FR2556876A1 - Process for the manufacture of structures made of composite materials forming a neutron shielding - Google Patents
Process for the manufacture of structures made of composite materials forming a neutron shielding Download PDFInfo
- Publication number
- FR2556876A1 FR2556876A1 FR8320005A FR8320005A FR2556876A1 FR 2556876 A1 FR2556876 A1 FR 2556876A1 FR 8320005 A FR8320005 A FR 8320005A FR 8320005 A FR8320005 A FR 8320005A FR 2556876 A1 FR2556876 A1 FR 2556876A1
- Authority
- FR
- France
- Prior art keywords
- gadolinium
- neutron
- absorbing material
- manufacture
- composite materials
- 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.)
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Classifications
-
- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21F—PROTECTION AGAINST X-RADIATION, GAMMA RADIATION, CORPUSCULAR RADIATION OR PARTICLE BOMBARDMENT; TREATING RADIOACTIVELY CONTAMINATED MATERIAL; DECONTAMINATION ARRANGEMENTS THEREFOR
- G21F1/00—Shielding characterised by the composition of the materials
- G21F1/02—Selection of uniform shielding materials
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- High Energy & Nuclear Physics (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
L'invention concerne un procédé de 2bracation de structures en matériaux composites formant blindage neutronique. The invention relates to a method of 2bracation of structures made of composite materials forming neutron shielding.
les qualités mécaniques et le faible poids des matériaux composites ont amené son utilisation des engins pour lesquels la diminution du poids est une préoccupation majeure. Aussi les matériaux composites servent-ils à la fabrication de corps de rentrée, de coiffes, de parties de structures dans les industries spatiales et aéronaùtiques. the mechanical qualities and the low weight of composite materials have led to its use of machines for which weight reduction is a major concern. Composite materials are therefore used for the production of reentry bodies, caps, parts of structures in the space and aeronautical industries.
Les risques nucléaires et notamment les effets des hauts flux de neutrons,susceptibles d'autre libérés par les explosions atomiques et les armes à radiation renforcée, sur les armes nucléaires voisines, sur les dispositifs électroniques et sur le personnel ont incité les constructeurs à protéger les installations, armes ou dispositifs essentiels par des blindages neutrophages. Ces blindages sont formés par une feuille ou un dbp8t d'un matériau présentant une section de capture importante vis à vis des neutrons. Le matériau ayant la plus forte section de capture est le gadolinium qui est abondamment utilisé dans le nucléaire pour "lempoisonnement" dans tous les cas où il y a un risque de criticité, par exemple dans le retraitement des combustibles nucléaires. Nuclear risks, and in particular the effects of high neutron fluxes, which may be released by atomic explosions and enhanced radiation weapons, on nearby nuclear weapons, on electronic devices and on personnel have prompted manufacturers to protect essential installations, weapons or devices by neutron shielding These shields are formed by a sheet or a dbp8t of a material having a large capture section with respect to the neutrons. The material with the highest capture section is gadolinium, which is widely used in nuclear power for "poisoning" in all cases where there is a risk of criticality, for example in the reprocessing of nuclear fuels.
L'invention a pour objet un procédé de fabrication de structures en matériau composite destiné 6 à servir de blindage neutronique. The subject of the invention is a method of manufacturing structures made of composite material intended to serve as neutron shielding.
Selon l'invention, le procédé consiste à introduire un matériau neutrophage dans au moins un des composants du matériau composite0
Les explications données ci-apres à titre d'exemple permettront de comprendre commuent l'invention peut entre réalisée.According to the invention, the method consists in introducing a neutron absorbing material into at least one of the components of the composite material.
The explanations given below by way of example will make it possible to understand how the invention can be carried out.
les matériaux composites comportent généralement une charge (fibres ou particules) enrobée de "résine". composite materials generally contain a filler (fibers or particles) coated with "resin".
Les caractéristiques déterminantes d?un composite sont : -la nature des fibres ou de la
charge,
-la nature de la "résine"
d'enrobage (phénolique, époxy...)
-les propriétés de la "résine,
-les propriétés de la charge
(mécaniques, thermiques,
électriques).The defining characteristics of a composite are: -the nature of the fibers or the
charge,
-the nature of the "resin"
coating (phenolic, epoxy ...)
-the properties of the "resin,
-the properties of the filler
(mechanical, thermal,
electric).
