated baseplate 315 in some cases than the embodiment of FIG. 35. Other perforated structures may be used for central portion 315e so long as through holes of any suitable configuration are provided to fluidly interconnect cavity 120 of the below grade CEC 110 to cavity 321 of above grade cask 300.

[0156] In some embodiments, a plurality of spacer plates 315d may be rigidly attached (e.g., welded) to a top surface of the perforated baseplate 315 inside cavity 321 as shown in FIG. 35. The spacer plates may be distributed over and spaced apart across the baseplate. Any suitably shaped structural steel plates may be used to construct the spacer plates. The spacer plates 315d are configured to engage and elevate a bottom of the nuclear waste canister 150 above the perforated baseplate in the above grade cask 300. This advantageously allows ventilation air to circulate and flow beneath the canister to enhance cooling the nuclear waste therein. Spacer plates 315d may be about 6 inches high in some embodiments and are arranged in a plurality of orientations to each other to create radiation scattering which further prevent radiation streaming or shine through the perforated baseplate 315.

[0157] With continuing general reference to FIGS. 21-44, the internal cavities 120, 321 of both the lower CEC 110 and upper cask 300 each have a height and transverse cross-sectional are configured for holding no more than a nuclear waste canister 150 therein, as previously described herein. The diameter of each cavity is intentionally larger than the outer diameter of the fuel canister 150 by an amount (e.g., less than ⅓ the diameter of the canister) to form a respective ventilation annulus 121 (CEC 110) or 322 (cask 300) between the canister 150 and CEC shell body 111 or inner shell 312 of the cask within internal cavities 120 or 321, respectively (see, e.g. FIG. 36A). The radial width W1 of annulus 121 in lower CEC 110 and width W2 of annulus 322 in upper cask 300 are each preferably sufficient to draw heat generated by the nuclear waste within each canister 150 away from the canister as the cooling ventilation air flows upwards alongside the outer surface of the canisters as it is heated via a natural convective thermo-siphon effect. A typical ventilation annulus inside a CEC or cask may be in the range of about and including 2-6 inches in radial width as a non-limiting example depending on the estimated heat load generated by the fuel canister 150. The ventilation annulus is defined by and extends vertically for the full height of the canister in each of the CEC and cask, and may terminate at top proximate to the top ends of the internal cavities as shown (see, e.g., FIG. 21). Accordingly, the canister 150 has a height approaching the full height of the cavity of the CEC and cask, and at least greater than ¾th the height of its respective cavity in which it is housed. This lower portions of each ventilation annulus 121 and 322 in the CEC and cask are placed in fluid communication with ambient atmosphere via the air inlet ducts extending through the sidewalls of the CEC and cask, as further described elsewhere herein.

[0158] In one embodiment, the radial width W2 of ventilation annulus 322 in upper cask 300 is preferably larger than radial width W1 of the ventilation annulus 121 in lower CEC 110. Because the nuclear waste canisters 150 stored in the CEC and cask have the same diameter which is standardized, the larger radial width W2 of the upper cask is the result of the cavity 321 of the upper cask having a larger diameter D2 than the diameter D1 of cavity 120 in the lower CEC (see, e.g., FIG. 36A). The additional annulus 322 volume thus created in the cavity 321 of upper cask 300 can advantageously accommodate the additional volume of heated ventilation air received from the lower CEC 110 without compromising the ability of the upper annulus 322 to absorb the additional heat generated by the canister 150 in the upper cask. By contrast, the CEC 110 may have a smaller diameter D1 cavity 120 since it only draws the volume of ambient cooling air inwards through its air inlets 125 necessary to accommodate the heat load created by a single nuclear waste canister 150 inside the CEC.

[0159] As shown in FIGS. 29 and 36A, a cask-to-cask interface 448 is formed between the upper cask 300 and lower CEC 110. Specifically, the interface may be defined by the joint between the bottom mounting flange 350 of the upper cask defined by baseplate 315 and the top surface 102a of the top pad 102. It bears special note that nuclear waste canister 150 in the cavity 321 of upper cask 300 is positioned above the interface 448 (e.g., bottom end of canister), and conversely the canister 150 in the cavity 120 of lower CEC 110 is positioned below interface 448 (e.g., top end of canister). The prevents radiation shine or streaming through the cask-to-cask interface 448 from the casks radially outwards to the ambient environment.

