[go: up one dir, main page]

EP3038113B1 - Use of a material comprising a solid matrix of a siliconised polymer and inorganic fillers such as neutron-absorbing material - Google Patents

Use of a material comprising a solid matrix of a siliconised polymer and inorganic fillers such as neutron-absorbing material Download PDF

Info

Publication number
EP3038113B1
EP3038113B1 EP15201763.8A EP15201763A EP3038113B1 EP 3038113 B1 EP3038113 B1 EP 3038113B1 EP 15201763 A EP15201763 A EP 15201763A EP 3038113 B1 EP3038113 B1 EP 3038113B1
Authority
EP
European Patent Office
Prior art keywords
use according
atoms
inorganic filler
hours
polysiloxane
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP15201763.8A
Other languages
German (de)
French (fr)
Other versions
EP3038113A1 (en
Inventor
Jean Félix SALAS
François GARONNE
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Commissariat a lEnergie Atomique et aux Energies Alternatives CEA filed Critical Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Publication of EP3038113A1 publication Critical patent/EP3038113A1/en
Application granted granted Critical
Publication of EP3038113B1 publication Critical patent/EP3038113B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21FPROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
    • G21F1/00Shielding characterised by the composition of the materials
    • G21F1/02Selection of uniform shielding materials
    • G21F1/10Organic substances; Dispersions in organic carriers
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21FPROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
    • G21F1/00Shielding characterised by the composition of the materials
    • G21F1/02Selection of uniform shielding materials
    • G21F1/10Organic substances; Dispersions in organic carriers
    • G21F1/103Dispersions in organic carriers

Definitions

  • the invention relates to the field of neutron protection, also called neutron shielding.
  • a material comprising a solid matrix based on a silicone polymer (resin or elastomer) as well as fillers dispersed in this matrix as a neutron-absorbing material.
  • This material besides being capable of slowing down and capturing neutrons very efficiently, has remarkable properties of resistance to high temperatures and, in particular, resistance to thermal aging, and has, among other additional advantages, being able to present itself under a number of conditions. flexible or rigid form depending on the use for which it is intended.
  • neutron protection elements can be of any size (whether in terms of length, width or thickness) and of any geometrical configuration and can be both flexible elements such as seals (for example, sealing ) or coatings (eg, sleeves or sleeves for cables, pipes, vats or the like) than rigid elements such as doors, frames, walls, partitions, screens or cabinets.
  • a material is called neutron when it is able to slow down and capture neutrons.
  • a material to be able to slow down and capture neutrons it should contain light nuclei, ie typically hydrogen atoms, which will slow down neutrons by an elastic scattering mechanism , and nuclei "greedy" in neutrons, such as boron, cadmium or lithium, which will capture the neutrons thus slowed down.
  • nuclei ie typically hydrogen atoms, which will slow down neutrons by an elastic scattering mechanism
  • nuclei "greedy" in neutrons such as boron, cadmium or lithium
  • the neutrophage materials which are obtained from a silicone elastomer, such as those proposed in references [5] and [6] are necessarily flexible materials and can not therefore be used to produce elements of rigid neutron protection.
  • the material described in reference [5] has a low hydrogen content because, on the one hand, the silicones are compounds that are not very rich in hydrogen and, on the other hand, the other components of this material are free of hydrogen.
  • a low hydrogen content is detrimental to the ability of the material to slow neutrons and, therefore, to play satisfactorily the role of neutron screen.
  • the inventors have therefore set themselves the goal of providing a neutron-absorbing material which is, in general, devoid of the various limits presented by the neutrophage materials proposed to date.
  • the present invention proposes the use of a material comprising a solid matrix based on a silicone polymer in which a hydrogenated inorganic filler and a borated inorganic filler are dispersed as a material. neutrophage, the silicone polymer being a polysiloxane which is formed by one or more siloxane repeating units and characterized in that in said siloxane repeating units the silicon atom is bonded to one or two aromatic groups.
  • the inventors have, in fact, found that the dispersion, within a matrix based on a silicone polymer, of inorganic fillers, respectively hydrogenated and borated, makes it possible to obtain a material which combines neutrophage and high temperatures particularly interesting and this silicone polymer is a silicone resin or a silicone elastomer.
  • the expression " based on a silicone polymer ", as applied to the solid matrix, means that this matrix has a polysiloxane for majority component, that is to say that this polysiloxane represents more than 50% by weight of the mass of said matrix.
  • the solid matrix comprise, as polymer, only this polysiloxane but it goes without saying that it can perfectly consist of a mixture of several different polysiloxanes or a mixture of one or more polysiloxanes and one or more other non-polysiloxane polymers, suitable for facilitating the use of the material or for imparting particular properties depending on the use for which it is intended, provided, of course, that this or these non-polysiloxane polymers are compatible with said polysiloxane (s).
  • the solid matrix comprises a polysiloxane which is formed by one or more siloxane repeating units in which the silicon atom is bonded to one or two aromatic groups, so that the material is as resistant as possible neutron and gamma irradiation.
  • the aromatic group (s) present in the polysiloxane are typically phenyl, benzyl, o-tolyl, m-tolyl, p-tolyl, o-xylyl or mesityl groups, phenyl being particularly preferred.
  • the polysiloxane is a homopolymer, i.e. it consists of only one repeating siloxane unit, which corresponds to formula (I) above, in which R 1 is phenyl, while R 2 is methyl or phenyl.
  • the polysiloxane is a poly [methyl (phenyl) siloxane] or a poly (diphenylsiloxane).
  • the hydrogenated inorganic filler is advantageously chosen from metal hydroxides, which, in addition to slowing the neutrons very effectively, have the advantage of giving the material an excellent fire resistance.
  • metal hydroxides examples include aluminum hydroxide (Al (OH) 3 , also called alumina hydrate), magnesium hydroxide (Mg (OH) 2 , also called hydrated magnesia) and their mixtures.
  • the borated inorganic filler it is advantageously chosen from zinc borates such as Zn 2 O 14.5 B 6 H 7 , Zn 4 O 8 B 2 H 2 or Zn 2 O 11 B 6 , disodium tetraborate decahydrate ( Na 2 B 4 O 7 • 10H 2 O or borax), boron carbide (B 4 C), boron oxide (B 2 O 3 ), boric acid (H 3 BO 3 ), colemanite ( Ca 2 O 14 B 6 H 10 ) and mixtures thereof.
  • zinc borates such as Zn 2 O 14.5 B 6 H 7 , Zn 4 O 8 B 2 H 2 or Zn 2 O 11 B 6 , disodium tetraborate decahydrate ( Na 2 B 4 O 7 • 10H 2 O or borax), boron carbide (B 4 C), boron oxide (B 2 O 3 ), boric acid (H 3 BO 3 ), colemanite ( Ca 2 O 14 B 6 H 10 ) and mixtures thereof.
  • the hydrogenated inorganic filler is aluminum hydroxide
  • the boron inorganic filler is a zinc borate because of the flame retardant properties of this type of compound and, more particularly, a zinc borate containing aluminum oxide.
  • hydrogen such as Zn 2 O 14.5 H 7 B 6 or Zn 4 O 8 B 2 H 2 .
  • the amount of hydrogenated inorganic filler is preferably selected so that, taking into account the quantities of hydrogen also present in the polysiloxane, the material has an atomic concentration of hydrogen ranging from 28 3,2.10 atoms / m 3 to 6.3.10 28 atoms / m 3 and more preferably 4.1.10 28 atoms / m 3 to 6.10 28 atoms / m 3 .
  • the amount of boron inorganic filler is preferably chosen so that the material has a boron atomic concentration ranging from 1.9 ⁇ 10 27 atoms / m 3 to 1.8 ⁇ 10 28 atoms / m 3 and, more preferably, from 2.1.10 27 atoms / m 3 to 9.10 27 atoms / m 3 .
  • the solid matrix may contain other adjuvants in order to modify the behavior of the material during its use or its properties of use, such as fillers (inorganic or organic) stabilizers, plasticizers, dyes, pigments, antistats, etc.
  • the solid matrix may contain inorganic fillers of the silica type, natural or synthetic, or carbon black to increase the hardness of the material.
  • the material is preferably used for the manufacture of neutron shielding elements (i.e. as a component of these protective elements) and, more preferably, as elements of Neutron protection for nuclear power plants or reprocessing plants for the reprocessing of spent nuclear fuel.
  • an accelerator or a crosslinking catalyst selected from the compounds conventionally used to accelerate or catalyze the crosslinking of silicones can be added to resin mixture or silicone elastomer / hydrogenated inorganic filler / borated inorganic filler.
  • the shaping of the mixture can be achieved by all the techniques conventionally used for shaping materials based on silicone resins or silicone elastomers, such as casting molding, compression molding or injection molding. .
  • the resins and elastomers without solvent are in the form of viscous liquids whose volatile mass is less than 10%, or even 5%, of the total mass of these resins or elastomers.
  • the use of this type of silicone greatly limits the amount of volatiles to be removed during the implementation of the material and, thereby, the creation within this material pores suitable for constitute pockets for the gaseous hydrogen likely to be produced by radiolysis of the material under the effect of ionizing radiation.
  • the crosslinking of this elastomer is preferably carried out while maintaining the silicone / silicone elastomer mixture.
  • a complementary heat treatment, for example a few hours at a temperature between 100 and 150 ° C, can then be applied to the material for increase its hardness and thus confer optimal mechanical properties, for example for subsequent machining.
  • This mixture is degassed under vacuum at 50 ° C, then poured into square molds, 10 cm square and 1 cm thick.
  • the molds thus filled are placed in an oven heated at 120 ° C. for 16 hours and then at 200 ° C. for 2 hours to induce the crosslinking of the silicone resin.
  • the density of the plates of the material thus obtained is measured according to the conventional technique of weighing in air / weighing in water. This density is equal to 1.7 and is consistent with the theoretical density. The material therefore contains no porosity.
  • the plates are subjected to tests in order to assess the ability of the material to retain over time, on the one hand, its properties neutrophages, and, on the other hand, its mechanical properties, when maintained at high temperatures.
  • the ability of the material to retain its neutrophage properties is assessed by an accelerated aging test to simulate the behavior of the material if it were maintained for 100,000 hours (more than 11 years) at 150 ° C. Briefly, this test consists in keeping the material plates for several hundred hours in an oven heated to 120 ° C, 150 ° C, 180 ° C or 205 ° C, to be measured at time intervals the mass of the plates and to establish, for each of these temperatures, a curve representing the mass loss of the material as a function of the residence time in the oven. A master curve corresponding to the loss of mass undergone by the material for a heating of 100,000 hours at the temperature of 150 ° C. is then constructed by translation of the three other curves with respect to that obtained for heating at 150 ° C.
  • elemental analyzes are carried out on plates of the material to determine the atomic hydrogen concentration of this material before it is placed in an oven and after a residence of 24 hours, 96 hours and 500 hours in an oven heated to 150 ° C.
  • the ability of the material to retain its mechanical properties is, in turn, appreciated by a thermal aging test which consists in keeping the plates of the material for 90 hours in an oven heated to 150 ° C or for 170 hours in a heated oven at 250 ° C and follow the evolution over time the evolution of the flexural Young's modulus and the maximum bending stress of the material, which is measured according to the NF EN ISO 178 standard.
  • figure 1 which represents the evolution of the atomic hydrogen concentration [H] at (in number of atoms / cm 3 ) of the material over time (in hours), as determined by the elementary analyzes (curve) and by Calculations made from the accelerated aging test (symbol ⁇ ), the atomic hydrogen concentration of the material decreases slightly when it is subjected to a temperature of 150 ° C for a very prolonged period of time. As a result, its neutrophage properties are remarkably well preserved.
  • figures 2 and 3 which respectively represent the evolution of Young's modulus in bending E (in MPa) and that of the maximum bending stress ⁇ max (in MPa) of the material over time (in hours), as obtained when this material is maintained for 90 hours at 150 ° C (A curves) or for 170 hours at 250 ° C (B curves), holding the material for several tens of hours at a temperature of 150 ° C or 250 ° C n does not cause significant degradation of its mechanical properties.
  • the plates of the material thus obtained are subjected to thermal aging tests in order to assess the ability of the material to retain over time, on the one hand, its neutrophage properties, and on the other hand, its mechanical properties, when maintained at elevated temperatures.
  • the ability of the material to retain its mechanical properties is, in turn, appreciated by a thermal aging test which consists of keeping the plates of the material for 500 hours in an oven heated to 150 ° C or for 200 hours in a heated oven at 250 ° C and to follow the evolution over time of the elongation at break A and the modulus E in tension of the material which is measured according to standard NF EN ISO 527-1.
  • Figures 5 and 6 which respectively represent the evolution of the elongation at break A (in%) and that of the Young's modulus in traction E (in MPa) of the material over time (in hours), as obtained when this material is maintained for 500 hours at 150 ° C (curves A) and for 200 hours at 250 ° C (curves B), the mechanical properties of the material stabilize after a hundred hours of aging at 150 ° C.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Dispersion Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Description