Suivant la destination de la structure, le matériau composite est choisi en fonction des caractéristiques désirées. C'est ainsi que dans le cas d'un corps de rentrée une attention particulière sera portée aux propriétés ablatives du composite (matrices multidirectionnelle ou unidirectionnelle) ainsi qu'aux propriétés réfractaires et diélectriques de la charge ou des fibres utilisés,
Ces diverses propriétés sont obtenues en chargeant le composite de nitures, oxydes, siliciures, carbures, borures de-métaux ou de métalloIdes. Depending on the destination of the structure, the composite material is chosen according to the desired characteristics. Thus, in the case of a reentry body, particular attention will be paid to the ablative properties of the composite (multidirectional or unidirectional matrices) as well as to the refractory and dielectric properties of the filler or fibers used,
These various properties are obtained by loading the composite with nitrides, oxides, silicides, carbides, de-metal or metalloid borides.
Jusqu'à présent seules les caractéris
tiques mécaniques, réfractaires et diélectriques ont été développées. C'est ainsi que l'on a obtenu des composites dont les caractéristiques mécaniques sont suscieptibles de rivaliser avec celles des métaux en utilisant des fibres de carbone ou de bore.So far only the characteristics
mechanical, refractory and dielectric ticks have been developed. This is how composites were obtained whose mechanical characteristics are capable of competing with those of metals by using carbon or boron fibers.
Or-le bore est un élément neutrophage dont la section de capture est de tordre de 4000 barns. Or-boron is a neutron absorbing element whose capture section is to twist 4000 barns.
Par suite de la faible épaisseur des fibres de la couche de bore sur les fibres supports (tungstène ou. Owing to the small thickness of the fibers of the boron layer on the support fibers (tungsten or.
graphite) le pouvoir d'arrêt d'un flux de neutrons important est faible et ne peut donner une protection efficace. graphite) the stopping power of a large neutron flux is low and cannot provide effective protection.
Suivant une caractéristique de l'invention on préfère utiliser comme matériau de charge le gadolinium dont la section de capture est de l'ordre de 46000 barns. Il s'agit cependant d'une valeur moyenne. En effet des techniques de préparation isotopique ou d'enrichissement permettraient avec les isotopes 155 et 157 qui sont contenus respectivement à 14,78% et 15,71 dans le gadolinium commerclal, d'obtenir des efficacités nettement plus élevées. According to a characteristic of the invention, it is preferred to use gadolinium as a filler material, the capture section of which is of the order of 46,000 barns. However, this is an average value. In fact, isotopic preparation or enrichment techniques would allow, with the isotopes 155 and 157 which are contained respectively at 14.78% and 15.71 in the commercial gadolinium, to obtain significantly higher efficiencies.
Le gadolinium 155 a une section absolue de 56200 barnspour tout le spectre neutrons, 70000 pour des neutrons de pile et le gadolinium 157, une section absolue de 242000 bats 160000 pour des neutrons de piles. Gadolinium 155 has an absolute section of 56,200 barnsp for the entire neutron spectrum, 70,000 for cell neutrons and gadolinium 157, an absolute section of 242,000 bats 160,000 for cell neutrons.
Le maximum d'efficacité se trouve dans le développement du borure de gadolinium où l'action des deux composants permet une très bonne effioacité dans tout le spectre d'énergie des neutrons. The maximum efficiency is found in the development of gadolinium boride where the action of the two components allows a very good effioacity in the whole spectrum of energy of the neutrons.
Des fibres d'oxyde de gadolinium et de borure de gadolinium présentent des caractéristiques très proches de celles des fibres de bore et un pouvoir d'arrêt vis à vis des neutrons très important
Le gadolinium en tant qutoxyde ou borure est utilisé, selon l'invention, pour la fabrication de fibres entrant dans' les matériaux composites ou bien incorporé dans la matrice dans le cas de matériaux frittes.Fibers of gadolinium oxide and of gadolinium boride have characteristics very similar to those of boron fibers and a very high stopping power with respect to neutrons
Gadolinium as oxide or boride is used, according to the invention, for the manufacture of fibers used in 'composite materials or else incorporated into the matrix in the case of sintered materials.
Les composés du gadolinium obtenus à l'état de fibres ou pulvérulant constituent au moins une partie de la charge de résines utilisées pour la fabrication de boucliers pour la protection du personnel et/ou du matériel susceptibles d'8tre soumis à un flux de neutrons. The gadolinium compounds obtained in the form of fibers or pulverulent constitute at least part of the charge of resins used for the manufacture of shields for the protection of the personnel and / or the material likely to be subjected to a flux of neutrons.
Le procddé de fabrication de structures en matériaux composites formant blindage neutronique consiste à utiliser une charge en un matériau neutrophage, la charge étant de préférence du gadolinium ou un composé chimique du gadolinium. The process for manufacturing structures in composite materials forming neutron shielding consists in using a filler in a neutron-absorbing material, the filler being preferably gadolinium or a chemical compound of gadolinium.
