EP2033198A1 - Geschichtetes bleifrei-röntgenschutzmaterial - Google Patents
Geschichtetes bleifrei-röntgenschutzmaterialInfo
- Publication number
- EP2033198A1 EP2033198A1 EP07764839A EP07764839A EP2033198A1 EP 2033198 A1 EP2033198 A1 EP 2033198A1 EP 07764839 A EP07764839 A EP 07764839A EP 07764839 A EP07764839 A EP 07764839A EP 2033198 A1 EP2033198 A1 EP 2033198A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- radiation protection
- layer
- protection material
- radiation
- layers
- 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.)
- Granted
Links
- 239000000463 material Substances 0.000 title claims abstract description 201
- 230000005855 radiation Effects 0.000 claims abstract description 281
- 230000004888 barrier function Effects 0.000 claims abstract description 73
- 239000002131 composite material Substances 0.000 claims abstract description 63
- 239000010410 layer Substances 0.000 claims description 324
- 239000012791 sliding layer Substances 0.000 claims description 42
- 230000003014 reinforcing effect Effects 0.000 claims description 23
- 238000010521 absorption reaction Methods 0.000 claims description 17
- 239000004744 fabric Substances 0.000 claims description 15
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 8
- 239000003365 glass fiber Substances 0.000 claims description 8
- 229910052718 tin Inorganic materials 0.000 claims description 8
- 229910052688 Gadolinium Inorganic materials 0.000 claims description 6
- 229910052797 bismuth Inorganic materials 0.000 claims description 6
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 6
- UIWYJDYFSGRHKR-UHFFFAOYSA-N gadolinium atom Chemical compound [Gd] UIWYJDYFSGRHKR-UHFFFAOYSA-N 0.000 claims description 6
- 229910052684 Cerium Inorganic materials 0.000 claims description 5
- 229910052746 lanthanum Inorganic materials 0.000 claims description 5
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 claims description 5
- 239000004760 aramid Substances 0.000 claims description 4
- 229920003235 aromatic polyamide Polymers 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052721 tungsten Inorganic materials 0.000 claims description 4
- 239000010937 tungsten Substances 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 229910052787 antimony Inorganic materials 0.000 claims description 3
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 229910052779 Neodymium Inorganic materials 0.000 claims description 2
- 229910052777 Praseodymium Inorganic materials 0.000 claims description 2
- 229910052788 barium Inorganic materials 0.000 claims description 2
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 claims description 2
- 229910052792 caesium Inorganic materials 0.000 claims description 2
- TVFDJXOCXUVLDH-UHFFFAOYSA-N caesium atom Chemical compound [Cs] TVFDJXOCXUVLDH-UHFFFAOYSA-N 0.000 claims description 2
- PNDPGZBMCMUPRI-UHFFFAOYSA-N iodine Chemical compound II PNDPGZBMCMUPRI-UHFFFAOYSA-N 0.000 claims description 2
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 2
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 2
- 239000004753 textile Substances 0.000 claims description 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims 3
- 230000001681 protective effect Effects 0.000 description 33
- 239000011159 matrix material Substances 0.000 description 13
- 238000004519 manufacturing process Methods 0.000 description 7
- 150000001875 compounds Chemical class 0.000 description 5
- 238000010276 construction Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 230000002787 reinforcement Effects 0.000 description 5
- 238000004876 x-ray fluorescence Methods 0.000 description 5
- 229920001971 elastomer Polymers 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 238000005259 measurement Methods 0.000 description 4
- 239000000843 powder Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000003313 weakening effect Effects 0.000 description 4
- 239000004952 Polyamide Substances 0.000 description 3
- 238000004026 adhesive bonding Methods 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 239000002657 fibrous material Substances 0.000 description 3
- 239000010408 film Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 229920002647 polyamide Polymers 0.000 description 3
- 229920000728 polyester Polymers 0.000 description 3
- 229920002635 polyurethane Polymers 0.000 description 3
- 239000004814 polyurethane Substances 0.000 description 3
- 210000001685 thyroid gland Anatomy 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000004809 Teflon Substances 0.000 description 2
- 229920006362 Teflon® Polymers 0.000 description 2
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000000806 elastomer Substances 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000002710 gonadal effect Effects 0.000 description 2
- 229910000464 lead oxide Inorganic materials 0.000 description 2
- 230000002611 ovarian Effects 0.000 description 2
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 2
- -1 polytetrafluoroethylene Polymers 0.000 description 2
