Patent Number: 053944496
Section: claims

1. An impact limiter for a nuclear fuel transportation cask comprising: an annular body having an inner periphery defined by an inner shell that mates with the transportation cask and an outer periphery defined by an outer shell that is non-circular, the annular body including an impact absorbing material between the inner shell and the outer shell; and  a tapered cap projecting from the annular body, said tapered cap having an outer periphery defined by an outer shell that is non-circular, the tapered cap including an impact absorbing material within the outer shell. 2. The impact limiter of claim 1, wherein the outer shell of the annular body is multisided. 3. The impact limiter of claim 2, wherein the multisided outer shell of the annular body has four primary sides and four secondary sides arranged in an alternating pattern. 4. The impact limiter of claim 3, wherein the primary sides are larger in surface area than the secondary sides. 5. The impact limiter of claim 1, wherein the outer shell of the tapered cap is multisided. 6. The impact limiter of claim 5, wherein the multisided outer shell of the tapered cap includes four primary sides and four secondary sides arranged in an alternating pattern. 7. The impact limiter of claim 6, wherein the primary sides are larger in surface area than the secondary sides. 8. The impact limiter of claim 1, wherein the impact absorbing material between the inner shell and the outer shell of the annular body exhibits substantially isotropic crush characteristics in a predetermined plane. 9. The impact limiter of claim 8, wherein the impact absorbing material in the annular body is an aluminum honeycomb with cross-laminated corrugations. 10. The impact limiter of claim 9, wherein the aluminum honeycomb is arranged in multiple layers, each layer including a plurality of blocks formed from the aluminum honeycomb with cross-laminated corrugations. 11. The impact limiter of claim 10, wherein the outer periphery of two discrete layers of the aluminum honeycomb are spaced apart from the inner periphery of the outer shell of the annular body and the outer periphery of two other discrete layers contact the inner periphery of the outer shell of the annular body. 12. The impact limiter of claim 1, wherein the impact absorbing material of the tapered cap comprises a foam material. 13. The impact limiter of claim 12, wherein the foam material is a closed cell polyurethane foam. 14. The impact limiter of claim 12, wherein the foam contacts the inner surface of the outer shell, the surface of contact being free of adhesion between the foam and the outer shell. 15. The impact limiter of claim 12, wherein the foam and the impact absorbing material of the annular body are separated by a separating plate, the foam contacting the separating plate along a contact surface, the contact surface being substantially free of adhesion between the foam and the separating plate. 16. The impact limiter of claim 12, further comprising a spacer for reducing heat transfer from the transportation cask to the foam material. 17. The impact limiter of claim 1, further comprising a shear stop for opposing a force applied to the impact absorbing material within the outer shell and preventing shearing of the impact absorbing material within the outer shell from the impact absorbing material between the inner shell and the outer shell.