EP2320432B1 - Verpackung für den Transport und/oder zur Zwischenlagerung radioaktiver Stoffe, die eine verstärkte Wärmeübertragung ermöglicht - Google Patents

Verpackung für den Transport und/oder zur Zwischenlagerung radioaktiver Stoffe, die eine verstärkte Wärmeübertragung ermöglicht Download PDF

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Publication number
EP2320432B1
EP2320432B1 EP10190306.0A EP10190306A EP2320432B1 EP 2320432 B1 EP2320432 B1 EP 2320432B1 EP 10190306 A EP10190306 A EP 10190306A EP 2320432 B1 EP2320432 B1 EP 2320432B1
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EP
European Patent Office
Prior art keywords
components
elements
along
canister according
radiological protection
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EP10190306.0A
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English (en)
French (fr)
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EP2320432A1 (de
Inventor
Olivier Bardon
Guillaume Foussard
Stavros Kitsos
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TN International SA
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TN International SA
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    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21FPROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
    • G21F5/00Transportable or portable shielded containers
    • G21F5/06Details of, or accessories to, the containers
    • G21F5/10Heat-removal systems, e.g. using circulating fluid or cooling fins
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21FPROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
    • G21F3/00Shielding characterised by its physical form, e.g. granules, or shape of the material
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21FPROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
    • G21F5/00Transportable or portable shielded containers
    • G21F5/005Containers for solid radioactive wastes, e.g. for ultimate disposal
    • G21F5/008Containers for fuel elements
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining

Definitions

  • the present invention relates to the field of transport and / or storage of radioactive materials, such as nuclear fuel assemblies, fresh or irradiated.
  • the invention relates to a package comprising a radiological protection device arranged between two concentric rings, forming a barrier against gamma radiation.
  • storage devices are used, also called “basket” or “rack” storage.
  • These storage devices usually of cylindrical shape and of substantially circular section, have a plurality of adjacent housings each adapted to receive a nuclear fuel assembly.
  • the storage device is intended to be housed in the cavity of a package to form together with it a container for the transport and / or storage of nuclear fuel assemblies, in which the nuclear material is confined.
  • the aforementioned cavity is generally defined by a lateral body extending in a longitudinal direction of the package, this lateral body comprising for example two concentric metal ferrules jointly forming an annular space inside which is housed a radiological protection device, in particular to form a barrier against gamma radiation emitted by the fuel assemblies housed in the cavity.
  • the radiological protection device is made using several prefabricated elements made of lead or in one of its alloys, distributed around the cavity, in the appropriate annular space defined by the two metal ferrules.
  • each of these elements is inserted between the two ferrules, in a longitudinal insertion direction.
  • a mounting clearance must be provided to allow such insertion, this game resulting in a discontinuity of material in the lateral body of the package, in the radial direction in which the inner ring is successively arranged, the protective elements radiological, and the outer shell.
  • the discontinuity of material observed has the effect of a considerable decrease in the thermal conductivity of the lateral body of the package, implying a low capacity of the latter to evacuate the heat produced by the fuel assemblies.
  • the gaps between the radiological protection elements and the ferrules may be reduced by decreasing manufacturing tolerances, but it is nevertheless very expensive, and does not by any means to eliminate discontinuities matter.
  • Another solution consists in separating the radiological protection function from the thermal conduction function, this being then fulfilled by means of additional elements of the fin type connecting the two ferrules, arranged alternately with the radiological protection elements in the radiator. annular space. Nevertheless, this further complicates the design of the package, and also requires the use of special techniques to ensure that the fins are in contact with each of the two side body ferrules.
  • the invention therefore aims to at least partially overcome the disadvantages mentioned above, relating to the achievements of the prior art.
  • the subject of the invention is a package for transporting and / or storing radioactive materials, said package comprising a lateral body extending around a longitudinal axis of said package, said lateral body forming a cavity of housing of radioactive materials and comprising an inner metal ferrule and an outer metal ferrule, the two ferrules being concentric and jointly forming an annular space within which a gamma radiation barrier radiation protection device is housed, said radiological protection device comprising at least first and second radiological protective metal elements adjacent in a circumferential direction of the packaging.
