Classifications

• • G—PHYSICS
  • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
  • G21F—PROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
  • G21F5/00—Transportable or portable shielded containers
  • G21F5/06—Details of, or accessories to, the containers
  • G21F5/10—Heat-removal systems, e.g. using circulating fluid or cooling fins
• • G—PHYSICS
  • G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
  • G21F—PROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
  • G21F5/00—Transportable or portable shielded containers
  • G21F5/005—Containers for solid radioactive wastes, e.g. for ultimate disposal
  • G21F5/008—Containers for fuel elements
• • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E30/00—Energy generation of nuclear origin
  • Y02E30/30—Nuclear fission reactors

Definitions

• the invention relates to a package for storing and / or transporting radioactive materials, such as fresh or irradiated nuclear fuel assemblies. It relates in particular to the attachment of a cooling element to an outer wall element of the package.
• a packaging for transporting and / or storing radioactive materials comprises a lateral body closed at its two longitudinal ends respectively by a bottom and a cover.
• the side body includes a plurality of cooling elements that protrude from outer wall members to the outside of the package. These cooling elements are often very close to each other along a circumferential direction of the package.
• the cooling elements are in particular fixed by welding to the wall elements. However, some welding processes generate a risk of damaging / cutting the cooling elements, especially near their base. Other welding processes may damage the outer wall elements.
• the invention aims to at least partially solve the problems encountered in the solutions of the prior art.
• the invention relates to a packaging for transporting and / or storing radioactive materials such as nuclear fuel assemblies.
• the package includes a wall member and a cooling member attached to the wall member.
• the cooling element protrudes from the wall element towards the outside of the package.
• the cooling element comprises a base and at least one fin integral with the base.
• the base extends on either side of the fin respectively towards two opposite lateral ends of the base, each of the lateral ends being fixed to the wall element via a weld.
• the base makes it possible to move the melting zone away from the base of the fin when attaching the cooling element to the wall element.
• the risk of damaging / cutting the fin is reduced when using known welding processes with an intense and localized heat input such as a laser beam or electron beam welding.
• the invention reduces the risks of damaging the cooling element, while limiting the deformations of the wall element during attachment of the cooling element to the wall element.
• the invention may optionally include one or more of the following features combined with one another or not.
• the wall element comprises a housing in which the base is arranged, at least one of the lateral ends of the base being connected to at least one lateral edge of the housing via a weld.
• the base is housed in the housing so as to be flush with the surface of the wall element at least at an edge of the housing. This results in better fixation of the cooling element and better thermal conduction between the cooling element and the wall element.
• the height of the base along at least one of the lateral ends is greater than or equal to half the average thickness of the fin.
• the thermal conduction between the base and the wall element is then improved.
• the wall element, the base and / or the fin comprise copper.
• Copper provides adequate thermal conduction but the wall element, base and / or fin are more susceptible to plastic deformation.
• the base and the fin are monobloc.
• the package comprises a neutron protection block and at least one internal thermal conduction element
• the wall element being rigidly secured to the internal thermal conduction element, the internal thermal conduction element being in contact with a ferrule of the packaging,
• the ferrule, the internal thermal conduction element and the wall element at least partially surrounding the neutron protection block.
• the cooling element comprises at least two fins and a base common to the fins, the base extending on either side of each fin towards two opposite lateral ends of the base. each end being secured to the wall member via a weld.
• the packaging comprises a second cooling element fixed to the wall element, the second cooling element comprising at least one fin integral with the base, the distance between the cooling elements being less than at the height of at least one of the fins.
• the number and density of the cooling elements make the packaging difficult to achieve, while providing good heat dissipation.
• the invention also relates to a thermal conduction element for packaging for transporting and / or storing radioactive materials, comprising:
• the inner heat conduction member and the cooling element being located on either side of the wall element which mechanically connects them and thermally
• the cooling element comprising a base and at least one fin integral with the base.
• the base extends on either side of the fin respectively towards two opposite lateral ends of the base, each of the lateral ends being fixed to the wall element via a weld.
• the invention also relates to a method of manufacturing a packaging for transporting and / or storing radioactive materials as defined above.
• the method comprises a step of welding each of the two opposite lateral ends of the base to the wall element.
• the width of the base between its two lateral ends is greater than or equal to twice the average thickness of the fin.
• the risk of cutting the fins is further reduced by further moving the melting zone from the base of the fin, when attaching the cooling element to the wall element.
• the base is welded to the wall element by electron beam or laser beam welding.
• the base is arranged in a housing formed in the wall element, the base being welded in the housing along a thermal contact interface, the thermal contact interface being inclined according to an angle of 0 ° to 30 ° relative to the direction of the height of the fin.