[0160] A radiation-shielded closure lid 314 is detachably coupled to the top end 319 of the above grade upper cask 300. Reference is made in general to FIGS. 21-44 as applicable, and in particular FIG. 37 which shows the lid in greater and enlarged cross-sectional detail. Lid 314 closes the normally upwardly open cavity 321 of upper cask 300 when in place. Lid 314 may be a circular cylindrical structure comprising a hollow metal outer housing 314b defining an interior space filled with a radiation shielding material 314a such as a concrete plug or liner encased by the outer housing. Other shielding materials may be used in addition to or instead of concrete. Lid 314 provides radiation shielding in the vertical upward direction, whereas the concrete liner 313 disposed between the inner and outer shells 312, 311 of the cask body 318 provides radiation shielding in the lateral or horizontal direction. With exception of the concrete liner, the foregoing lid-related components are preferably all formed of a metal such as without limitation steel (e.g. carbon or stainless).

[0161] Housing 314b of lid 314 may include circular top cover plate 314b-1, circular bottom cover plate 314b-2, and a circumferentially-extending peripheral ring wall or shell 314b-3 extending vertically between the ring plate and top plate (see, e.g. FIG. 6). The top and bottom cover plates may be flat and the ring shell 314b-3 may be cylindrical in shape in a certain embodiment.

[0162] A plurality of circumferentially spaced apart cylindrical standoffs 441 may be provided which elevate the bottom cover plate 314b-2 of lid 314 above the top end 319 of the upper cask 300. This provides a vertical gap of annular configuration which extends circumferentially all around the lid between the bottom cover plate and the top end of the cask to define an air outlet duct 440 through the lid to atmosphere. The air outlet duct 440 may extend 360 degrees all around the lid 314 except for interruptions by the standoffs 441. An annular mesh screen 444 with open flow areas encloses the annular air outlet duct 340 to prevent the ingress of debris or other materials into the cask, while concomitantly allowing the heated ventilation air to exit the lid back to atmosphere.

[0163] A central air collection recess 314c is formed beneath bottom cover plate 314b-2 of lid 314 on the underside of the lid by gap created by the standoffs 441. Central air collection recess 314c is downwardly open to internal cavity 321 of cask 300 to receive the vertically rising ventilation air from the ventilation annulus 322 which is heated by the canister. The central air collection recess collects the heated ventilation air and directs the air radially outwards back to ambient atmosphere through the air outlet ducts 440.

[0164] Vertical stiffening plates 314d welded between the top and bottom cover plates through the concrete radiation shielding material 314a structurally stiffens the lid housing. In one embodiment, as best shown in FIG. 37, the stiffening plates are further configured and operable to detachably engage the top end 319 of the cask 300 to which the lid is mounted. For this purpose, the stiffening plates 314d may include a step-shaped cutout 314d-1 configured to engage the top end of the cask. The stiffening plates therefore serve to primarily support the full weight of the heavy radiation-shielded lid which is not imposed on the standoffs 441. The bottom cover plate 314b-2 may be welded to each of the standoffs which partially supports the weight of the lid.

[0165] The standoffs 441 may play a further role in detachably coupling the lid 314 to the upper cask 300. Although the heavy weight of the concrete-filled lid tends to keep the lid in place on the cask, it is desirable to provide additional securement in form of bolting the lid to the cask. For that purpose, a plurality of threaded lid bolts 442 may be provided each of which extends vertically through one standoff 441 and threadably engages a mating threaded socket 445 provided in the top end 319 of the cask 300. In one embodiment, each socket may be provided by a vertically oriented lid mounting plate 246 which is welded between inner and outer shells 312, 311 of the cask (see, e.g., FIG. 21). Each threaded socket is welded to its associated lid mounting plate which is embedded in the concrete radiation-shielding material 314a. Each standoff 441 includes a tubular access sleeve 443 which extends vertically through the radiation shielding material 314a of the lid 314 as shown to allow an operator to access the lid bolting.

[0166] Additional features of the passive ventilation air system used to cool the nuclear waste inside the above grade upper casks 300 will now be described.

[0167] The present nuclear waste storage system disclosed herein includes a natural circulation air ventilation system (i.e. unpowered by fans/blowers) for removing decay heat emitted from the canister 150 which holds the SNF or other high level radioactive waste. The cooling airflow provided by the ambient air surrounding the cask has flow driven by the natural convective thermo-siphon effect in which ventilation air within the ventilation annuluses 121 and 322 of the lower CEC 110 and upper cask 300 is heated by the canisters 150 therein which emit the heat generated by the decaying SNF or other radioactive waste stored inside. This air heating generates an upflow of the heated air within each respective ventilation annulus. This natural convection driven airflow effect is well understood in the art without further elaboration.