  • said first element bears against the outer shell and at a distance from said inner shell, while said second element bears against the inner shell and at a distance from said outer shell.
  • said first and second elements are in contact with each other in an interface taking, in section along any plane orthogonal to the longitudinal axis and passing through this interface, the shape of a line segment defining with a radial line crossing it in the middle an acute angle (A).
  • the invention thus offers a clever design allowing the radiological protection elements to conduct heat satisfactorily between the two ferrules. Indeed, the heat is conducted continuously first between the inner ferrule and the second radiological protection element, by the contact between these parts, then through the interface between the first and second elements, and finally between the first radiological protection element and the outer shell, still due to the expected contact between these parts.
  • the particular geometry and layout of the radiological protection elements allow to confer on the lateral body of the packaging a satisfactory thermal conductivity.
  • the presence of helium or thermal conduction fins is therefore no longer necessary, which makes it possible to present a packaging of simplified design and manufacture.
  • first and second radiological protection elements are no longer intended, as in the prior art, to approach closer to each of the two ferrules, but each being only in contact with one and remotely on the other of the two ferrules, the manufacturing tolerances of these elements can be increased. This advantageously results in a significant cost reduction.
  • one and / or the other radiological protection elements can be coated with a heat conductive layer at the contact interface, to further improve the thermal conduction between these elements.
  • This layer is preferably thin, and deformable, for example made of lead or in one of its alloys.
  • this heat conducting layer solution can also be adopted at the contacts between the radiological protection elements and the ferrules.
  • said angle (A) is between 30 and 60 °, and more preferably, is close to 45 °.
  • the interfaces thus inclined allow a satisfactory radial plating of the radiological protection elements, when these are circumferentially constrained.
  • said interface is plane.
  • the package comprises at least one first metal radiological protection element and two second metal radiological protection elements arranged on either side of said first element in the circumferential direction, said first element being in contact with each of the two elements.
  • second elements respectively according to two interfaces each taking, in section along any plane orthogonal to the longitudinal axis and passing through this interface, the shape of a line segment defining with a radial line passing through it in the middle an acute angle (A) , the two line segments being respectively supported by lines approximating one of the other going radially inward and intercepting between the two radial lines.
  • the first element is solicited by the two second elements, which therefore participate jointly in its plating against the outer shell.
  • this first element participates in the plating of the second two elements against the inner shell.
  • the package preferably comprises at least one second metal radiological protection element and two first metal radiological protection elements arranged on either side of said second element in the circumferential direction, said second element being in contact with each of the first two elements respectively according to two interfaces each taking, in section along any plane orthogonal to the longitudinal axis and passing through said interface, the shape of a line segment defining with a radial straight line crossing it in the middle an acute angle (A), the two line segments being respectively supported by lines approaching one another radially outwardly and interposed between the two radial lines.
  • A acute angle
  • first and second elements arranged alternately in the circumferential direction, and cooperating in the aforementioned manner, namely that each of them is solicited by its two adjacent elements, which jointly participate in its plating against its associated ferrule.
  • each first radiological protection element has a section, in any plane orthogonal to the longitudinal axis, in the overall shape of a trapezium whose large base bears against the outer shell and the small base at a distance from the inner shell
  • each second radiological protection element has a section, in any plane orthogonal to the longitudinal axis, of overall shape of trapezium whose large base bears against the inner ferrule and the small base remote from the outer ferrule, and the faces of the first and second elements defining the sides of the trapezoids are in contact two by two, so as to form said interfaces.
  • first elements could adopt a form different from that of the second elements, just as different forms could be adopted within the first / second elements.
  • other forms envisaged are for example the triangle, or the truncated trapezium at the two corners between the large base and the sides.
  • the large base is intercepted, locally in the middle, orthogonally by a radial line.
  • each trapezoid is isosceles.
  • each trapezium is preferably straight, and even more preferably in the form of a circular arc of diameter identical to that of the ferrule surface that it contacts, in order to increase the contact area between these two elements.
  • the ratio of lengths between the large base and the small base is between 3 and 8. The larger the ratio, the more effective the heat transfer.