• the attachment of the cooling element to the base is improved, while promoting heat exchange between the base and the cooling element.
• the manufacturing method comprises a step of making notches in a plate to form fins of the cooling element, the notches being spaced apart from one another along the longitudinal direction of the plate. .
• the plate comprises the base of the cooling element.
• the step of welding the lateral ends of the base in the longitudinal direction of the plate takes place after the step of making the cuts.
• the method comprises a step of twisting the fins about their longitudinal axis after the welding step.
• FIG. 1 is a partially perspective and partially sectional representation of a package for transporting and / or storing nuclear fuel assemblies, according to a first embodiment of the invention
• Figure 2 is a partial cross-sectional representation of the package, according to the first embodiment
• Figure 3 is a partial elevational representation of a thermal conduction element of the package according to the first embodiment
• FIG. 4 is a partially perspective view and partially in section of a package, according to a second embodiment of the invention.
• Figure 5 is a partial elevational representation of a thermal conduction element of the package, according to the second embodiment
• FIG. 6 is a partial cross-sectional representation of a cooling element of the package, according to the first or second embodiment
• Figure 7 is a partial cross-sectional representation of an alternative embodiment of the cooling element and the wall element
• FIG. 8 at least partially illustrates the implementation of the method of manufacturing the package, according to the first or the second embodiment
• Figure 9 at least partially illustrates the implementation of an alternative embodiment of a method of manufacturing a package
• Figure 10 illustrates the embodiment of a plurality of fins during the manufacture of a package, according to the first embodiment.
• Figure 1 shows a package 2 for transporting and / or storing radioactive materials such as nuclear fuel assemblies.
• the package 2 comprises a lateral body 20 delimited radially inwards by a ferrule 21 made of steel and radially outwardly by thermal conduction elements 22.
• the lateral body 20 extends along a longitudinal axis X-X of the package.
• the package is closed on both sides of the lateral body 20 in the longitudinal direction X-X by a cover 4 and by a bottom 6.
• the adjective “longitudinal” means substantially parallel to the longitudinal axis XX
• the adjective “radial” means oriented in a direction substantially orthogonal to that axis
• the adjective “transverse” means according to a plane substantially orthogonal to the longitudinal axis XX.
• the term “circumferential” refers to a direction about the longitudinal axis X-X.
• the collar 21 defines an internal cavity 5 of the package 2 inside which is housed a basket 7 for storing nuclear fuel assemblies inside the package 2.
• the package 2 and the basket 7 housed in the package 2 define a container 1 for the transport and / or storage of radioactive materials.
• the thermal conduction elements 22 each comprise a wall element 26 and at least one cooling element 30 which is welded to an outer surface Si of the wall element 26.
• the heat conduction element 22 is made of copper or aluminum. one of its alloys for its high thermal conductivity.
• each thermal conduction element 22 is shown in a circumferential direction with two cooling elements 30 for greater visibility.
• the thermal conduction element 22 is shown with three cooling elements 30 including a first cooling element 31 and a second cooling element 32.
• the thermal conduction elements 22 also each comprise an internal thermal conduction element 28 which is curved at its first end 28a and which is connected to the inner surface S 2 of the wall element 26 at its second end 28b opposite the first end 28a.
• the first ends 28a are fixed to the shell 21, for example by welding.
• the wall elements 26 are interconnected by welds 29, so as to form an outer wall of the package 2.
• the cooling elements 30 protrude radially from the wall element 26 towards the outside of the package 2, while the internal heat-conducting element 28 projects from the wall element 26 towards the inside of the housing. In other words, the cooling elements 30 and the internal heat-conducting elements 28 are located radially on either side of the wall elements 26.
• the thermal conduction elements 22 each enclose a neutron protection block 24 inside the lateral body 20.
• This neutron protection block 34 is situated, in the circumferential direction, between two consecutive internal conduction elements 28. It is located in the radial direction between the collar 21 on the one hand and the wall element 26 of the thermal conduction element 22 on the other hand.
• the cooling elements 30 each comprise a plurality of fins 34 which are spaced apart from each other along the longitudinal direction XX of the package 2 and which are extend in a radial direction YY. Moreover, the fins 34 are each twisted about their longitudinal axis Y-Y.
• Each of the cooling elements 30 comprises a single base
• the base 40 which is common to its fins 34 and from which radially extend the fins 34.
• the base 40 extends substantially continuously along the longitudinal direction X-X over the entire length of the cooling element 30.