DOMAINE TECHNIQUETECHNICAL AREA

L'invention se rapporte au domaine de la protection neutronique, aussi appelée blindage neutronique.The invention relates to the field of neutron protection, also called neutron shielding.

Plus spécifiquement, elle se rapporte à l'utilisation d'un matériau comprenant une matrice solide à base d'un polymère (résine ou élastomère) silicone ainsi que des charges dispersées dans cette matrice comme matériau neutrophage.More specifically, it relates to the use of a material comprising a solid matrix based on a silicone polymer (resin or elastomer) as well as fillers dispersed in this matrix as a neutron-absorbing material.

Ce matériau, outre d'être capable de ralentir et de capturer très efficacement les neutrons, présente des propriétés remarquables de résistance aux températures élevées et, notamment de tenue au vieillissement thermique, et a, entre autres avantages supplémentaires, de pouvoir se présenter sous une forme souple ou rigide en fonction de l'usage auquel il est destiné.This material, besides being capable of slowing down and capturing neutrons very efficiently, has remarkable properties of resistance to high temperatures and, in particular, resistance to thermal aging, and has, among other additional advantages, being able to present itself under a number of conditions. flexible or rigid form depending on the use for which it is intended.

De ce fait, il est particulièrement utile pour la fabrication d'éléments de protection contre les neutrons qui sont destinés à être utilisés dans des environnements où règnent en permanence ou de façon transitoire des températures élevées, tels que ceux que l'on peut trouver dans les centrales nucléaires et dans les usines de traitement de combustibles nucléaires irradiés.Therefore, it is particularly useful for the manufacture of neutron shielding elements which are intended to be used in environments where high temperatures, such as those found in nuclear power plants and irradiated nuclear fuel plants.

Ces éléments de protection neutronique peuvent être de toutes dimensions (que ce soit en termes de longueur, de largeur ou d'épaisseur) et de toutes configurations géométriques et peuvent être aussi bien des éléments flexibles tels que des joints (par exemple, d'étanchéité) ou des revêtements (par exemple, de type gaines ou manchons pour câbles, canalisations, cuves ou analogues) que des éléments rigides tels que des portes, des châssis, des parois, des cloisons, des paravents ou des armoires.These neutron protection elements can be of any size (whether in terms of length, width or thickness) and of any geometrical configuration and can be both flexible elements such as seals (for example, sealing ) or coatings (eg, sleeves or sleeves for cables, pipes, vats or the like) than rigid elements such as doors, frames, walls, partitions, screens or cabinets.

ÉTAT DE LA TECHNIQUE ANTÉRIEURESTATE OF THE PRIOR ART

Un matériau est dit neutrophage quand il est capable de ralentir et de capturer les neutrons.A material is called neutron when it is able to slow down and capture neutrons.

Pour qu'un matériau soit capable de ralentir et de capturer les neutrons, il convient qu'il renferme des noyaux légers, c'est-à-dire typiquement des atomes d'hydrogène, qui vont ralentir les neutrons par un mécanisme de diffusion élastique, et des noyaux « gourmands » en neutrons, comme des atomes de bore, de cadmium ou de lithium, qui vont capturer les neutrons ainsi ralentis.For a material to be able to slow down and capture neutrons, it should contain light nuclei, ie typically hydrogen atoms, which will slow down neutrons by an elastic scattering mechanism , and nuclei "greedy" in neutrons, such as boron, cadmium or lithium, which will capture the neutrons thus slowed down.