  • each of said plurality of first and second elements is maintained only by contacts in the annular space. This implies, in particular, that no additional fastening means is reported between a protective element and its associated shell, or between two directly consecutive protection elements.
  • the design allows these elements to maintain each other by contact, also using ferrules. This possibility is also offered for protection elements with a shape different from that of the trapezoid.
  • the package may then comprise clamping means housed in said annular space, for constraining said plurality of first and second elements in the circumferential direction, and thus cause the plating of these elements radially against their associated ferrule.
  • each of said plurality of first and second elements takes the form of a trapezoidal prism.
  • each of said plurality of first elements or each of said plurality of second elements is fixedly mounted on its associated shell, for example by pins / nuts or equivalent means, and each of the plurality other elements is maintained only by contacts in the annular space, between its two adjacent elements attached to their ferrule.
  • each of said plurality of elements fixedly mounted on its associated shell has a decreasing section in a given direction of the longitudinal direction of the package, and each of the plurality of the other elements has a section increasing in said given direction of the longitudinal direction.
  • the intensity of the contacts is therefore dependent on the longitudinal relative position between the elements. Consequently, when one of the longitudinal sliding protection elements is inserted between its two associated fixed protection elements, the contacts between the elements, once established, have an intensity that increases as one continues insertion.
  • the subject of the invention is also a method for manufacturing a package as described above, in which each first and second radiological protection metal element is inserted into said annular space, and then a clamping is carried out. to constrain these elements in the circumferential direction.
  • the container 1 generally comprises a packaging 2 object of the present invention, inside which there is a storage device 4, also called storage basket.
  • the device 4 is intended to be placed in a housing cavity 6 of the package 2, as schematically shown in FIG. figure 1 on which it is also possible to see the longitudinal axis 8 of this package, coincident with the longitudinal axes of the storage device and the housing cavity.
  • longitudinal should be understood as parallel to the longitudinal axis 8 and the longitudinal direction X of the package
  • circumferential should be understood as orthogonal to the same longitudinal axis 8, as well as to a transverse direction of the package.
  • the storage device 4 comprises a plurality of adjacent housings arranged parallel to the axis 8, the latter being each adapted to receive at least one fuel assembly of square or rectangular section , and preferably only one.
  • the container 1 and this device 4 have been shown in a vertical loading / unloading position of the fuel assemblies, different from the horizontal / recumbent position usually adopted during the transportation of the assemblies.
  • the package 2 has essentially a bottom 10 on which the device 4 is intended to rest in a vertical position, a cover 12, and a lateral body 14 extending around and along the axis longitudinal 8, this body 14 defining a packaging opening for penetrating the basket into the housing cavity 6, and then being closed by the cover 12.
  • this lateral body 14 which defines the housing cavity 6, with the aid of a lateral inner surface 16 of substantially cylindrical shape and of circular section, and of axis coincident with the axis 8.
  • the bottom 10, which defines the bottom of the cavity 6 open at the cover 12, can be made in one piece with at least a portion of the lateral body 14, without departing from the scope of the invention.
  • FIG 2 a part of the lateral body 14, which firstly has two concentric metal ferrules jointly forming an annular space 18 centered on the longitudinal axis of the package (not visible in this figure), can be seen in detail, this space 18 housing a radiological protection device 20 specific to the present invention.
  • the ferrules 22, 24 are for example steel.
  • This protective device 20 is in particular designed to form a barrier against gamma radiation emitted by the irradiated fuel assemblies housed in the cavity 6. Thus, it is housed between the inner ferrule 22 whose surface interior corresponds to the inner lateral surface 16 of the cavity 6, and the outer shell 24.
  • the protection device 20 comprises a plurality of first and second radiological protection elements, respectively referenced 30 and 32, which are arranged alternately in the circumferential direction T, also said direction tangential.
  • the number of these elements 30, 32 may be several tens.
  • the first and second elements 30, 32 are metallic, preferably lead or cast iron blocks or in one of their alloys, this type of material making it possible to provide both a radiological protection against gamma radiation, and a satisfactory thermal conductivity.
  • Each of the first and second members 30, 32 has a substantially trapezoidal section, which, in this first preferred embodiment, is preferably constant over its entire length.