• the distance "d" between two consecutive cooling elements 31, 32 is smaller than the height hi of the fins 34, which allows a good evacuation of the heat out of the package 2. Nevertheless, the small distance “D” between the cooling elements 30 relative to their height hi tends to make the package 2 more difficult to manufacture.
• the heat is discharged out of the container 1 from the shell 21, successively through the internal thermal conduction elements 28, the wall elements 26 and possibly the cooling elements 30.
• Figures 4 and 5 show a container 1 for the transport and / or storage of radioactive material which differs from the container 1 according to the first embodiment by the structure of the cooling elements 30.
• the cooling elements 30 each comprise a single fin 35 in the form of a plate. This fin 35 extends substantially over the entire length of the package 2 in the longitudinal direction X-X.
• the base 40 extends substantially continuously along the longitudinal direction X-X over the entire length of the cooling element 30.
• the distance "d" between two consecutive fins 31, 32 is substantially identical to that between two consecutive fins 34 of the first embodiment.
• the number of cooling elements 30 of the package 2 according to the second embodiment is substantially identical to the number of cooling elements 30 of the package 2 according to the first embodiment. Only two cooling elements 30 have been shown in FIG. 5 for more readability.
• each of the cooling elements 30 has at least one fin 34, 35 and the base 40.
• the cooling element 30 is connected to the wall element 26 at level of the base 40.
• the base 40 includes a first lateral end 44 and a second lateral end 45 opposite the first lateral end 44.
• the fin 34, 35 is located between the lateral ends 44, 45.
• the lateral surfaces delimiting the lateral ends 44, 45 are substantially orthogonal to the bottom 42 of the base.
• the bottom 42 of the base is substantially orthogonal to the Y-Y axis of the fin 34, 35.
• the width of the base l 2 taken between its lateral ends 44, 45 is approximately equal to twice the average thickness ei of the fin 34, 35.
• the width l 4 of the first end 44 is substantially equal to the width I5 of the second end 45.
• the height h 2 of the base is greater than or equal to half the thickness ei of the fin 34, 35.
• the base 40 is housed in a groove 50 made in the wall element 26.
• This groove 50 extends substantially in the longitudinal direction XX of the package 2. It forms a recess formed in the outer surface Si of the wall element 26.
• the base 40 is housed in the groove 50 so as to be flush with the surface of the wall element 26.
• the height h 2 of the base 40 is substantially equal to the height h 3 of the groove 50. which promotes heat exchange between the bottom of the groove 52 and the bottom 42 of the base 40 by contact.
• the groove 50 is delimited laterally by a first lateral edge 54 and by a second lateral edge 55 opposite to the first lateral edge 54.
• the first lateral edge 54 is intended to be in mechanical contact with the first lateral end 44 of the base along a first heat exchange interface S 4 via a first weld.
• the first lateral edge 54 has a shape substantially complementary to that of the first lateral end 44.
• the first weld extends all along the first lateral edge 54, which promotes the heat exchange between the wall element 26 and the fin 34, 35.
• the second lateral edge 55 is intended to be in mechanical contact with the second lateral end 45 of the base along a second heat exchange surface S5 via a second weld.
• the second lateral edge 55 has a shape substantially complementary to that of the second lateral end 45.
• the second weld extends substantially along the entire second lateral edge 55, which promotes the heat exchange between the wall element 26 and fin 34, which are represented by the arrow F.
• the first weld and the second weld are the only welds from the base 40 to the wall element 26. They are made without filler material.
• the groove 50 has a width b between its lateral edges 54, 55 which is substantially equal to the width l 2 of the base 40 taking into account the first weld and the second weld, in order to promote heat exchange between the wall element 26 and the cooling element 30.
• FIG. 7 shows an alternative embodiment in which the first lateral end 44 has a frustoconical shape forming an angle ⁇ 1 with the YY axis of the fin 34, 35 and the second lateral end 45 has a frustoconical shape forming an angle a 2 with the axis YY of the fin 34, 35.
• the angle ai is substantially equal to the angle a 2 and about 30 ° at most, to facilitate the attachment of the base 40 to the side edges 54, 55 of the groove, while ensuring a suitable thermal conduction between the wall element 26 and the cooling element 30.
• the method of manufacturing the package 2 according to the first or second embodiment is illustrated with reference to FIG. 8.
• the cooling elements 30 are fixed to the wall element 26 by welding with intense and localized heat input such as laser beam or electron beam welding.
• the cooling element 30 is first placed in the groove 50 of the wall element 26 so as to be flush with the surface of the wall element 26, as illustrated by the arrow A.
• the cooling element 30 is fixed at its first lateral end 44 to the first lateral edge 54 by a first welding beam 61, so as to make the first weld along the first thermal contact interface S 4 .