Le gadolinium ou son composé chimique est déposé sous forme d'une couche mince par tout moyen connus sur des fils ou rubans. Les fils ainsi traités sont utilisés dans la fabrication de panneaux ou de structures. Gadolinium or its chemical compound is deposited in the form of a thin layer by any known means on wires or ribbons. The wires thus treated are used in the manufacture of panels or structures.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8320005A FR2556876B1 (en) | 1983-12-14 | 1983-12-14 | PROCESS FOR MANUFACTURING COMPOSITE MATERIAL STRUCTURES FORMING NEUTRONIC SHIELDING |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8320005A FR2556876B1 (en) | 1983-12-14 | 1983-12-14 | PROCESS FOR MANUFACTURING COMPOSITE MATERIAL STRUCTURES FORMING NEUTRONIC SHIELDING |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2556876A1 true FR2556876A1 (en) | 1985-06-21 |
FR2556876B1 FR2556876B1 (en) | 1988-12-02 |
Family
ID=9295157
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8320005A Expired FR2556876B1 (en) | 1983-12-14 | 1983-12-14 | PROCESS FOR MANUFACTURING COMPOSITE MATERIAL STRUCTURES FORMING NEUTRONIC SHIELDING |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2556876B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0258177A1 (en) * | 1986-07-30 | 1988-03-02 | Claude Planchamp | Nuclear-radiation absorbers |
WO1996004408A1 (en) * | 1994-08-01 | 1996-02-15 | The Secretary Of State For Defence | Composite materials |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1169530A (en) * | 1955-08-31 | 1958-12-29 | Improvements to equipment, elements or parts of construction likely to provide protection against radiation | |
GB808726A (en) * | 1955-05-12 | 1959-02-11 | Eltro G M B H & Co Ges Fur Str | Improvements in radiated energy absorbing materials |
US2961415A (en) * | 1956-11-02 | 1960-11-22 | Irving R Axelrad | Settable neutron radiation shielding material |
US2971095A (en) * | 1955-03-23 | 1961-02-07 | Bjorksten Res Lab Inc | Radiation shielding fabric |
FR1440335A (en) * | 1964-08-18 | 1966-05-27 | Bosse Fa Otto | Method of manufacturing a neutron shielding device |
FR1555637A (en) * | 1966-09-30 | 1969-01-31 | ||
US3827982A (en) * | 1964-10-26 | 1974-08-06 | W Hall | Moldable lead composition |
US3950271A (en) * | 1974-04-26 | 1976-04-13 | Allied Chemical Corporation | Nuclear shields |
GB2001676A (en) * | 1977-07-27 | 1979-02-07 | Renault | Composite metallic/non-metallic product |
EP0072550A1 (en) * | 1981-08-14 | 1983-02-23 | Toray Industries, Inc. | A neutron-shielding composite fiber and a method of manufacturing same |
-
1983
- 1983-12-14 FR FR8320005A patent/FR2556876B1/en not_active Expired
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2971095A (en) * | 1955-03-23 | 1961-02-07 | Bjorksten Res Lab Inc | Radiation shielding fabric |
GB808726A (en) * | 1955-05-12 | 1959-02-11 | Eltro G M B H & Co Ges Fur Str | Improvements in radiated energy absorbing materials |
FR1169530A (en) * | 1955-08-31 | 1958-12-29 | Improvements to equipment, elements or parts of construction likely to provide protection against radiation | |
US2961415A (en) * | 1956-11-02 | 1960-11-22 | Irving R Axelrad | Settable neutron radiation shielding material |
FR1440335A (en) * | 1964-08-18 | 1966-05-27 | Bosse Fa Otto | Method of manufacturing a neutron shielding device |
US3827982A (en) * | 1964-10-26 | 1974-08-06 | W Hall | Moldable lead composition |
FR1555637A (en) * | 1966-09-30 | 1969-01-31 | ||
US3950271A (en) * | 1974-04-26 | 1976-04-13 | Allied Chemical Corporation | Nuclear shields |
GB2001676A (en) * | 1977-07-27 | 1979-02-07 | Renault | Composite metallic/non-metallic product |
EP0072550A1 (en) * | 1981-08-14 | 1983-02-23 | Toray Industries, Inc. | A neutron-shielding composite fiber and a method of manufacturing same |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0258177A1 (en) * | 1986-07-30 | 1988-03-02 | Claude Planchamp | Nuclear-radiation absorbers |
WO1996004408A1 (en) * | 1994-08-01 | 1996-02-15 | The Secretary Of State For Defence | Composite materials |
GB2304733A (en) * | 1994-08-01 | 1997-03-26 | Secr Defence | Composite materials |
GB2304733B (en) * | 1994-08-01 | 1998-05-20 | Secr Defence | Composite materials |
US5922460A (en) * | 1994-08-01 | 1999-07-13 | The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain & Northern Ireland Of Defence Evaluation And Research Agency | Composite materials |
Also Published As
Publication number | Publication date |
---|---|
FR2556876B1 (en) | 1988-12-02 |
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