  • each element here takes the form of a straight prism of axis parallel to the axis 8, trapezoidal base, housed between the two rings 22, 24, and extending longitudinally along the length of the cavity 6.
  • the trapezoidal section takes the overall shape of an isosceles trapezium.
  • the face which defines the large base is supported, and more preferably in direct contact, against the inner surface 24a of the outer shell 24.
  • This contact is preferably surface, over the entire surface of the prism which is opposite the inner surface 24a.
  • the large base preferably adopts a convex circular arc shape of diameter that is close to or identical to that of the inner surface 24a, and of the same center, even if a large straight base could be envisaged, without departing from the scope of the invention.
  • the small base is spaced from the outer surface 22a of the inner ferrule 22, a substantial clearance can be provided, for example greater than 5 mm, or much more.
  • the aforementioned radial clearance represents between 1/30 and 1/10 of the radial thickness of the space 18.
  • each second element 32 has its face defining the large base in abutment, and more preferably in direct contact, against the outer surface 22a of the inner shell 22.
  • This contact is preferably surface-based, over the entire surface of the prism which is opposite the outer surface 22a.
  • the large base here adopts a concave arc shape of diameter close to or identical to that of the outer surface 22a, and the same center, although a large straight base could also be considered.
  • the small base is spaced from the inner surface 24a of the inner ferrule 22, a substantial clearance can be provided, for example greater than 5 mm, or much more.
  • the aforementioned radial clearance represents more generally between 1/30 and 1/10 of the radial thickness of the space 18.
  • the faces of the first and second elements 30, 32 which define the small bases of the trapezoids may have, in cross section, various shapes, for example straight or in arcs of circles.
  • each contact interface 40 adopts, in section along any plane orthogonal to the longitudinal axis 8 and passing through this interface, the shape of a line segment defining, with a radial straight line 41 passing through it in the middle M, an acute angle A.
  • This acute angle A which is therefore between the values of 0 ° and 90 °, excluded from the range, is preferably between 30 and 60 °, and even more preferably of the order of 45 °.
  • the direction of inclination of the aforementioned line segment is such that the radial straight line 41 first extends through the first element 30 starting from the segment and going radially outwards, and extends first to through the second element 32 starting from the segment and going radially inwards.
  • the line segment 40 extends radially inwardly from its center being circumferentially offset from the radial line 41 in a circumferential offset direction corresponding to that of the first element 30 relative to the second element 32.
  • the first leftmost element 30 is circumferentially offset from the second leftmost element 32 in a clockwise direction.
  • the radially inner portion of the segment 40 is offset from the radial line 41.
  • the two interfaces 40 defined thereby each take the form of an inclined line segment of the acute angle A with respect to its associated radial line 41.
  • these two straight segments 40 are respectively supported by two straight lines 40 'approaching one another radially inwardly, and intersecting at a point I situated between the two radial lines 41 , 41 crossing these two same segments in their middle.
  • each segment 40 forms part of the line 40 'which supports it.
  • the two interfaces 40 defined thereby each take the form of an inclined line segment of the acute angle A with respect to its associated radial line 41.
  • these two straight segments 40 are respectively supported by two straight lines 40 'approaching one another radially outwardly, and intercepting at a point I located between the two radial straight lines 41, 41 passing through these two same segments in their middle.
  • the ratio of lengths between the large base E and the small base e is between 3 and 8.
  • the heat generated by the assemblies is conducted continuously between the two rings 22, 24, which gives a satisfactory thermal conductivity to the lateral body.
  • the heat is firstly conducted between the inner ferrule 22 and the faces defining the large bases of the second elements 32, then by the contact interfaces 40 between the first and second elements 30, 32, and finally between the faces defining the large bases of the first elements 30 and outer shell 24.
  • One of the main advantages of this solution lies in obtaining continuous privileged paths of thermal conduction between the two rings, with elements 30, 32 of simple shape, each in contact with only one of these two ferrules. This last point implies that they can be manufactured with significant tolerances, decreasing their cost of production.
  • each of the elements 30, 32 is thus maintained solely by contacts in the annular space 18, each of them being pressed against one of the ferrules and against its two adjacent protective elements.