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 2
- 239000004810 polytetrafluoroethylene Substances 0.000 description 2
- 238000009958 sewing Methods 0.000 description 2
- 229920002994 synthetic fiber Polymers 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 210000001519 tissue Anatomy 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
- 238000002583 angiography Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- UYAHIZSMUZPPFV-UHFFFAOYSA-N erbium Chemical compound [Er] UYAHIZSMUZPPFV-UHFFFAOYSA-N 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 210000002149 gonad Anatomy 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 229920000126 latex Polymers 0.000 description 1
- 239000004816 latex Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 210000005075 mammary gland Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000002324 minimally invasive surgery Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000011241 protective layer Substances 0.000 description 1
- 230000001012 protector Effects 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- 210000001550 testis Anatomy 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 230000001988 toxicity Effects 0.000 description 1
- 231100000419 toxicity Toxicity 0.000 description 1
- 239000011345 viscous material Substances 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
- 238000004846 x-ray emission Methods 0.000 description 1
- NAWDYIZEMPQZHO-UHFFFAOYSA-N ytterbium Chemical compound [Yb] NAWDYIZEMPQZHO-UHFFFAOYSA-N 0.000 description 1
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
- G21F1/12—Laminated shielding materials
Definitions
- the present invention relates to a layered X-ray protection material, and more particularly, to a radiation protection material in which a secondary radiation layer with a low Z radiation protection material and a barrier layer with a high Z radiation protection material are provided.
- Radiation protection materials having a secondary radiation layer with a low-Z radiation protection material and a barrier layer with a high-Z radiation protection material are known from WO 2005/024846 A1, WO 2005/023 116 A1 and DE 1 010 666 A1, but are still used in practice not used.
- Radiation protection materials are used in medical technology for the protection of the treating physicians, but also for the protection of non-irradiated body sites of patients to be screened.
- Typical applications include protective aprons, which are mainly worn by doctors and medical personnel, as well as partial body protection equipment, such as gloves, head protection, thyroid protection, gonad protector, ovarian protection. In particular, the latter three serve the protection of non-exposed parts of the patient to be screened.
- fixed protective devices are located in the immediate vicinity of the patient or the examiner, such as radiation protection curtains and protective shields on X-ray machines.
- Radiation protection clothing in the medical field usually contains lead or lead oxide as protective material.
- lead has disadvantages in terms of the toxicity resulting environmental impact and the relatively high weight. For this reason, efforts have recently been made to make available lead-free radiation protection material and thus lead-free radiation protection clothing as a result.
- Radiation protection materials should have sufficient absorption properties in the energy range of an X-ray tube with a voltage of 60 to 125 kV.
- the absorption properties of the respective radiation protection material are represented by a weakening equilibrium or a weakening factor, eg. B. expressed in the form of the Pb attenuation Equivalent (short: lead equivalent) (International Standard IEC 61331-1, protective devices against diagnostic medical X-radiation).
- the elements used in the lead-free radiation protection materials have in part a very strongly deviating dependence of the absorption of the beam energy.
- some of the elements used for absorption purposes have sufficient absorption in the relevant energy range, a portion of the absorbed energy is distributed spatially distributed as X-ray fluorescence radiation from the lead-free radiation protection material.
- the X-ray fluorescence radiation, the classical scattered radiation and the Compton scattering are collectively referred to as secondary radiation.
- the X-ray fluorescence radiation represents a significant proportion of the secondary radiation.
- combinations of different elements are often used to model the absorption behavior of lead. As has been shown, the lead-free radiation protection materials hitherto on the market have hardly any weight advantage over lead.
- the secondary radiation which consists mainly of X-ray fluorescence (characteristic X-radiation) is effectively shielded by the barrier layer, so that they can not escape from the protective material. Only under this condition, it is possible to achieve a weight advantage of a maximum of about 20% compared to lead.