• the cooling element 30 is fixed at its second lateral end 45 to the second lateral edge 55 by a second welding beam 62, so as to perform the second weld along the second thermal contact interface S5.
• the welding of the cooling element 30 at the lateral ends 44, 45 of the base makes it possible to move the welding bundles 61, 62 away from the fin 34, 35, which limits the risks of cutting it during the welding.
• the welding beams 61, 62 are in particular substantially parallel to the Y-Y axis of the fin 34, 35.
• the cooling elements 30 are welded one after the other to the wall element 26 along the circumferential direction of the package 2.
• a second cooling element 32 is attached to the wall element 26 only when the first cooling element 31 which is immediately adjacent thereto has been fixed to the corresponding wall element 26 over the entire length of this cooling element 31.
• FIG. 9 illustrates the manufacture of a package 2 for transporting and / or storing radioactive materials according to a third embodiment.
• the cooling elements 30 of this package each comprise either a plurality of fins 34 spaced in the longitudinal direction X-X, according to the first embodiment, or a single fin 35 shaped plate, as in the second embodiment.
• the manufacturing method according to FIG. 9 differs from the manufacturing method according to FIG. 8 in that the base 40 of each cooling element 30 is not housed in a groove 50. On the contrary, the base 40 is welded. on the uniformly flat surface of the wall element 26.
• the cooling element 30 is fixed at its first lateral end 44 by the first welding beam 61, along a third thermal contact interface S6.
• the cooling element 30 is fixed at its second lateral end 45 by a second welding beam 62, along a fourth thermal contact interface S 7 .
• the third thermal contact interface S6 and the fourth thermal contact interface S 7 result from the fusion of the lateral ends 44, 45 of the em base 40 on the wall element 26.
• the welding beams are preferably substantially parallel with respect to the axis YY of the at least one fin 34, 35 of the cooling element 30.
• the angle ⁇ of the first welding beam 61 with the axis YY is in particular between 0 ° and 30 °.
• the angle ⁇ 2 of the second welding beam 62 with the axis YY is in particular between 0 ° and 30 °.
• the angle Qi is substantially identical to the angle ⁇ 2 .
• Figure 10 illustrates the manufacture of the fins 34 of one of the cooling elements 30 of the package 2 according to the first embodiment.
• the manufacturing method comprises a step of producing notches 33 in a plate 36 so as to form fins 34.
• This plate 36 is of a shape similar to that of the cooling element 30 according to the second embodiment of realization.
• the notches 33 are evenly spaced from each other along the longitudinal direction X-X.
• the fins 34 each have a rectangular shape.
• the notched cooling element 30 is then welded to the wall element 26 over substantially the entire length of the cooling element 30.
• the fins 34 are then twisted along the arrow B, preferably each in the same direction, around their longitudinal axis Y-Y, so as to increase the spacing between two consecutive fins 34.
• the heat conduction element 22 is then substantially identical to that shown in FIG. 3 with reference to the first embodiment.
• the packages 2 have a substantially cylindrical lateral body 20. Nevertheless, the lateral body 20 may take other suitable forms, such as a hexagonal shape.
• the heat conducting elements 22 shown may comprise a single cooling element 30, two cooling elements 30 with three or more cooling elements 30. Nevertheless, the distance "d" between the cooling elements 30 is preferably less than the height hi of the fins 34, 35.
• the cooling elements 30 each extend substantially in the longitudinal direction X-X of the package 2, but it is understood that they can be inclined with respect to the longitudinal axis X-X.
• the cooling elements 30 preferably remain substantially parallel to each other.
• the base 40 is substantially symmetrical by plane symmetry passing through the Y-Y axis of the fin 34, 35 of the cooling element. Nevertheless, it could be asymmetrical with respect to this plan.
• the notches 33 can be made only after the cooling element 30 has been welded to the wall element 26.
• the bottom 42 of the base 40 may also be welded to the bottom 52 of the groove.
• the welds may possibly be made with a filler material.

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• 2015
  • 2015-10-16 FR FR1559894A patent/FR3042635B1/fr active Active
• 2016
  • 2016-10-13 US US15/768,797 patent/US10522260B2/en active Active
  • 2016-10-13 KR KR1020187010579A patent/KR102567921B1/ko active IP Right Grant
  • 2016-10-13 CN CN201680059984.8A patent/CN108140438B/zh active Active
  • 2016-10-13 WO PCT/EP2016/074561 patent/WO2017064174A1/fr active Application Filing
  • 2016-10-13 JP JP2018519377A patent/JP6828030B2/ja active Active
  • 2016-10-13 EP EP16781429.2A patent/EP3363022A1/de not_active Withdrawn

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