  • the elements 30, 32 can thus be inserted longitudinally one after the other in the space 18, each element then being placed in contact with the last element previously inserted, at the level of one of its lateral faces defining a trapezium side, its other side face being for it to serve as a contact support for the next element to be inserted.
  • the plurality of elements 30, 32 may extend continuously 360 °. Nevertheless, to overcome the possible difficulties of mounting the last radiological protection element, said plurality of elements 30, 32 may extend over substantially less than 360 ° in order to leave an angular sector dedicated to the location of means of protection. circumferential tightening in the space 18.
  • a circumferential clamping device 44 is shown schematically on the figure 3 placed between the two end elements of said plurality of elements forming an angular sector close to 360 °.
  • This device which may have any design deemed appropriate by those skilled in the art, makes it possible to constrain the elements 30, 32 in the circumferential direction, as shown schematically by the arrows 46.
  • This circumferential stressing of said plurality of elements generates, between each pair of any two adjacent elements 30, 32, an increase in the contact force exerted on the faces defining the sides of the trapeziums, this force oriented orthogonally to the interface 40 being represented by the arrows 48 on the figure 3 .
  • the force 48 makes it possible to constrain each of the two elements 30, 32 against its ferrule associated, as has been schematized by the arrows 50.
  • one of the two elements 30, 32 exerts on the other an effort against the plating against its associated ferrule, and vice versa.
  • circumferential clamping devices 44 for example three arranged at 120 °. Whatever the number of these devices 44, two of them directly consecutive in the circumferential direction delimit between them a plurality of elements 30, 32 they force circumferentially. So, in the example shown on the figure 4 three separate sets 52 'are each provided, each forming a plurality of elements 30, 32 slid into the annular space 18, as well as three clamping devices 44 each participating in the circumferential pressurization of two adjacent sets 52'.
  • clamping devices 44 In the case where several clamping devices 44 are provided in the annular space 18, at least one of them can then take the form of an element fixed to one of the ferrules 22, 24, of shape identical or similar to that of the elements 30, 32. Although this device does not include means for deploying circumferentially, it still performs a clamping function in combination with each clamping device being directly consecutive, constituting a pressure stop for the plurality of elements with which it is associated.
  • the fixed element may furthermore perform an angular indexing function of the elements 30, 32, and also serves as a fixed support capable of holding the first element 30, 32 in position after it has been slipped into the annular space 18, during the manufacture of the package.
  • a circumferential clamping device 44 capable of being deployed in this direction in order to constrain said plurality of elements 30, 32. It adopts a general shape that is identical or similar to that of the elements 30, 32 by its generally isosceles trapezoidal cross-sectional shape, but, unlike the latter made preferably in one piece, it is designed from three distinct parts. Indeed, it firstly comprises two lateral portions 50 each having a face intended to form one of the sides of the trapezium, these two faces being intended to contact the two elements placed on either side of this device 44.
  • the clamping device 44 takes the form of a first element 30, it then contacts the two second members 32 which are directly adjacent thereto in the circumferential direction, and vice versa.
  • These parts 50 are symmetrical and jointly define a face intended to form the small base of the trapezium. They also each comprise a face intended to form a portion of the large base of the trapezium, this large base being completed, in its center, by the base of a clamping element 52 of triangular section, intended to be inserted between the two parts. 50.
  • This clamping element 52 is tapered, namely that it has a triangular section which decreases in the longitudinal direction X, as is visible on the Figures 7a and 7b . If the base of this clamping element 52 is provided to complete the large base of the trapezium, its two flat lateral faces are in turn intended to pressurize two flat bearing surfaces 54 at a distance and facing each other, belonging respectively to the two lateral parts 50.
  • the inclinations of the lateral faces of the clamping element 52 and the bearing surfaces 54 are provided to simultaneously obtain two surface contacts, preferably planar contacts.
  • the device 44 operates as follows. First, the two lateral pieces 50 are inserted into the interior space defined by the ferrules, between two elements 30, 32. Then, it is the clamping element 52 which is slid longitudinally between the two surfaces of support 54, until the contacts contacts plans. Continuing longitudinal displacement of the clamping member 52 by relative to the parts 50 leads to separate them from one another in the circumferential direction T, and thus to constrain in this same direction the plurality of radiological protection elements 30, 32, which then flatten each other against their ferrule associated, because of the relative radial displacement between these elements.