Il a ainsi été proposé :

  • un matériau neutrophage rigide, qui est obtenu par polymérisation/ réticulation d'une résine polyester insaturé dans laquelle ont été préalablement incorporées des particules de polyéthylène pour augmenter le taux d'hydrogène de la résine, ainsi qu'un composé boré, lithié ou cadmié (voir US-A-4,134,937 , ci-après référence [1]) ;
  • un matériau neutrophage rigide, qui est obtenu par durcissement d'un mortier comprenant des granulats d'un composé boré inorganique tel que la colémanite, du ciment alumineux et de l'eau (voir EP-A-0 106 759 , ci-après référence [2]):
  • un matériau neutrophage rigide, qui est obtenu par polymérisation/ réticulation d'une résine polyester insaturé ou d'une résine vinylester dans laquelle ont été préalablement incorporés un composé inorganique hydrogéné du type hydroxyde d'aluminium ou de magnésium, ainsi qu'un composé inorganique de bore du type acide borique, colémanite ou borate de zinc (voir WO-A-03/030183 et WO-A-03/050822 , ci-après références [3] et [4]) ;
  • un matériau neutrophage souple, qui est obtenu par vulcanisation d'un élastomère, typiquement un caoutchouc silicone bi-composant, dans lequel ont été préalablement incorporés un composé écran aux rayonnements γ (par exemple, du carbure de tungstène), un composé absorbant les neutrons/bloquant les rayonnements γ (par exemple, du carbure de bore), un composé thermoconducteur (par exemple, du diamant), un composé résistant à la chaleur (par exemple, de la silice), un composé absorbant les neutrons/électroconducteur (par exemple, du sulfate de baryum) et un composé absorbant l'hydrogène sous forme gazeuse (par exemple, du palladium spongieux) (voir WO-A-02/101756 , ci-après référence [5]) ; et
  • un matériau neutrophage souple, qui est obtenu par vulcanisation d'un polydiméthylsiloxane auquel ont été ajoutés un polypropylène, de l'hydroxyde d'aluminium et du carbure de bore (voir KR 1019980078181 B1 , ci-après référence [6]).
It has been proposed:
  • a rigid neutrophage material, which is obtained by polymerization / crosslinking of an unsaturated polyester resin in which polyethylene particles have been previously incorporated to increase the hydrogen content of the resin, and a borated, lithiated or cadmium compound ( see US Patent 4,134,937 , hereinafter reference [1] );
  • a rigid neutrophage material which is obtained by curing a mortar comprising aggregates of an inorganic boron compound such as colemanite, aluminous cement and water (see EP-A-0 106 759 , hereinafter reference [2] ):
  • a rigid neutron-absorbing material which is obtained by polymerization / crosslinking of an unsaturated polyester resin or a vinylester resin in which a hydrogenated inorganic compound of the aluminum hydroxide or magnesium type has been previously incorporated, as well as an inorganic compound of boric acid type, colemanite or zinc borate (see WO-A-03/030183 and WO-A-03/050822 , hereinafter references [3] and [4] );
  • a flexible neutrophage material, which is obtained by vulcanization of an elastomer, typically a two-component silicone rubber, into which a γ-radiation shielding compound (for example, tungsten carbide), a neutron absorbing compound, has been previously incorporated; γ blocking (e.g., boron carbide), a thermally conductive compound (e.g., diamond), a heat-resistant compound (e.g., silica), a compound neutron absorbing / electroconductive (e.g., barium sulfate) and hydrogen-absorbing compound in gaseous form (e.g., sponge palladium) (see WO-A-02/101756 , hereinafter reference [5] ); and
  • a soft neutrophage material which is obtained by vulcanizing a polydimethylsiloxane to which polypropylene, aluminum hydroxide and boron carbide have been added (see KR 1019980078181 B1 , hereinafter reference [6] ).

Il se trouve que les matériaux neutrophages qui sont obtenus par polymérisation/réticulation d'une résine thermodurcissable, tels que ceux proposés dans les références [1], [3] et [4], sont obligatoirement des matériaux rigides et ne peuvent donc être utilisés pour la fabrication d'éléments de protection neutronique flexibles. Il en est de même pour les matériaux obtenus par durcissement d'un mortier, tel que celui proposé dans la référence [2]. It happens that the neutrophage materials which are obtained by polymerization / crosslinking of a thermosetting resin, such as those proposed in references [1], [3] and [4], are necessarily rigid materials and can not be used for the manufacture of flexible neutron protection elements. It is the same for materials obtained by hardening a mortar, such as that proposed in reference [2].

A l'inverse, les matériaux neutrophages qui sont obtenus à partir d'un élastomère silicone, tels que ceux proposés dans les références [5] et [6], sont obligatoirement des matériaux souples et ne peuvent donc être utilisés pour réaliser des éléments de protection neutronique rigides. De plus, le matériau décrit dans la référence [5] présente une faible teneur en hydrogène en raison de ce que, d'une part, les silicones sont des composés peu riches en hydrogène et, d'autre part, les autres composants de ce matériau sont exempts d'hydrogène. Or, une faible teneur en hydrogène est préjudiciable à la capacité du matériau à ralentir les neutrons et, donc, à jouer de manière satisfaisante le rôle d'écran neutronique.On the other hand, the neutrophage materials which are obtained from a silicone elastomer, such as those proposed in references [5] and [6], are necessarily flexible materials and can not therefore be used to produce elements of rigid neutron protection. In addition, the material described in reference [5] has a low hydrogen content because, on the one hand, the silicones are compounds that are not very rich in hydrogen and, on the other hand, the other components of this material are free of hydrogen. However, a low hydrogen content is detrimental to the ability of the material to slow neutrons and, therefore, to play satisfactorily the role of neutron screen.

Les Inventeurs se sont donc fixés pour but de fournir un matériau neutrophage qui soit, d'une manière générale, dénué des différentes limites présentées par les matériaux neutrophages proposés à ce jour.The inventors have therefore set themselves the goal of providing a neutron-absorbing material which is, in general, devoid of the various limits presented by the neutrophage materials proposed to date.

Plus spécifiquement, ils se sont fixé pour but de fournir un matériau qui, outre de présenter de remarquables propriétés neutrophages, soit également capable de résister à des températures très élevées, c'est-à-dire des températures de 150 à 200°C en continu et de 250 à 300°C en pointe, et puisse de plus se présenter aussi bien sous une forme souple que rigide de manière à être utilisable dans le plus grand nombre d'applications possible.More specifically, they have set themselves the goal of providing a material which, in addition to having outstanding neutron-absorbing properties, is also capable of withstanding very high temperatures, i.e., temperatures of 150 to 200 ° C. continuous and from 250 to 300 ° C peak, and can also be in both flexible and rigid form so as to be used in as many applications as possible.

Ils se sont, de plus, fixés pour but que la fabrication de ce matériau soit simple à mettre en oeuvre et puisse être réalisée à des coûts compatibles avec une exploitation à une échelle industrielle.In addition, they have set themselves the goal that the manufacture of this material is simple to implement and can be carried out at costs compatible with an industrial scale operation.

EXPOSÉ DE L'INVENTIONSTATEMENT OF THE INVENTION

Ces buts et d'autres encore sont atteints par la présente invention qui propose l'utilisation d'un matériau comprenant une matrice solide à base d'un polymère silicone, dans laquelle sont dispersées une charge inorganique hydrogénée et une charge inorganique borée, comme matériau neutrophage, le polymère silicone étant un polysiloxane qui est formé par un ou plusieurs motifs répétitifs siloxane et caractérisé en ce que dans lesdits motifs répétitifs siloxane l'atome de silicium est lié à un ou deux groupes aromatiques.These and other objects are achieved by the present invention which proposes the use of a material comprising a solid matrix based on a silicone polymer in which a hydrogenated inorganic filler and a borated inorganic filler are dispersed as a material. neutrophage, the silicone polymer being a polysiloxane which is formed by one or more siloxane repeating units and characterized in that in said siloxane repeating units the silicon atom is bonded to one or two aromatic groups.

Les Inventeurs ont, en effet, constaté que la dispersion, au sein d'une matrice à base d'un polymère silicone, de charges inorganiques, respectivement hydrogénée et borée, permet d'obtenir un matériau qui cumule des propriétés neutrophages et de résistance aux températures élevées particulièrement intéressantes et ce, que ce polymère silicone soit une résine silicone ou un élastomère silicone.The inventors have, in fact, found that the dispersion, within a matrix based on a silicone polymer, of inorganic fillers, respectively hydrogenated and borated, makes it possible to obtain a material which combines neutrophage and high temperatures particularly interesting and this silicone polymer is a silicone resin or a silicone elastomer.

Il est donc possible, en jouant sur le fait que les résines silicones conduisent à des matériaux rigides alors que les élastomères silicones conduisent à des matériaux souples, de conférer à ce matériau une rigidité ou, au contraire, une souplesse parfaitement adaptée à l'usage auquel il est destiné.It is therefore possible, by playing on the fact that silicone resins lead to rigid materials while silicone elastomers lead to flexible materials, to give this material rigidity or, conversely, a flexibility perfectly adapted to the use for which it is intended.

Dans ce qui précède et ce qui suit, l'expression « à base d'un polymère silicone », telle qu'appliquée à la matrice solide, signifie que cette matrice a un polysiloxane pour composant majoritaire, c'est-à-dire que ce polysiloxane représente plus de 50% en masse de la masse de ladite matrice.In what precedes and what follows, the expression " based on a silicone polymer ", as applied to the solid matrix, means that this matrix has a polysiloxane for majority component, that is to say that this polysiloxane represents more than 50% by weight of the mass of said matrix.

