Patent Number: 
Section: claims

1. A system for storing nuclear fuel assemblies, comprising:a support structure;a plurality of cells located within the support structure, wherein the plurality of cells comprise a first cell configured to house a first fuel assembly and a second cell configured to house a second fuel assembly;a plurality of compartments separating and forming substantially an entire space between the plurality of cells and configured to provide passageways for coolant entering a bottom end of the support structure to remove heat from the nuclear fuel assemblies;a first perforation configured to transfer coolant between the first cell and one or more of the compartments; anda second perforation configured to transfer coolant between the second cell and the one or more compartments, wherein at least a portion of the coolant entering the bottom end of the support structure and travelling towards a top end of the support structure is transferred between the plurality of cells and the plurality of compartments. 2. The system of claim 1, wherein the first perforation is located at a first position adjacent a compartment separating the first cell from the second cell, wherein the second perforation is located at a second position adjacent the compartment, and wherein the second position is offset from the first position so that the first perforation and the second perforation do not provide a line-of-sight between the first fuel assembly and the second fuel assembly. 3. The system of claim 2, wherein the plurality of cells are arranged in a grid pattern associated with an X-Y plane, wherein the plurality of fuel cells are configured to store the plurality of fuel assemblies in a Z direction normal to the X-Y plane, and wherein the plurality of compartments comprise:a first set of compartments having a cross-sectional length oriented in the X direction of the X-Y plane extending substantially an entire X direction length of the cells;a second set of compartments having a cross-sectional length oriented in the Y direction of the X-Y plane extending substantially an entire X direction length of the cells; andthe first and second compartments have a cross-sectional length in the Z direction substantially an entire length of the fuel assemblies. 4. The system of claim 3, further comprising a third perforation configured to transfer coolant between one or more of the first set of compartments and one or more of the second set of compartments. 5. The system of claim 3, wherein the second position is offset from the first position in the X-Y plane. 6. The system of claim 3, wherein the second position is offset from the first position in the Z direction. 7. The system of claim 1, further comprising a number of multiple heat sinks attached to the support structure and configured to radiate heat away from the fuel assemblies. 8. The system of claim 1, wherein the support structure comprises:a first storage rack comprising a first set of cells configured to house a first group of fuel assemblies, including the first cell and the first fuel assembly; anda second storage rack mounted on top of the first storage rack and comprising a second set of cells configured to house a second group of fuel assemblies, wherein the second set of cells includes an upper cell located directly above the first cell, and wherein the upper cell is configured as a through-channel to provide substantially unimpeded flow of coolant from the first cell. 9. The system of claim 8, wherein an upper fuel assembly housed in the second set of cells is located directly above an empty cell of the first storage rack, and wherein the empty cell provides an additional through-channel to provide substantially unimpeded flow of coolant from the empty cell to the upper fuel assembly. 10. The system of claim 9, further comprising:a sensor configured to monitor when a level of coolant at least partially surrounding the support structure falls beneath a minimum threshold; anda ventilation system configured to direct air into the additional through-channel to cool the upper fuel assembly in response to the monitored level of coolant falling beneath the minimum threshold. 11. A system for storing nuclear fuel assemblies, comprising:a support structure;a plurality of cells located within the support structure configured to individually house the nuclear fuel assemblies; anda plurality of compartments separating the plurality of cells and configured to provide passageways for coolant entering a bottom end of the support structure to remove heat from the nuclear fuel assemblies,wherein the plurality of cells are arranged in a grid pattern associated with an X-Y plane, wherein the plurality of fuel cells are configured to store the plurality of fuel assemblies in a Z direction normal to the X-Y plane, and wherein the plurality of compartments comprise:a first set of compartments having a cross-sectional length oriented in the X direction of the X-Y plane extending substantially an entire X direction length of the cells;a second set of compartments having a cross-sectional length oriented in the Y direction of the X-Y plane extending substantially an entire Y direction length of the cells; andthe first and second compartments having a cross-sectional length oriented in the Z direction extending substantially an entire Z direction length of the fuel assemblies. 12. The system of claim 11 wherein the compartments form an entire space between the plurality of cells. 13. The system of claim 11, wherein a first one of the perforations is located at a first position adjacent a compartment separating the first cell from the second cell, wherein a second one of the perforations is located at a second position adjacent the compartment, and wherein the second position is offset from the first position so that the first perforation and the second perforation do not provide a line-of-sight between the first fuel assembly and the second fuel assembly. 14. The system of claim 13, wherein a third one of the perforations is configured to transfer coolant between one or more of the first set of compartments and one or more of the second set of compartments. 15. The system of claim 13, wherein the second position is offset from the first position in the X-Y plane. 16. The system of claim 13, wherein the second position is offset from the first position in the Z direction. 17. The system of claim 11, further comprising multiple heat sinks attached to the support structure and configured to radiate heat away from the fuel assemblies.