  • each first element 30 remains maintained only by contacts in the annular space 18, between its two adjacent second elements 32 fixed to the ferrule 22, and the outer ferrule 24.
  • the second elements 32 each have a trapezoidal section decreasing in a given direction of the longitudinal direction X, and that, conversely, the first elements 30 each have a trapezoidal section increasing in given meaning, this being the most visible on the Figures 10a and 10b .
  • each first element 30 is slid longitudinally between its two second fixed elements 32 associated and between the two rings 22, 24, to obtaining two planar contacts between the lateral faces of the elements 30, 32 defining the sides of the trapeziums, and obtaining a planar contact between the face of the element 30 defining the large base and the outer shell.
  • the side faces of the elements 30, 32, defining the sides of the trapezoids are planar.
  • the variation of trapezoidal section in the longitudinal direction is such that the lateral faces of the elements 30 and 32 are inclined with respect to the longitudinal axis by a value between 1 and 10 °.
  • the mere self weight of the element 30 may be sufficient to achieve the desired contact forces.
  • the third embodiment shown on the figure 11 differs from the previous ones in that the first elements 30 have a truncated trapezoidal overall cross-section at the two corners between the large base and the sides, and in that the second elements 32 have a cross-section in overall shape of triangle.
  • the other characteristics are identical or similar, in particular as regards the inclination of the contact interfaces 40.

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Packaging Of Annular Or Rod-Shaped Articles, Wearing Apparel, Cassettes, Or The Like (AREA)
  • Buffer Packaging (AREA)

Claims (17)

  1. Verpackung (2) für den Transport und/oder die Zwischenlagerung radioaktiver Materialien, wobei die Verpackung einen lateralen Körper (14) umfasst, der sich um eine Längsachse (8) der Verpackung herum erstreckt, wobei der laterale Körper einen Hohlraum (6) zur Aufnahme der radioaktiven Materialien bildet und einen metallischen Innenmantel (22) sowie einen metallischen Außenmantel (24) umfasst, wobei die zwei Mäntel konzentrisch sind und gemeinsam einen ringförmigen Raum (18) bilden, in dem eine radiologische Schutzvorrichtung (20) aufgenommen ist, die eine Barriere gegen die Gammastrahlen bildet, wobei die radiologische Schutzvorrichtung wenigstens ein erstes und ein zweites metallisches radiologisches Schutzelement (30, 32) umfasst, die in einer Umfangsrichtung der Verpackung benachbart sind,
    dadurch gekennzeichnet, dass
    das erste Element (30) in Anlage an dem Außenmantel (24) und in einem Abstand von dem Innenmantel (22) ist, wohingegen das zweite Element (32) in Anlage an dem Innenmantel (22) und in einem Abstand von dem Außenmantel (24) ist, und
    dass das erste und das zweite Element (30, 32) miteinander in Kontakt sind entlang einer Grenzfläche (40), die in einem Schnitt entlang einer beliebigen Ebene, die zur Längsachse (8) orthogonal ist und diese Grenzfläche schneidet, die Form eines Geradensegments aufweist, das mit einer radialen Geraden, die es in seiner Mitte schneidet, einen spitzen Winkel (A) bildet.
  2. Verpackung nach Anspruch 1, dadurch gekennzeichnet, dass der Winkel (A) zwischen 30 und 60° enthalten ist.
  3. Verpackung nach Anspruch 1 oder Anspruch 2, dadurch gekennzeichnet, dass die Grenzfläche (40) eben ist.
  4. Verpackung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass sie wenigstens ein erstes metallisches radiologisches Schutzelement (30) sowie zwei zweite metallische radiologische Schutzelemente (32) umfasst, die auf beiden Seiten des ersten Elements (30) in der Umfangsrichtung angeordnet sind, wobei das erste Element (30) in Kontakt mit jedem der zwei zweiten Elemente (32) entlang jeweils zwei Grenzflächen (40) ist, die jeweils im Schnitt entlang einer beliebigen Ebene, die zur Längsachse (8) orthogonal ist und diese Grenzfläche schneidet, die Form eines Geradensegments aufweist, das mit einer radialen Geraden, die es in seiner Mitte schneidet, einen spitzen Winkel (A) definiert, wobei die zwei Geradensegmente jeweils durch zwei Geraden getragen werden, die sich einander annähern, wobei sie radial nach innen verlaufen und sich zwischen den zwei radialen Geraden schneiden.