Dans le cadre de l'invention, on préfère que la matrice solide ne comprenne, en tant que polymère, que ce polysiloxane mais il va de soi qu'elle peut parfaitement être constituée d'un mélange de plusieurs polysiloxanes différents ou d'un mélange d'un ou plusieurs polysiloxanes et d'un ou plusieurs autres polymères non polysiloxanes, propres à faciliter la mise en oeuvre du matériau ou à lui conférer des propriétés particulières en fonction de l'usage auquel il est destiné, pour autant, bien entendu, que ce ou ces polymères non polysiloxanes soient compatibles avec ledit ou lesdits polysiloxanes.In the context of the invention, it is preferred that the solid matrix comprise, as polymer, only this polysiloxane but it goes without saying that it can perfectly consist of a mixture of several different polysiloxanes or a mixture of one or more polysiloxanes and one or more other non-polysiloxane polymers, suitable for facilitating the use of the material or for imparting particular properties depending on the use for which it is intended, provided, of course, that this or these non-polysiloxane polymers are compatible with said polysiloxane (s).

Conformément à l'invention, la matrice solide comprend un polysiloxane qui est formé par un ou plusieurs motifs répétitifs siloxane dans lesquels l'atome de silicium est lié à un ou deux groupes aromatiques, de manière à ce que le matériau soit le plus résistant possible aux irradiations neutroniques et gamma.According to the invention, the solid matrix comprises a polysiloxane which is formed by one or more siloxane repeating units in which the silicon atom is bonded to one or two aromatic groups, so that the material is as resistant as possible neutron and gamma irradiation.

Plus encore, on préfère que ce polysiloxane soit formé d'un ou plusieurs motifs répétitifs siloxane qui répondent chacun à la formule (I) ci-après :

Figure imgb0001
dans laquelle :

  • R1 représente un groupe aromatique, tandis que
  • R2 représente un groupe alkyle comprenant de 1 à 4 atomes de carbone, c'est-à-dire méthyle, éthyle, propyle, isopropyle, n-butyle, isobutyle ou tert-butyle, ou bien un groupe aromatique.
More preferably, it is preferred that this polysiloxane be formed of one or more siloxane repeating units which each correspond to formula (I) below:
Figure imgb0001
in which :
  • R 1 represents an aromatic group, while
  • R 2 represents an alkyl group comprising from 1 to 4 carbon atoms, that is to say methyl, ethyl, propyl, isopropyl, n- butyl, isobutyl or tert- butyl, or an aromatic group.

Le ou les groupes aromatiques présents dans le polysiloxane sont typiquement des groupes phényle, benzyle, o-tolyle, m-tolyle, p-tolyle, o-xylyle ou mésityle, le groupe phényle étant particulièrement préféré.The aromatic group (s) present in the polysiloxane are typically phenyl, benzyl, o-tolyl, m-tolyl, p-tolyl, o-xylyl or mesityl groups, phenyl being particularly preferred.

De manière préférée entre toutes, le polysiloxane est un homopolymère, c'est-à-dire qu'il n'est constitué que d'un seul motif répétitif siloxane, lequel répond à la formule (I) ci-avant, dans laquelle R1 est un groupe phényle, tandis que R2 est un groupe méthyle ou phényle. En d'autres termes, le polysiloxane est un poly[méthyl(phényl)siloxane] ou un poly(diphénylsiloxane).Most preferably, the polysiloxane is a homopolymer, i.e. it consists of only one repeating siloxane unit, which corresponds to formula (I) above, in which R 1 is phenyl, while R 2 is methyl or phenyl. In other words, the polysiloxane is a poly [methyl (phenyl) siloxane] or a poly (diphenylsiloxane).

La charge inorganique hydrogénée est avantageusement choisie parmi les hydroxydes métalliques, qui, outre de ralentir très efficacement les neutrons, présentent l'avantage de conférer en plus au matériau une excellente tenue au feu.The hydrogenated inorganic filler is advantageously chosen from metal hydroxides, which, in addition to slowing the neutrons very effectively, have the advantage of giving the material an excellent fire resistance.

A titre d'exemples d'hydroxydes métalliques susceptibles d'être utilisés, on peut notamment citer l'hydroxyde d'aluminium (Al(OH)3, encore appelé hydrate d'alumine), l'hydroxyde de magnésium (Mg(OH)2, encore appelé magnésie hydratée) et leurs mélanges.As examples of metal hydroxides that may be used, there may be mentioned aluminum hydroxide (Al (OH) 3 , also called alumina hydrate), magnesium hydroxide (Mg (OH) 2 , also called hydrated magnesia) and their mixtures.

Quant à la charge inorganique borée, elle est avantageusement choisie parmi les borates de zinc tels que Zn2O14,5B6 H7, Zn4O8B2H2 ou Zn2O11B6, le tétraborate disodique décahydraté (Na2B4O7•10H2O ou borax), le carbure de bore (B4C), l'oxyde de bore (B2O3), l'acide borique (H3BO3), la colémanite (Ca2O14B6H10) et leurs mélanges.As for the borated inorganic filler, it is advantageously chosen from zinc borates such as Zn 2 O 14.5 B 6 H 7 , Zn 4 O 8 B 2 H 2 or Zn 2 O 11 B 6 , disodium tetraborate decahydrate ( Na 2 B 4 O 7 • 10H 2 O or borax), boron carbide (B 4 C), boron oxide (B 2 O 3 ), boric acid (H 3 BO 3 ), colemanite ( Ca 2 O 14 B 6 H 10 ) and mixtures thereof.

De préférence, la charge inorganique hydrogénée est de l'hydroxyde d'aluminium, tandis que la charge inorganique borée est un borate de zinc en raison des propriétés ignifuges que présente ce type de composé et, plus spécialement, un borate de zinc contenant de l'hydrogène comme Zn2O14,5H7B6 ou Zn4O8B2H2.Preferably, the hydrogenated inorganic filler is aluminum hydroxide, while the boron inorganic filler is a zinc borate because of the flame retardant properties of this type of compound and, more particularly, a zinc borate containing aluminum oxide. hydrogen such as Zn 2 O 14.5 H 7 B 6 or Zn 4 O 8 B 2 H 2 .

Conformément à l'invention, la quantité de charge inorganique hydrogénée est, de préférence, choisie de sorte que, compte-tenu des quantités d'hydrogène également présentes dans le polysiloxane, le matériau présente une concentration atomique en hydrogène allant de 3,2.1028 atomes/m3 à 6,3.1028 atomes/m3 et, mieux encore, de 4,1.1028 atomes/m3 à 6.1028 atomes/m3.According to the invention, the amount of hydrogenated inorganic filler is preferably selected so that, taking into account the quantities of hydrogen also present in the polysiloxane, the material has an atomic concentration of hydrogen ranging from 28 3,2.10 atoms / m 3 to 6.3.10 28 atoms / m 3 and more preferably 4.1.10 28 atoms / m 3 to 6.10 28 atoms / m 3 .

Par ailleurs, la quantité de charge inorganique borée est, de préférence, choisie de sorte que le matériau présente une concentration atomique en bore allant de 1,9.1027 atomes/m3 à 1,8.1028 atomes/m3 et, mieux encore, de 2,1.1027 atomes/m3 à 9.1027 atomes/m3.Moreover, the amount of boron inorganic filler is preferably chosen so that the material has a boron atomic concentration ranging from 1.9 × 10 27 atoms / m 3 to 1.8 × 10 28 atoms / m 3 and, more preferably, from 2.1.10 27 atoms / m 3 to 9.10 27 atoms / m 3 .

Outre la charge inorganique hydrogénée et la charge inorganique borée, la matrice solide peut renfermer d'autres adjuvants en vue de modifier le comportement du matériau lors de sa mise en oeuvre ou ses propriétés d'usage, tels que des charges (inorganiques ou organiques), des stabilisants, des plastifiants, des colorants, des pigments, des antistatiques, etc.In addition to the hydrogenated inorganic filler and borated inorganic filler, the solid matrix may contain other adjuvants in order to modify the behavior of the material during its use or its properties of use, such as fillers (inorganic or organic) stabilizers, plasticizers, dyes, pigments, antistats, etc.

En particulier, la matrice solide peut renfermer des charges inorganiques du type silice, naturelle ou synthétique, ou noir de carbone pour augmenter la dureté du matériau.In particular, the solid matrix may contain inorganic fillers of the silica type, natural or synthetic, or carbon black to increase the hardness of the material.