[0168] Referring generally to FIGS. 21-44 as applicable, the cask ventilation provisions of the upper cask 300 include a plurality of circumferentially spaced apart ventilation air inlet ducts 420 configured to draw in and introduce ambient ventilation air radially inwards into the internal cavity 321 of the cask. Air inlet ducts 420 establish fluid communication between cask cavity 321 (including ventilation annulus 322 formed in the cavity between canister 150 and inner shell 312 of the cask body 310) and ambient atmosphere which provides the source of the cooling air.

[0169] The air inlet ducts 420 may be circumferentially spaced apart around the perimeter/circumference of upper cask 300. The inlet ducts 300 may be equally or unequally spaced apart and may include at least four ducts to deliver ambient cooling air to each quadrant of the nuclear waste canister 150 contained in internal cavity 321 of upper cask 300. In the illustrated embodiment, each quadrant of the canister is cooled by a pair of inlet ducts 420 (i.e. 8 ducts total).

[0170] In one non-limiting preferred embodiment, the air inlet ducts 420 are disposed in and formed through the lower portion of the upper cask body 310 proximate to the bottom end 320 of the cask and cavity 321 therein to introduce ambient cooling or ventilation air into the lower portion of the cavity and upper ventilation annulus 322 of the upper cask 300. Accordingly, each air inlet duct 420 extends horizontally/laterally and radially completely through the sidewall 318 formed by the cask body 310 from outer shell 311 to inner shell 312. The radially oriented ducts 420 define air inlet passageways which place the lower portion of the cask cavity 321 and ventilation annulus 322 of upper cask 300 in fluid communication with ambient atmosphere and cooling air.

[0171] Air inlet ducts 210 of upper cask 100b introduces fresh cool ambient ventilation air radially inwards into the upper cask cavity 321 where it mixes with already heated ventilation air flowing vertically upwards from the lower CEC 110 into the upper cask cavity. Advantageously, this mixing of air streams tempers and cools the rising heated ventilation air from the lower CEC so that it is better able to absorb heat emitted by the nuclear waste canister 150 inside the upper cask 300. The stacked assemblage of the lower CEC 110 and upper cask 300 therefore are cooled by two vertically spaced apart sets of air inlets; air inlets 125 of CEC 110 being below grade and air inlet ducts 420 of cask 300 being above grade. This provides adequate cooling capacity for the heat load generated by the thermal energy emissions for both nuclear waste canisters 101 accommodated by the nuclear waste storage system.

[0172] The air inlet ducts 420 of the upper cask 300 each include an entrance opening 411 located at and penetrating the outer or external surface 311a of the upper cask outer shell 311 and an exit opening 412 located at and penetrating the inner or internal surface 312a of inner shell 311. A metallic flow conduit 413 of suitable configuration extends between and fluidly couples the entrance and exit of each inlet duct. The flow conduits 413 may have any suitable configuration and polygonal or non-polygonal cross-sectional shape. In one embodiment, as shown, the flow conduits may have a box-like configuration with a rectilinear cross-sectional shape (e.g., rectangular or square). Air inlet ducts 420 of upper cask 300 may be vertically elongated in configuration n one non-limiting embodiment.

[0173] Each flow conduit 413 of the upper air inlet ducts 420 extends radially through the sidewall 318 of the cask body 310 (i.e. shells 311, 312 and radiation shielding material 313 therebetween) to fluidly connect ambient air to the internal cavity 321 and ventilation annulus 322 of the upper cask 300 (see, e.g., The flow conduit 313 may therefore be embedded within the radiation-shielding material liner of the upper cask 100b.

[0174] To prevent radiation streaming from the SNF or other radioactive waste stored inside the canister 150 when disposed in upper cask 300 to the ambient environment through the inlet ducts 420, each inlet duct may have a circuitous configuration to draw ambient ventilation air radially inwards into the cask cavity 321 in a circuitous path such that no straight line of sight exists between external entrance opening 201 and the internal exit opening 212 of each air inlet duct. To provide such a circuitous configuration, the entrance opening 211 may be radially and angularly offset from exit opening 212 of the duct. In one non-limiting example, the entrance opening 211 may be located at a first angular position defined by a radial reference line R1 and the exit opening 212 may be located at a second angular position defined by a second radial reference line R2 (see, e.g., FIG. 44). The entrance and exit openings 411, 412 may be angularly offset at an angle A1 between about and including 20 to 40 degrees. Angle A1 may be about 30 degrees in one preferred but non-limiting embodiment. The flow conduit 413 located therebetween extends transversely to radial references lines R1 and R2 through the radiation-shielding material 313 liner of the upper cask body 310 as shown to fluidly coupled the entrance and exit openings. The foregoing configuration and arrangement eliminates any straight line of sight through the upper set of air inlet ducts 420.