  5. Verpackung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass sie wenigstens ein zweites metallisches radiologisches Schutzelement (32) sowie zwei erste metallische radiologische Schutzelemente (30) umfasst, die auf beiden Seiten des zweiten Elements (32) in der Umfangsrichtung angeordnet sind, wobei das zweite Element (32) in Kontakt mit jedem der zwei ersten Elemente (30) entlang jeweils zwei Grenzflächen (40) ist, die jeweils im Schnitt entlang einer beliebigen Ebene, die zur Längsachse (8) orthogonal ist und diese Grenzfläche schneidet, die Form eines Geradensegments aufweist, das mit einer radialen Geraden, die es in seiner Mitte schneidet, einen spitzen Winkel definiert, wobei die zwei Geradensegmente jeweils durch zwei Geraden getragen werden, die sich einander annähern, wobei sie radial nach außen verlaufen und sich zwischen den zwei radialen Geraden schneiden.
  6. Verpackung nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass sie eine Mehrzahl von ersten und zweiten metallischen radiologischen Schutzelementen (30, 32) umfasst, die alternierend in der Umfangsrichtung angeordnet sind.
  7. Verpackung nach Anspruch 6, dadurch gekennzeichnet, dass jedes erste radiologische Schutzelement (30) einen Schnitt in einer beliebigen, zur Längsachse (8) orthogonalen Ebene in der allgemeinen Form eines Trapez aufweist, dessen große Basis in Anlage an dem Außenmantel (24) und dessen kleine Basis in einem Abstand von dem Innenmantel (22) ist,
    das jedes zweite radiologische Schutzelement (32) einen Schnitt in einer beliebigen, zur Längsachse (8) orthogonalen Ebene in der allgemeinen Form eines Trapez aufweist, dessen große Basis in Anlage an dem Innenmantel (22) und dessen kleine Basis in einem Abstand von dem Außenmantel (24) ist, und
    dass die Flächen des ersten und des zweiten Elements (30, 32), die die Seiten der Trapeze definieren, paarweise derart in Kontakt sind, dass sie die Grenzflächen (40) bilden.
  8. Verpackung nach Anspruch 7, dadurch gekennzeichnet, dass für jedes Trapez die große Basis lokal in ihrer Mitte orthogonal durch eine radiale Gerade geschnitten wird.
  9. Verpackung nach Anspruch 7 oder Anspruch 8, dadurch gekennzeichnet, dass jedes Trapez gleichschenklig ist.
  10. Verpackung nach einem der Ansprüche 7-9, dadurch gekennzeichnet, dass die große Basis jedes Trapezes gerade ist oder die Form eines Kreisbogens mit identischem Durchmesser wie jener der Oberfläche des Mantels hat, den es kontaktiert.
  11. Verpackung nach einem der Ansprüche 7-10, dadurch gekennzeichnet, dass für jedes Trapez das Verhältnis der Längen zwischen der großen Basis und der kleinen Basis zwischen 3 und 8 enthalten ist.
  12. Verpackung nach einem der Ansprüche 6-11, dadurch gekennzeichnet, dass jedes aus der Mehrzahl von ersten und zweiten Elementen (30, 32) ausschließlich durch Kontakte in dem ringförmigen Raum (18) gehalten ist.
  13. Verpackung nach Anspruch 12, dadurch gekennzeichnet, dass sie Spannmittel (44) umfasst, die in dem ringförmigen Raum (18) aufgenommen sind und es erlauben, die Mehrzahl von ersten und zweiten Elementen in der Umfangsrichtung zusammen zu drücken.
  14. Verpackung nach Anspruch 12 oder Anspruch 13, dadurch gekennzeichnet, dass jedes aus der Mehrzahl von ersten und zweiten Elementen (30,32) die Form eines Prismas mit trapezförmiger Basis hat.