Conformément à l'invention, le matériau est, de préférence, utilisé pour la fabrication d'éléments de protection contre les neutrons (c'est-à-dire comme composant de ces éléments de protection) et, mieux encore, d'éléments de protection neutronique destinés à des centrales nucléaires ou à des usines de retraitement de retraitement de combustibles nucléaires irradiés.In accordance with the invention, the material is preferably used for the manufacture of neutron shielding elements (i.e. as a component of these protective elements) and, more preferably, as elements of Neutron protection for nuclear power plants or reprocessing plants for the reprocessing of spent nuclear fuel.

Un matériau, tel que précédemment défini, peut être préparé par un procédé comprenant :

  • le mélange d'une résine silicone ou d'un élastomère silicone avec une charge inorganique hydrogénée, une charge inorganique borée ;
  • le dégazage, par exemple sous vide, du mélange ainsi obtenu ;
  • la mise en forme du mélange ainsi dégazé ; puis
  • la réticulation de la résine silicone ou de l'élastomère silicone présent dans le mélange ainsi mis en forme.
A material, as previously defined, can be prepared by a process comprising:
  • mixing a silicone resin or a silicone elastomer with a hydrogenated inorganic filler, a borated inorganic filler;
  • degassing, for example under vacuum, of the mixture thus obtained;
  • shaping the mixture thus degassed; then
  • the crosslinking of the silicone resin or of the silicone elastomer present in the mixture thus shaped.

Si besoin est, un accélérateur ou un catalyseur de réticulation, choisi parmi les composés classiquement utilisés pour accélérer ou catalyser la réticulation de silicones (sels métalliques, par exemple de platine ou d'étain, composés organostanneux, peroxydes, etc) peut être ajouté au mélange résine ou élastomère silicone/charge inorganique hydrogénée/charge inorganique borée. La mise en forme du mélange peut-être réalisée par toutes les techniques classiquement utilisées pour la mise en forme de matériaux à base de résines silicones ou d'élastomères silicones, telles que le moulage par coulée, le moulage par compression ou le moulage par injection.If necessary, an accelerator or a crosslinking catalyst selected from the compounds conventionally used to accelerate or catalyze the crosslinking of silicones (metal salts, for example platinum or tin, organostannous compounds, peroxides, etc.) can be added to resin mixture or silicone elastomer / hydrogenated inorganic filler / borated inorganic filler. The shaping of the mixture can be achieved by all the techniques conventionally used for shaping materials based on silicone resins or silicone elastomers, such as casting molding, compression molding or injection molding. .

Pour la réalisation par moulage d'éléments de protection neutronique de forte épaisseur, on préfère utiliser une résine silicone ou un élastomère silicone sans solvant. Typiquement, les résines et élastomères sans solvant se présentent sous la forme de liquides visqueux dont la masse de volatils est inférieure à 10%, voire à 5%, de la masse totale de ces résines ou élastomères. En effet, l'utilisation de ce type de silicones limite fortement la quantité de volatils devant être évacués pendant la mise en oeuvre du matériau et, par là même, la création au sein de ce matériau de pores propres à constituer des poches pour l'hydrogène gazeux susceptible d'être produit par radiolyse du matériau sous l'effet de rayonnements ionisants.For the molding of neutron protection elements of large thickness, it is preferred to use a silicone resin or a silicone elastomer without solvent. Typically, the resins and elastomers without solvent are in the form of viscous liquids whose volatile mass is less than 10%, or even 5%, of the total mass of these resins or elastomers. Indeed, the use of this type of silicone greatly limits the amount of volatiles to be removed during the implementation of the material and, thereby, the creation within this material pores suitable for constitute pockets for the gaseous hydrogen likely to be produced by radiolysis of the material under the effect of ionizing radiation.

Il va de soi que l'utilisation d'une résine silicone ou d'un élastomère silicone sans solvant peut aussi être envisagée pour réaliser des éléments de protection neutronique qui ne sont ni réalisés par moulage, ni épais.It goes without saying that the use of a silicone resin or a silicone elastomer without solvent can also be envisaged to produce neutron protection elements which are neither made by molding nor thick.

Dans le cas où le matériau est réalisé à partir d'une résine silicone ou d'un élastomère silicone réticulable à chaud (encore appelé élastomère silicone HTV pour « High Temperature Vulcanization »), la réticulation de cette résine ou de cet élastomère est, de préférence, effectuée en deux étapes :

  • une première étape d'une durée typiquement de 10 à 16 heures, pendant laquelle le mélange résine ou élastomère silicone/charge inorganique hydrogénée/charge inorganique borée est soumis à une température qui ne dépasse pas 150°C et qui est idéalement comprise entre 100 et 150°C, de manière à obtenir une densification déjà importante de la résine ou de l'élastomère par réticulation partielle mais tout en limitant les risques de déshydratation des charges inorganiques hydrogénée et borée ; et
  • une deuxième étape d'une durée typiquement de 1 à 5 heures, pendant laquelle le mélange résine ou élastomère silicone/charge inorganique hydrogénée/charge inorganique borée est soumis à une température supérieure à 150°C et qui est idéalement comprise entre 150 et 200°C, de manière à achever la réticulation de la résine ou de l'élastomère et à conférer au matériau des propriétés optimales de résistance thermique.
In the case where the material is made from a silicone resin or a silicone elastomer heat curable (also called HTV silicone elastomer for "High Temperature Vulcanization"), the crosslinking of the resin or elastomer is of preferably, carried out in two steps:
  • a first step of a duration typically of 10 to 16 hours, during which the resin mixture or silicone elastomer / hydrogenated inorganic filler / borated inorganic filler is subjected to a temperature which does not exceed 150 ° C and which is ideally between 100 and 150 ° C, so as to obtain an already substantial densification of the resin or of the elastomer by partial crosslinking but while limiting the risks of dehydration of the hydrogenated and borated inorganic fillers; and
  • a second step of a duration typically of 1 to 5 hours, during which the resin mixture or silicone elastomer / hydrogenated inorganic filler / borated inorganic filler is subjected to a temperature above 150 ° C and which is ideally between 150 and 200 ° C, so as to complete the crosslinking of the resin or elastomer and to impart to the material optimum properties of thermal resistance.

Dans le cas où le matériau est réalisé à partir d'un élastomère silicone réticulable à froid (encore appelé élastomère silicone RTV pour « Room Temperature Vulcanization »), la réticulation de cet élastomère est, de préférence, effectuée en maintenant le mélange élastomère silicone/charge inorganique hydrogénée/charge inorganique borée à température ambiante (23-25°C) pendant une durée typiquement de 24 heures. Un traitement thermique complémentaire, par exemple de quelques heures à une température comprise entre 100 et 150°C, peut être alors appliqué au matériau pour augmenter sa dureté et lui conférer ainsi des propriétés mécaniques optimales, par exemple en vue d'un usinage ultérieur.In the case where the material is made from a cold-crosslinkable silicone elastomer (also called RTV silicone elastomer for " Room Temperature Vulcanization "), the crosslinking of this elastomer is preferably carried out while maintaining the silicone / silicone elastomer mixture. hydrogenated inorganic filler / inorganic filler borated at room temperature (23-25 ° C) for a period of typically 24 hours. A complementary heat treatment, for example a few hours at a temperature between 100 and 150 ° C, can then be applied to the material for increase its hardness and thus confer optimal mechanical properties, for example for subsequent machining.

D'autres caractéristiques et avantages de l'invention apparaîtront mieux à la lecture du complément de description qui suit, qui se rapporte à des exemples de préparation de matériaux utiles selon l'invention et de démonstration de leurs propriétés.Other features and advantages of the invention will appear better on reading the additional description which follows, which relates to examples of preparation of useful materials according to the invention and demonstration of their properties.

Bien entendu, ces exemples ne sont donnés qu'à titre d'illustration de l'objet de l'invention et ne constituent en aucun cas une limitation de cet objet.Of course, these examples are given only by way of illustration of the object of the invention and do not constitute in any way a limitation of this object.

