Patent Number: 
Section: claims

1. A shock-absorbing device for a fuel assembly including a plurality of fuel rods, the shock-absorbing device comprising:a first nozzle and a second nozzle including one surfaces, respectively, by which the plurality of fuel rods are sandwiched, the first and second nozzles including other surfaces having a plurality of legs for defining first and second depressions, respectively;a nozzle support fitted to a center portion of the first depression of the first nozzle, the nozzle support being comprised of iron, aluminum alloy containing boron)(B10), stainless steel, lead, or concrete so that radiation from the fuel assembly is shielded; anda buffer combined with the nozzle support, the buffer having stiffness in a longitudinal direction of the fuel rods being equal to or less than that of the nozzle support, whereinthe nozzle support and the buffer are arranged in sequence along the longitudinal direction of the fuel rods as separating from the depressions and whereinthe buffer is either one of the followings (a) to (g):(a) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member;(b) a buffer including a bottom plate and a plurality of plate materials fitted to the bottom plate;(c) a buffer including a bottom plate and a plurality of rod members arranged with an axial direction being parallel to the longitudinal direction of the fuel rods;(d) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member, the casing being coupled with a pipe for housing the plurality of fuel rods by a coupling member (33);(e) a buffer including a first buffer that is provided with a depression and contacts the plurality of legs and a second buffer that is provided on the depression and contacts the nozzle support;(f) a buffer including a first buffer that contacts the plurality of legs and a second buffer that is provided with a salient and contacts the nozzle support at the salient, the first buffer having stiffness in a compression direction lower than that of the second buffer in the compression direction;(g) a buffer that has a depression and contacts the nozzle support at the depression, the buffer contacting the plurality of legs. 2. The shock-absorbing device for a fuel assembly according to claim 1, whereinthe first nozzle is arranged on a bottom side of a fuel assembly housing container for transporting the fuel assembly. 3. The shock-absorbing device for a fuel assembly according to claim 1, whereinthe second nozzle is arranged at an opening side of a fuel assembly housing container for transporting the fuel assembly. 4. A fuel assembly housing container comprising:a body that is a container with a bottom and houses a fuel assembly in an internal space thereof; andthe shock-absorbing device for a fuel assembly according to claim 1, which is arranged at least on a bottom of the body. 5. The fuel assembly housing container according to claim 4, wherein the shock-absorbing device for a fuel assembly according to claim 1 is arranged on a lid fitted to an opening of the internal space. 6. A shock-absorbing device for a fuel assembly including a plurality of fuel rods, the shock-absorbing device comprising:a first nozzle and a second nozzle including one surfaces, respectively, by which the plurality of fuel rods are sandwiched, the first and second nozzles including other surfaces having a plurality of legs for defining first and second depressions, respectively;a nozzle support fitted to a center portion of the second depression of the second nozzle, the nozzle support being comprised of iron, aluminum alloy containing boron)(B10), stainless steel, lead, or concrete so that radiation from the fuel assembly is shielded; anda buffer combined with the nozzle support, the buffer having stiffness combined with the first nozzle and the second nozzle in a longitudinal direction of the fuel rods being equal to or less than that of the nozzle support, whereinthe nozzle support and the buffer are arranged in sequence along the longitudinal direction of the fuel rods as separating from the depressions and whereinthe buffer is either one of the followings (a) to (g):(a) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member;(b) a buffer including a bottom plate and a plurality of plate materials fitted to the bottom plate;(c) a buffer including a bottom plate and a plurality of rod members arranged with an axial direction being parallel to the longitudinal direction of the fuel rods;(d) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member (11I), the casing being coupled with a pipe for housing the plurality of fuel rods by a coupling member;(e) a buffer including a first buffer that is provided with a depression and contacts the plurality of legs and a second buffer that is provided on the depression and contacts the nozzle support;(f) a buffer including a first buffer that contacts the plurality of legs and a second buffer that is provided with a salient and contacts the nozzle support at the salient, the first buffer having stiffness in a compression direction lower than that of the second buffer in the compression direction;(g) a buffer that has a depression and contacts the nozzle support at the depression, the buffer contacting the plurality of legs. 7. A shock-absorbing device for a fuel assembly including a plurality of fuel rods, the shock-absorbing device comprising:a first nozzle and a second nozzle, the first and second nozzles including one surfaces, respectively, by which the plurality of fuel rods are sandwiched and the first and second nozzles including other surfaces having a plurality of legs for defining first and second depressions, respectively;first and second nozzle supports fitted to a center portion of the first depression of the first nozzle and a center portion of the second depression of the second nozzle, respectively, the first and second nozzle supports being comprised of iron, aluminum alloy containing boron (B10), stainless steel, lead, or concrete so that radiation from the fuel assembly is shielded; andfirst and second buffers combined with the first and second nozzle supports, respectively, the first and second buffers having stiffness in a longitudinal direction of the fuel rods being equal to or less than that of the first and second nozzle supports, respectively, whereinthe first nozzle support and the first buffer are arranged in sequence along the longitudinal direction of the fuel rods as separating from the first depression and the second nozzle support and the second buffer are arranged in sequence along the longitudinal direction of the fuel rods as separating from the second depression and whereinthe first and second buffers are selected from either one of the followings (a) to (g):(a) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member;(b) a buffer including a bottom plate and a plurality of plate materials fitted to the bottom plate (11B);(c) a buffer including a bottom plate and a plurality of rod members arranged with an axial direction being parallel to the longitudinal direction of the fuel rods;(d) a buffer including a buffer member including a hydrogen-containing resin so as to shield neutron and a casing holding and surrounding the buffer member, the casing being coupled with a pipe for housing the plurality of fuel rods by a coupling member;(e) a buffer including a first buffer that is provided with a depression and contacts the plurality of legs and a second buffer that is provided on the depression and contacts the nozzle support;(f) a buffer including a first buffer that contacts the plurality of legs and a second buffer that is provided with a salient and contacts the nozzle support at the salient, the first buffer having stiffness in a compression direction lower than that of the second buffer in the compression direction;(g) a buffer that has a depression and contacts the nozzle support at the depression, the buffer contacting the plurality of legs. 8. The shock-absorbing device for a fuel assembly according to claim 7, whereinthe first nozzle is arranged on a bottom side of a fuel assembly housing container for transporting the fuel assembly. 9. The shock-absorbing device for a fuel assembly according to claim 7, whereinthe second nozzle is arranged at an opening side of a fuel assembly housing container for transporting the fuel assembly. 10. A fuel assembly housing container comprising:a body that is a container with a bottom and houses a fuel assembly in an internal space thereof; andthe shock-absorbing device for a fuel assembly according to claim 7, which is arranged at least on a bottom of the body. 11. The fuel assembly housing container according to claim 10, wherein the shock-absorbing device for a fuel assembly is arranged on a lid fitted to an opening of the internal space.