  15. Verpackung nach einem der Ansprüche 6-11, dadurch gekennzeichnet, dass jedes aus der Mehrzahl von ersten Elementen (30) oder jedes aus der Mehrzahl von zweiten Elementen (32) fest an seinem zugeordneten Mantel (24, 22) montiert ist, und dass jedes aus der Mehrzahl von anderen Elementen ausschließlich durch Kontakte in dem ringförmigen Raum (18) gehalten ist.
  16. Verpackung nach Anspruch 15, dadurch gekennzeichnet, dass jedes aus der Mehrzahl von Elementen (32), die fest an ihrem zugeordneten Mantel (22) montiert sind, einen Querschnitt aufweist, der sich in einer gegebenen Richtung der Längsrichtung (X) der Verpackung verringert, und dass jedes aus der Mehrzahl von anderen Elementen (32) einen Querschnitt aufweist, der in der gegebenen Richtung der Längsrichtung zunimmt.
  17. Verfahren zur Herstellung einer Verpackung nach einem der Ansprüche 1-14, bei dem man jedes erste und zweite metallische Element zum radiologischen Schutz in den ringförmigen Raum einsetzt und dann einen Spannvorgang realisiert, der ein Zusammendrücken dieser Elemente in der Umfangsrichtung erlaubt.
EP10190306.0A 2009-11-10 2010-11-08 Verpackung für den Transport und/oder zur Zwischenlagerung radioaktiver Stoffe, die eine verstärkte Wärmeübertragung ermöglicht Not-in-force EP2320432B1 (de)

Applications Claiming Priority (1)

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FR0957929A FR2952467B1 (fr) 2009-11-10 2009-11-10 Emballage pour le transport et/ou entreposage de matieres radioactives conferant un transfert thermique renforce

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EP2320432A1 EP2320432A1 (de) 2011-05-11
EP2320432B1 true EP2320432B1 (de) 2013-10-16

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FR2961942B1 (fr) * 2010-06-25 2014-04-11 Tn Int Conteneur pour le transport et/ou l'entreposage de matieres radioactives
FR2988898A1 (fr) * 2012-03-28 2013-10-04 Commissariat Energie Atomique Procede et dispositif mobile permettant de reduire les resistances thermiques entre deux solides
KR101559300B1 (ko) 2013-12-03 2015-11-20 한국원자력환경공단 사용후핵연료 저장용 캐니스터 이송용기
CN121132229B (zh) * 2025-10-17 2026-04-21 天津瑞迪瀚森科技有限公司 一种放射源的装配台

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FR2181540B1 (de) * 1972-04-27 1974-12-20 Commissariat Energie Atomique
JP3342994B2 (ja) * 1995-08-04 2002-11-11 株式会社神戸製鋼所 放射性物質の輸送兼貯蔵用容器
FR2776118B1 (fr) * 1998-03-13 2000-06-09 Transnucleaire Dispositif de protection contre les rayonnements pour conteneur de transport de matieres radioactives
KR100466066B1 (ko) * 2000-04-25 2005-01-13 미츠비시 쥬고교 가부시키가이샤 열간 확장 성형용 금속 빌렛
JP2002098797A (ja) * 2000-09-26 2002-04-05 Mitsubishi Heavy Ind Ltd キャニスタおよびこれを備えた金属収納容器
JP4291588B2 (ja) * 2003-01-31 2009-07-08 株式会社神戸製鋼所 コンクリートキャスク並びにその製造方法
JP2007139677A (ja) * 2005-11-22 2007-06-07 Hitachi Ltd 放射性物質収納容器およびその製造方法
US7973298B2 (en) * 2007-10-10 2011-07-05 Kobe Steel, Ltd. Transport/storage cask for radioactive material
JP2008076408A (ja) * 2007-10-22 2008-04-03 Mitsubishi Heavy Ind Ltd 放射性物質格納容器

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EP2320432A1 (de) 2011-05-11
US20110272603A1 (en) 2011-11-10
KR20110052488A (ko) 2011-05-18
US8716686B2 (en) 2014-05-06
JP2011102802A (ja) 2011-05-26
FR2952467B1 (fr) 2011-12-23
ES2441225T3 (es) 2014-02-03

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