BRÈVE DESCRIPTION DES FIGURESBRIEF DESCRIPTION OF THE FIGURES

  • La figure 1 illustre l'évolution de la concentration atomique en hydrogène, notée [H]at et exprimée en nombre d'atomes/cm3, d'un matériau rigide utile selon l'invention au cours du temps, exprimé en heures, telle que déterminée par des analyses élémentaires (dosage chimique) d'échantillons de ce matériau ayant été maintenus 24 heures, 96 heures et 500 heures à 150°C (courbe) et par des calculs effectués à partir d'un test de vieillissement accéléré (symbole ◆).The figure 1 illustrates the evolution of the atomic concentration in hydrogen, denoted [H] at and expressed in number of atoms / cm 3 , of a rigid material useful according to the invention over time, expressed in hours, as determined by elemental analyzes (chemical assay) of samples of this material having been maintained for 24 hours, 96 hours and 500 hours at 150 ° C (curve) and by calculations performed from an accelerated aging test (symbol ◆).
  • La figure 2 illustre l'évolution du module d'Young en flexion, noté E et exprimé en MPa, d'un matériau rigide utile selon l'invention au cours du temps, exprimé en heures, lorsque ce matériau est maintenu pendant 90 heures à 150°C (courbe A) ou pendant 170 heures à 250°C (courbe B).The figure 2 illustrates the evolution of the Young modulus in flexion, denoted E and expressed in MPa, of a rigid material useful according to the invention over time, expressed in hours, when this material is maintained for 90 hours at 150 ° C. (curve A) or for 170 hours at 250 ° C (curve B).
  • La figure 3 illustre l'évolution de la contrainte maximale en flexion, notée σmax et exprimée en MPa, d'un matériau rigide utile selon l'invention au cours du temps, exprimé en heures, lorsque ce matériau est maintenu pendant 90 heures à 150°C (courbe A) ou pendant 170 heures à 250°C (courbe B).The figure 3 illustrates the evolution of the maximum bending stress, denoted σ max and expressed in MPa, of a rigid material useful according to the invention over time, expressed in hours, when this material is maintained for 90 hours at 150 ° C. (curve A) or for 170 hours at 250 ° C (curve B).
  • La figure 4 illustre l'évolution de la concentration atomique en hydrogène, notée [H]at et exprimée en nombre d'atomes/cm3, d'un matériau souple utile selon l'invention au cours du temps, exprimé en heures, telle que déterminée par dosage chimique d'échantillons de ce matériau ayant été maintenus 24 heures, 96 heures et 500 heures à 150°C (courbe) et par des calculs effectués à partir d'un test de vieillissement accéléré (symbole ◆).The figure 4 illustrates the evolution of the atomic concentration in hydrogen, denoted [H] at and expressed in number of atoms / cm 3 , of a flexible material useful according to the invention over time, expressed in hours, as determined by chemical determination of samples of this material having been maintained for 24 hours, 96 hours and 500 hours at 150 ° C (curve) and by calculations performed from an accelerated aging test (symbol ◆).
  • La figure 5 illustre l'évolution de l'allongement à la rupture, noté A et exprimé en %, d'un matériau souple utile selon l'invention au cours du temps, exprimé en heures, lorsque ce matériau est maintenu pendant 500 heures à 150°C (courbe A) et pendant 200 heures à 250°C (courbe B).The figure 5 illustrates the evolution of the elongation at break, denoted A and expressed in%, of a flexible material useful according to the invention over time, expressed in hours, when this material is maintained for 500 hours at 150 ° C. (curve A) and for 200 hours at 250 ° C (curve B).
  • La figure 6 illustre l'évolution du module d'Young en traction, noté E et exprimé en MPa, d'un matériau souple utile selon l'invention au cours du temps, exprimé en heures, lorsque ce matériau est maintenu pendant 500 heures à 150°C (courbe A) et pendant 200 heures à 250°C (courbe B).The figure 6 illustrates the evolution of Young's tensile modulus, denoted E and expressed in MPa, of a flexible material useful according to the invention over time, expressed in hours, when this material is maintained for 500 hours at 150 ° C. (curve A) and for 200 hours at 250 ° C (curve B).
EXPOSÉ DÉTAILLÉ DE MODES DE RÉALISATION PARTICULIERSDETAILED PRESENTATION OF PARTICULAR EMBODIMENTS EXEMPLE 1 : Préparation d'un matériau rigide utile selon l'inventionEXAMPLE 1 Preparation of a Rigid Material Useful According to the Invention

On prépare, dans un mélangeur à turbine, un mélange comprenant :

  • 40% en masse d'une résine silicone à motif répétitif méthyl(phényl)-siloxane sans solvant (référence Silres™ H62 C-société Wacker Chemie AG) ;
  • 17% en masse de borate de zinc de formule Zn2O14,5H7B6 (référence Firebrake™ ZB - société Borax) ;
  • 43% en masse d'hydroxyde d'aluminium (référence SH150 - société Rio Tinto Alcan).
A mixture is prepared in a turbine mixer comprising:
  • 40% by weight of a silicone resin with repeating unit methyl (phenyl) -siloxane without solvent (reference Silres ™ H62 C-company Wacker Chemie AG);
  • 17% by weight of zinc borate of formula Zn 2 O 14.5 H 7 B 6 (reference Firebrake ™ ZB - Borax company);
  • 43% by weight of aluminum hydroxide (reference SH150 - Rio Tinto Alcan company).

Ce mélange est dégazé sous vide à 50°C, puis coulé dans des moules de forme carrée, de 10 cm de côté et de 1 cm d'épaisseur.This mixture is degassed under vacuum at 50 ° C, then poured into square molds, 10 cm square and 1 cm thick.

Les moules ainsi remplis sont placés dans une étuve chauffée à 120°C pendant 16 heures, puis à 200°C pendant 2 heures, pour induire la réticulation de la résine silicone.The molds thus filled are placed in an oven heated at 120 ° C. for 16 hours and then at 200 ° C. for 2 hours to induce the crosslinking of the silicone resin.

Après démoulage, la densité des plaques du matériau ainsi obtenu est mesurée selon la technique classique de pesée dans l'air/pesée dans l'eau. Cette densité est égale à 1,7 et est conforme à la densité théorique. Le matériau ne contient donc aucune porosité.After demolding, the density of the plates of the material thus obtained is measured according to the conventional technique of weighing in air / weighing in water. This density is equal to 1.7 and is consistent with the theoretical density. The material therefore contains no porosity.

Par ailleurs, les plaques sont soumises à des tests en vue d'apprécier l'aptitude du matériau à conserver dans le temps, d'une part, ses propriétés neutrophages, et, d'autre part, ses propriétés mécaniques, lorsqu'il est maintenu à des températures élevées.Furthermore, the plates are subjected to tests in order to assess the ability of the material to retain over time, on the one hand, its properties neutrophages, and, on the other hand, its mechanical properties, when maintained at high temperatures.

L'aptitude du matériau à conserver ses propriétés neutrophages est appréciée par un test de vieillissement accéléré permettant de simuler le comportement que présenterait le matériau s'il était maintenu pendant 100 000 heures (soit plus de 11 ans) à 150°C. Succinctement, ce test consiste à maintenir les plaques du matériau pendant plusieurs centaines d'heures dans une étuve chauffée à 120°C, 150°C, 180°C ou 205°C, à mesurer à intervalles de temps la masse des plaques et à établir, pour chacune de ces températures, une courbe représentant la perte de masse du matériau en fonction du temps de séjour dans l'étuve. Une courbe maîtresse correspondant à la perte de masse subie par le matériau pour un chauffage de 100 000 heures à la température de 150°C est alors construite par translation des trois autres courbes par rapport à celle obtenue pour un chauffage à 150°C de sorte à ne former qu'une seule courbe continue, ce qui revient, en échelle de temps logarithmique, à multiplier les temps de vieillissement par un coefficient d'accélération, respectivement de 0,1 pour la température de 120°C, de 1 pour la température de 150°C, de 45 pour la température de 180°C et de 90 pour la température de 205°C.The ability of the material to retain its neutrophage properties is assessed by an accelerated aging test to simulate the behavior of the material if it were maintained for 100,000 hours (more than 11 years) at 150 ° C. Briefly, this test consists in keeping the material plates for several hundred hours in an oven heated to 120 ° C, 150 ° C, 180 ° C or 205 ° C, to be measured at time intervals the mass of the plates and to establish, for each of these temperatures, a curve representing the mass loss of the material as a function of the residence time in the oven. A master curve corresponding to the loss of mass undergone by the material for a heating of 100,000 hours at the temperature of 150 ° C. is then constructed by translation of the three other curves with respect to that obtained for heating at 150 ° C. Thus to form a single continuous curve, which amounts, in logarithmic time scale, to multiply the aging times by an acceleration coefficient, respectively by 0.1 for the temperature of 120 ° C, by 1 for the temperature of 150 ° C, 45 for the temperature of 180 ° C and 90 for the temperature of 205 ° C.

Par ailleurs, des analyses élémentaires sont réalisées sur des plaques du matériau pour déterminer la concentration atomique en hydrogène de ce matériau avant sa mise en étuve et après un séjour de 24 heures, 96 heures et 500 heures en étuve chauffée à 150°C.In addition, elemental analyzes are carried out on plates of the material to determine the atomic hydrogen concentration of this material before it is placed in an oven and after a residence of 24 hours, 96 hours and 500 hours in an oven heated to 150 ° C.