[0175] In operation of the passive ventilation air cooling system, air residing inside the ventilation annulus 121 of the below grade lower CEC 110 between the canister 150 and CEC shell body 111 is heated by the thermal energy emitted by the canister (i.e. nuclear waste container therein). The heated ventilation cooling air rises flowing vertically upwards within the annulus to the open top end of the lower CEC. Due to the natural convective thermo-siphon effect, the rising heated ventilation air concurrently draws available ambient cooling air from above grade surrounding the CEC vertically downwards via cooling air feeder shell(s) 130, then laterally/horizontally to the CEC air inlets 125 in the manner previously described herein. The cool ambient air flow radially inwards through the air inlets 125 adjacent to the bottom of the CEC cavity 120 into the CEC.

[0176] Concurrently, air residing inside the ventilation annulus 322 of the above grade upper cask 300 between its canister 150 and inner shell 312 is heated by the thermal energy emitted by the canister (i.e. nuclear waste container therein). This heated ventilation air inside upper cask 300 rises flowing vertically upwards within the annulus to the top end of the upper cask beneath the lid 314. Due to the natural convective thermo-siphon effect, the rising heated ventilation air concurrently draws available ambient cooling air surrounding the cask radially inwards through its set of air inlet ducts 420 adjacent to the bottom of the upper cask 300.

[0177] The process continues with the rising heated ventilation air in the lower CEC 110 which leaves the lower CEC and flows through the through holes 315a of the upper cask perforated baseplate 315 to enter the bottom of the ventilation annulus 322 inside upper cask 300. This heated ventilation air mixes with cool ambient air drawn into the upper cask via the set of air inlet ducts 420 as previously described herein. The mixed air is further heated by the canister 150 in the upper cask 300 as noted above. The further heated ventilation air continues to flow upwards and reaches the top end of the upper cask from which it is discharged back to atmosphere through the annular air outlet duct 440 defined by top closure lid 314 on the cask. This ventilation air circulation pattern continues indefinitely as long as the canisters emit some degree of heat.

[0178] Deployment of Stackable Nuclear Waste Storage System

[0179] There are at least two deployment scenarios in which the stackable nuclear waste storage system may be used to store nuclear waste at an ISFSI or other site. A method or process for storing nuclear waste will now be summarized with respect to these scenarios and variations thereof.

[0180] In a first deployment scenario, one or more below grade CECs 110 alone may be used at a first point in time for a period of time until additional nuclear waste storage capacity is required in the future at the storage site. The mounting of the lower CECs and later upper casks 300 into the tiered assemblage disclosed herein is therefore intended to be staggered over time instead of during the same in installation sequence as in the second deployment scenario described below. Each lower CEC of the stacked storage modules may be buried and positioned at a discrete location on the concrete pad S of the storage facility (see, e.g., FIGS. 1-3). The cooling air feeder shells 130 and flow conduits 160 associated with each CEC 110 are fluidly coupled to their respective one or more CECs as previously described herein.

[0181] With the CECs 110 each embedded in the concrete top pad 102 and engineered fill 140, a first nuclear waste canister 150 is lowered and inserted into each CEC internal cavity 120. The canister 150 is in a dry condition and may be loaded into cask 100a via a commercially-available transfer cask which is a lighter vessel with thinner walls providing less radiation shielding (sidewalls without concrete) than heavier thick walled storage casks with concrete sidewalls such as lower and upper casks 100a, 100b. Transfer casks are typically submerged in the fuel pool with a nuclear waste canister (e.g., MPC) pre-loaded therein, which is then with SNF assemblies in a known manner. The canisters are in a wetted condition inside the transfer cask rather than a dry condition such as when canisters 101 disclosed herein are loaded into the lower and upper casks 100a, 100b. Examples transfer casks which may be used are disclosed in commonly-owned U.S. Pat. Nos. 9,466,400 and 7,330,525, which are incorporated herein by reference in their entireties. Transfer casks may also be used to load the canister into the upper cask 300 described below.

[0182] With the canister now emplaced, a CEC lid 115 is then positioned on and mounted on top of the CEC in the same manner described above.