En considérant le cas le plus sévère, à savoir que la perte de masse subie par le matériau correspondrait à une perte d'eau, on peut estimer la quantité d'hydrogène restant dans le matériau après plusieurs années de vieillissement à la température de 150°C.Considering the most severe case, namely that the loss of mass undergone by the material would correspond to a loss of water, it is possible to estimate the quantity of hydrogen remaining in the material after several years of aging at the temperature of 150 ° vs.

L'aptitude du matériau à conserver ses propriétés mécaniques est, quant à elle, appréciée par un test de vieillissement thermique qui consiste à maintenir les plaques du matériau pendant 90 heures dans une étuve chauffée à 150°C ou pendant 170 heures dans une étuve chauffée à 250°C et à suivre l'évolution dans le temps l'évolution du module d'Young en flexion et de la contrainte maximale en flexion du matériau que l'on mesure selon la norme NF EN ISO 178.The ability of the material to retain its mechanical properties is, in turn, appreciated by a thermal aging test which consists in keeping the plates of the material for 90 hours in an oven heated to 150 ° C or for 170 hours in a heated oven at 250 ° C and follow the evolution over time the evolution of the flexural Young's modulus and the maximum bending stress of the material, which is measured according to the NF EN ISO 178 standard.

Les résultats de ces tests sont illustrés sur les figures 1, 2 et 3.The results of these tests are illustrated on the Figures 1, 2 and 3 .

Comme le montre la figure 1, qui représente l'évolution de la concentration atomique en hydrogène [H]at (en nombre d'atomes/cm3) du matériau au cours du temps (en heures), telle que déterminée par les analyses élémentaires (courbe) et par des calculs effectués à partir du test de vieillissement accéléré (symbole ◆), la concentration atomique en hydrogène du matériau diminue peu lorsque celui-ci est soumis à une température de 150°C pendant une période de temps très prolongée. Il en résulte que ses propriétés neutrophages sont remarquablement bien conservées.As shown in figure 1 , which represents the evolution of the atomic hydrogen concentration [H] at (in number of atoms / cm 3 ) of the material over time (in hours), as determined by the elementary analyzes (curve) and by Calculations made from the accelerated aging test (symbol ◆), the atomic hydrogen concentration of the material decreases slightly when it is subjected to a temperature of 150 ° C for a very prolonged period of time. As a result, its neutrophage properties are remarkably well preserved.

Par ailleurs, comme le montrent les figures 2 et 3, qui représentent respectivement l'évolution du module d'Young en flexion E (en MPa) et celle de la contrainte maximale en flexion σmax (en MPa) du matériau au cours du temps (en heures), telles qu'obtenues lorsque ce matériau est maintenu pendant 90 heures à 150°C (courbes A) ou pendant 170 heures à 250°C (courbes B), le maintien du matériau pendant plusieurs dizaines d'heures à une température de 150°C ou de 250°C n'entraîne pas de dégradation notable de ses propriétés mécaniques.Moreover, as shown by figures 2 and 3 , which respectively represent the evolution of Young's modulus in bending E (in MPa) and that of the maximum bending stress σ max (in MPa) of the material over time (in hours), as obtained when this material is maintained for 90 hours at 150 ° C (A curves) or for 170 hours at 250 ° C (B curves), holding the material for several tens of hours at a temperature of 150 ° C or 250 ° C n does not cause significant degradation of its mechanical properties.

EXEMPLE 2 : Préparation d'un matériau souple utile selon l'inventionEXAMPLE 2 Preparation of a flexible material useful according to the invention

On procède comme dans l'exemple 1 ci-avant à ceci près que :

  • d'une part, on remplace la résine silicone, qui est utilisée dans cet exemple, par un élastomère silicone liquide à motif méthyl(phényl)siloxane, également sans solvant (référence Elastosil™ RT 601- société Wacker Chemie AG) ; et
  • d'autre part, la réticulation (ou vulcanisation) de l'élastomère silicone est réalisée en laissant les moules pendant 24 heures à température ambiante et en les plaçant ensuite dans une étuve que l'on chauffe d'abord pendant 1 heure à 100°C, puis pendant 1 heure à 150°C.
The procedure is as in Example 1 above except that:
  • on the one hand, the silicone resin, which is used in this example, is replaced by a liquid silicone elastomer having a methyl (phenyl) siloxane unit, also without a solvent (reference Elastosil ™ RT 601-Wacker Chemie AG); and
  • on the other hand, the crosslinking (or vulcanization) of the silicone elastomer is carried out by leaving the molds for 24 hours at room temperature and then placing them in an oven which is first heated for 1 hour at 100 ° C. C, then for 1 hour at 150 ° C.

Après démoulage, les plaques du matériau ainsi obtenu sont soumises à des tests de vieillissement thermique en vue d'apprécier l'aptitude du matériau à conserver dans le temps, d'une part, ses propriétés neutrophages, et, d'autre part, ses propriétés mécaniques, lorsqu'il est maintenu à des températures élevées.After demolding, the plates of the material thus obtained are subjected to thermal aging tests in order to assess the ability of the material to retain over time, on the one hand, its neutrophage properties, and on the other hand, its mechanical properties, when maintained at elevated temperatures.

L'aptitude du matériau à conserver ses propriétés neutrophages est appréciée par un test de vieillissement accéléré identique à celui décrit dans l'exemple 1 ci-avant.The ability of the material to retain its neutrophage properties is appreciated by an accelerated aging test identical to that described in Example 1 above.

L'aptitude du matériau à conserver ses propriétés mécaniques est, quant à elle, appréciée par un test de vieillissement thermique qui consiste à maintenir les plaques du matériau pendant 500 heures dans une étuve chauffée à 150°C ou pendant 200 heures dans une étuve chauffée à 250°C et à suivre l'évolution dans le temps de l'allongement à la rupture A et du module E en traction du matériau que l'on mesure selon la norme NF EN ISO 527-1.The ability of the material to retain its mechanical properties is, in turn, appreciated by a thermal aging test which consists of keeping the plates of the material for 500 hours in an oven heated to 150 ° C or for 200 hours in a heated oven at 250 ° C and to follow the evolution over time of the elongation at break A and the modulus E in tension of the material which is measured according to standard NF EN ISO 527-1.

Les résultats de ces tests sont illustrés sur les figures 4, 5 et 6.The results of these tests are illustrated on the figures 4 , 5 and 6 .

Comme le montre la figure 4, qui représente l'évolution de la concentration atomique en hydrogène [H]at (en nombre d'atomes/cm3) du matériau au cours du temps (en heures), telle que déterminée par les analyses élémentaires (courbe) et par des calculs effectués à partir du test de vieillissement accéléré (symbole ◆), la quantité d'atomes d'hydrogène perdus par ce matériau est très faible (inférieure à 5%) lorsque celui-ci est soumis à une température de 150°C pendant une période de temps très prolongée. Il en résulte que les propriétés neutrophages du matériau sont remarquablement bien conservées.As shown in figure 4 , which represents the evolution of the atomic hydrogen concentration [H] at (in number of atoms / cm 3 ) of the material over time (in hours), as determined by the elementary analyzes (curve) and by calculated from the accelerated aging test (symbol ◆), the quantity of hydrogen atoms lost by this material is very small (less than 5%) when it is subjected to a temperature of 150 ° C during a very prolonged period of time. As a result, the neutrophagic properties of the material are remarkably well preserved.

Par ailleurs, comme le montrent les figures 5 et 6, qui représentent respectivement l'évolution de l'allongement à la rupture A (en %) et celle du module d'Young en traction E (en MPa) du matériau au cours du temps (en heures), telles qu'obtenues lorsque ce matériau est maintenu pendant 500 heures à 150°C (courbes A) et pendant 200 heures à 250°C (courbes B), les propriétés mécaniques du matériau se stabilisent après une centaine d'heures de vieillissement à 150°C.Moreover, as shown by Figures 5 and 6 , which respectively represent the evolution of the elongation at break A (in%) and that of the Young's modulus in traction E (in MPa) of the material over time (in hours), as obtained when this material is maintained for 500 hours at 150 ° C (curves A) and for 200 hours at 250 ° C (curves B), the mechanical properties of the material stabilize after a hundred hours of aging at 150 ° C.

Ces figures montrent également que l'allongement à la rupture d'un matériau à base d'un élastomère silicone reste élevé par rapport à celui de matériaux à base d'une résine thermodurcissable et ce, qu'il s'agisse d'une résine polyester insaturé, vinylester, époxyde ou même silicone. Ceci permet de réduire les risques de fissuration du matériau par dilatation thermique lorsque celui-ci est exposé à des variations importantes de température.These figures also show that the elongation at break of a material based on a silicone elastomer remains high compared to that of materials based on a thermosetting resin and whether it is a resin unsaturated polyester, vinylester, epoxy or even silicone. This reduces the risk of cracking of the material by thermal expansion when it is exposed to significant temperature variations.