[0183] With the canister 150 now positioned in the CEC and lid in place, the thermo-siphon ventilation air system becomes activated due to the heat generated by the canister inside. Cool ambient ventilation air is drawn through the one or more cooling air feeder shells 130 and flow conduits 160 into the CEC cavity 120 via the air inlets 125. The cooling air is heated by the thermal energy emitted from nuclear waste in the canister and rises upwards through the ventilation annulus 121 of the CEC, and is then returned to atmosphere as heated ventilation air through the air outlet 118 defined by the lid 115 as previously described herein. The method includes operating the CEC 110 for a period of time to store and cool the radioactive waste in the CEC.

[0184] At a second point in time (later than the first point in time such as for example days, weeks, months, or years later), additional storage capacity may be added as required by installing one or more upper casks 300 on some or all of the lower CECs 110 previously installed at the nuclear waste storage site. An empty and upwardly open upper cask 300 is first positioned on concrete top pad 102 in a temporary staging area. A second canister 150 is loaded and inserted into the upper cask. The lid 115 on the lower CEC 110 may be removed leaving an upwardly open vessel. The upper cask 300 may then be lifted and positioned over and above the corresponding below grade CEC and bolted to the top pad 102. The perforated baseplate 315 of upper cask may abuttingly engage the upper annular seating flange 111c of the CEC on the top surface 102a of top pad 102 (see, e.g., FIG. 36B), but is not bolted or otherwise fixedly coupled thereto in any manner. The mutual engagement is one of a flat-to-flat interface and seal at this cask-to-CEC interface 448. The cask lid 314 may then be installed and bolted on the top end 319 of the upper cask 300 either while the cask is still on top pad 102 after loading the second canister 150 therein and before lifting, or after the cask is positioned on the top pad above the CEC.

[0185] With the canister 150 now positioned in the upper cask 300 and its lid in place, the air ventilation system is activated which for the upper cask includes a combined thermo-siphon effect and venturi effect. The thermo-siphon effect is triggered by heat generated by the canister inside the cask as previously described herein. The venturi effect is triggered by the velocity of the rising and upward flowing heated stream received in the upper cask cavity 321 from the lower CEC 110 below. Cool ambient air drawn through the upper air inlet ducts 420 via the venturi effect in part and thermo-siphon in part rises upwards through the ventilation annulus 322 of the upper cask 300, and is then returned to atmosphere as further heated ventilation air through the air outlet ducts 440 defined by the lid 314. In addition, the ventilation air introduced into the upper cask via the upper air inlet ducts 320 of the cask system is mixed in the ventilation annulus 322 with the already heated ventilation received from the lower CEC 110, as previously described herein. The combined and mixed ventilation air streams are thus discharged together from the lid on the upper cask.

[0186] In a second deployment scenario of the stackable nuclear waste storage system, both the lower CEC 110 and upper cask 300 may be installed at the storage site (e.g., ISFSI) contemporaneously at the same point in time initially. The method or process includes positioning the CEC 110 on the concrete base pad 101, preferably anchoring the CEC to the pad to provide stability, and then loading/inserting the first nuclear waste canister 150 therein.

[0187] The method or process continues in the same manner previously described above for the first deployment scenario until the upper cask 300 is mounted on top pad 102 with lid in place above the CEC 110 to establish fluid communication between the internal cavities 321 and 120 through the perforated baseplate 315.

[0188] Numerous other variations in the sequence and/or methods described above with respect to each deployment scenario may be used.

[0189] It bears noting that the cask body 310 of the above grade upper cask 300 is free of any air outlets (i.e. sidewall 318). The air outlet 440 is instead defined by the cask lid 314. It also bears noting that the shell body 111 of the below grade CEC 110 is free of any air outlets. The air outlet 118 instead is defined by the CEC lid 115 but only when the CEC is used alone before the upper cask 300 is mounted above and fluidly coupled to the CEC.

[0190] While the foregoing description and drawings represent exemplary embodiments of the present disclosure, it will be understood that various additions, modifications and substitutions may be made therein without departing from the spirit and scope and range of equivalents of the accompanying claims. In particular, it will be clear to those skilled in the art that the present invention may be embodied in other forms, structures, arrangements, proportions, sizes, and with other elements, materials, and components, without departing from the spirit or essential characteristics thereof. In addition, numerous variations in the methods/processes described herein may be made within the scope of the present disclosure. One skilled in the art will further appreciate that the embodiments may be used with many modifications of structure, arrangement, proportions, sizes, materials, and components and otherwise, used in the practice of the disclosure, which are particularly adapted to specific environments and operative requirements without departing from the principles described herein. The presently disclosed embodiments are therefore to be considered in all respects as illustrative and not restrictive. The appended claims should be construed broadly, to include other variants and embodiments of the disclosure, which may be made by those skilled in the art without departing from the scope and range of equivalents.