RÉFÉRENCES CITÉESREFERENCES CITED

  1. [1][1] US-A-4,134,937US Patent 4,134,937
  2. [2][2] EP-A-0 106 759EP-A-0 106 759
  3. [3][3] WO-A-03/030183WO-A-03/030183
  4. [4][4] WO-A-03/050822WO-A-03/050822
  5. [5][5] WO-A-02/101756WO-A-02/101756
  6. [6][6] KR 1019980078181 B1KR 1019980078181 B1

Claims (15)

  1. Use of a material comprising a solid matrix based on a silicone polymer, in which are dispersed a hydrogenated inorganic filler and a borated inorganic filler, as a neutrophage material, said silicone polymer being a polysiloxane which is formed with one or several siloxane recurrent units and characterized in that the silicon atom is bound to one or two aromatic groups.
  2. Use according to claim 1, wherein the polysiloxane is formed with one or several siloxane recurrent units, each fitting the formula (1) hereafter:
    Figure imgb0004
    wherein:
    R1 represents an aromatic group, while
    R2 represents an alkyl group comprising 1 to 4 carbon atoms or an aromatic group.
  3. Use according to claim 1 or claim 2, wherein the polysiloxane is a homopolymer.
  4. Use according to claim 3, wherein the polysiloxane is a poly[methyl(phenyl)siloxane] or a poly(diphenylsiloxane).
  5. Use according to any of claims 1 to 4, wherein the hydrogenated inorganic filler is selected from among metal hydroxides.
  6. Use according to claim 5, wherein the hydrogenated inorganic filler is selected from among aluminium hydroxide, magnesium hydroxide and mixtures thereof.
  7. Use according to claim 6, wherein the hydrogenated inorganic filler is aluminium hydroxide.
  8. Use according to any of claims 1 to 7, wherein the borated inorganic filler is selected from among zinc borates, boron carbide, boron oxide, boric acid, colemanite and mixtures thereof.
  9. Use according to claim 8, wherein the borated inorganic filler is a zinc borate.
  10. Use according to any of claims 1 to 9, wherein the material has an atomic hydrogen concentration ranging from 3.2x1028 atoms/m3 to 6.3x1028 atoms/m3.
  11. Use according to claim 10, wherein the material has an atomic hydrogen concentration ranging from 4.1x1028 atoms/m3 to 6x1028 atoms/m3.
  12. Use according to any of claims 1 to 11, wherein the material has an atomic boron concentration ranging from 1.9x1027 atoms/m3 to 1.8x1028 atoms/m3.
  13. Use according to claim 12, wherein the material has an atomic boron concentration ranging from 2.1x1027 atoms/m3 to 9x1027 atoms/m3.
  14. Use according to any of claims 1 to 13, wherein the material is a component of a flexible or rigid neutron protection element.
  15. Use according to claim 14, wherein the neutron protective element is an element of a nuclear power station or of a plant for processing irradiated nuclear fuels.
EP15201763.8A 2014-12-23 2015-12-21 Use of a material comprising a solid matrix of a siliconised polymer and inorganic fillers such as neutron-absorbing material Active EP3038113B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1463216A FR3030865A1 (en) 2014-12-23 2014-12-23 USE OF A MATERIAL COMPRISING A SOLID MATRIX BASED ON A SILICONE POLYMER AND INORGANIC LOADS AS MATERIAL NEUTROPHAGE

Publications (2)

Publication Number Publication Date
EP3038113A1 EP3038113A1 (en) 2016-06-29
EP3038113B1 true EP3038113B1 (en) 2017-11-29

Family

ID=53298445

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15201763.8A Active EP3038113B1 (en) 2014-12-23 2015-12-21 Use of a material comprising a solid matrix of a siliconised polymer and inorganic fillers such as neutron-absorbing material

Country Status (3)

Country Link
EP (1) EP3038113B1 (en)
ES (1) ES2659793T3 (en)
FR (1) FR3030865A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2849037C1 (en) * 2025-04-10 2025-10-22 Федеральное государственное бюджетное учреждение науки Ордена Трудового Красного Знамени Институт нефтехимического синтеза им. А.В. Топчиева Российской академии наук (ИНХС РАН) Epoxy x-ray protective material and method for its production

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN120089472B (en) * 2025-03-13 2025-09-19 广州珠江电缆有限公司 Preparation process and application of high temperature resistant and fireproof cable

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4134937A (en) 1974-06-12 1979-01-16 Monsanto Research Corporation Polyester resin composition
FR2534733A1 (en) 1982-10-15 1984-04-20 Commissariat Energie Atomique BORON-CONTAINING NEUTROMPHAGE MATERIAL AND MANUFACTURING METHOD THEREOF
KR100298036B1 (en) * 1997-04-25 2001-11-14 장인순 Silicone Rubber Neutron Shielding Composition
US6608319B2 (en) 2001-06-08 2003-08-19 Adrian Joseph Flexible amorphous composition for high level radiation and environmental protection
FR2830367B1 (en) 2001-10-01 2003-12-19 Transnucleaire NEUTRONIC SHIELDING AND SUB-CRITICITY MAINTAINING MATERIAL BASED ON UNSATURATED POLYESTER
FR2833402B1 (en) 2001-12-12 2004-03-12 Transnucleaire NEUTRONIC SHIELDING AND SUB-CRITICITY MAINTAINING MATERIAL BASED ON VINYLESTER RESIN

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2849037C1 (en) * 2025-04-10 2025-10-22 Федеральное государственное бюджетное учреждение науки Ордена Трудового Красного Знамени Институт нефтехимического синтеза им. А.В. Топчиева Российской академии наук (ИНХС РАН) Epoxy x-ray protective material and method for its production

Also Published As

Publication number Publication date
FR3030865A1 (en) 2016-06-24
EP3038113A1 (en) 2016-06-29
ES2659793T3 (en) 2018-03-19

Similar Documents

Publication Publication Date Title
CA1024680A (en) Vulcanizing at room temperature organopolysiloxanic compositions for elastomers capable of adhering to all kinds of surfaces
KR101873592B1 (en) Curing method for silicone resin composition
CA1228691A (en) Organopolysiloxanic compositions containing polyacyloxysilanes and hard ening very fast to form elastomers in the presence of a promoter of the metallic hydroxide type
US20040209972A1 (en) Dual-cure silicone compounds exhibiting elastomeric properties
US20200010621A1 (en) Two-step curable thermally conductive silicone composition and method for producing same
US8293810B2 (en) Rapid prototyping resin compositions
FR2500842A1 (en) SILICONE RUBBER COMPOSITION FOR COATING PHOTOVOLTAIC ELEMENTS
EP3277758B1 (en) Coating material
JPH03227365A (en) Radiation-curing organosiloxane gel composition and method of using it
WO2011148896A1 (en) Polysiloxane composition, hardened material and optical device
CA1096096A (en) Siloxane elastomer prepared from mercaptoorganopolysiloxanes
EP3038113B1 (en) Use of a material comprising a solid matrix of a siliconised polymer and inorganic fillers such as neutron-absorbing material
EP3161881A1 (en) Layered polymer structures and methods
CN101336383B (en) Impact resistant optical waveguide and method of making same
RU2451704C1 (en) Polydimethylsiloxane based neutron shield composition
US11180598B2 (en) Ultraviolet curable organopolysiloxane composition, silicone gel cured product and method for producing same, and pressure sensor
TWI782998B (en) UV curable polysiloxane adhesive composition and polysiloxane adhesive film
CN104710798B (en) Fluorosilicone rubber composition
Marnot et al. Thermal weathering of 3D-printed lunar regolith simulant composites
JP6957538B2 (en) A method for producing a liquid silicone elastomer composition for a radiation shielding material, a method for producing a liquid silicone elastomer composition for a radiation shielding material, and a radiation shielding silicone rubber molded product.
JP7180684B2 (en) UV curable silicone composition and its cured product
KR20180076337A (en) Composition for organic electronic device encapsulant and encapsulant manufactured by using the same
Donskoi et al. Fluorosiloxane sealants for aviation industry
FR2644619A1 (en) Heat-resistant materials
WO2019023840A1 (en) Ice-phobic coatings

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20161222

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20170711

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 951076

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171215

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: FRENCH

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 3

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602015006332

Country of ref document: DE

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2659793

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20180319

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20171129

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 951076

Country of ref document: AT

Kind code of ref document: T

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180228

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180228

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180301

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602015006332

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171221

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20171231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171221

26N No opposition filed

Effective date: 20180830

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20151221

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181231

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20181231

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20171129

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20180329

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20241227

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20241227

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20241216

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20241219

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20250117

Year of fee payment: 10