- the barrier layer serves to absorb the secondary radiation, in particular the high proportion of X-ray fluorescence radiation which arises in the secondary radiation layer during the absorption, in particular of low-energy X-ray radiation.
- the barrier layer is provided close to the body in radiation protection clothing, while the secondary radiation layer is provided as the body-distant layer.
- X-ray or radiation protection clothing is generally - depending on the application - provided in various protection classes, eg. B. 0.25 mm, 0.35 mm, 0.50, 1.0 mm Pb nominal value, it has already been proposed to build radiation protection material with these different protective values by the combination of individual layers in order to ensure easy production.
- a hitherto neglected problem is the fact that in a radiation protection material with a proximal barrier layer and a secondary radiation layer remote from the body, only the secondary radiation directed onto the body of the examiner is absorbed by the barrier layer. This is sufficient for normal X-ray examinations, since the patient is generally alone while taking the picture. This is more problematic, for example, in an operation in which the patient is X-rayed regularly or continuously and the surgeon and / or other medical assistants stay very close to the patient. Medical personnel are relatively well protected by the X-ray protective aprons that each of them wears. The situation is different for the patient who, in addition to the normal x-ray dose, receives the additional dose of secondary radiation emitted by the radiation protection clothing of the medical staff. This problem has received little or no attention so far.
- a radiation protection material which in particular different classes, eg. B. protection of 0.25, 0.35 and 0.50 mm Pb nominal value, can be relatively easily produced and absorbed on both sides - to both the examiner and the patient - outgoing secondary radiation to a considerable extent.
- this object is achieved by a multi-layered, lead-free radiation protection material which has at least two individual composite layers, wherein each individual composite layer has a secondary radiation layer with a low-Z radiation protection material and a barrier layer with a high-Z radiation protection material, and wherein the individual composite layers layers are arranged in the radiation protection material such that in each case a barrier layer is disposed on the two surfaces of the radiation protection material and the respective secondary radiation layer is arranged at a distance from the surface.
- the secondary radiation layers lie in the interior of the radiation protection material, while the barrier layers are each arranged on a surface or oriented towards the surface.
- the X-ray radiation penetrating into the protective material is particularly effectively absorbed by the secondary radiation layer which is arranged inside the lead-free radiation protection material.
- the secondary radiation which forms during this absorption can not escape from the radiation protection material since a barrier layer is provided on each of the two surfaces.
- the layer construction according to the invention comprising at least two individual composite layers brings considerable production advantages.
- a radiation protection material with the desired protective values from a single individual composite layer material of this kind, namely, two such layers forming a radiation protection material of 0.25 mm Pb nominal value, three such individual composite layers a radiation protection material with the protective value of 0.35 mm Pb nominal value form and four individual composite layers radiation protection material with a protective value of 0.50 mm nominal value.
- the individual composite layers can either be processed further during production into the layered radiation protection material having the desired protective value, for example by folding and / or gluing.
- the layer sequence can be connected by gluing. It is also possible to sew the individual layers together.
- connection is to provide the individual layers in a common envelope.
- a "bag” of a suitable material for example textile material or PVC
- the individual layers then hang like a curtain in the bag.
- the bag and / or the individual layers can be sewn together, for example, an edge stitching can be provided. It is also possible to weld the individual layers together. Here, too, edge welding is possible.
- an inner and an outer covering layer which are connected to the individual intermediate layers, for example by sewing or welding. Other connection options can be provided.
- a disadvantage of the construction of the radiation protection material from loosely superposed individual layers is their susceptibility to mechanical damage.
- the radiation protection material is rubbed off.
- This is especially true in the construction of multi-layered individual layers, but generally also for radiation protection materials, which are made only of a thick layer.
- the sliding layer can be provided as a separate layer.
- the sliding layer may also be formed integrally with the layer of radiation protection material.
- a thin Teflon coating may be provided on the layer of radiation protection material.
- These intermediate layers can be applied from the already mentioned Teflon material both separately and, as stated above, as an additional layer on the lead-free material.
- a fiber material for example glass fiber, which is available in very thin layers, as a slip-promoting intermediate layer.
- the radiation protection material it is advantageous in the case of the radiation protection material to provide sliding layers where non-planar adjoining adjacent components lie against one another, to provide sliding layers, in order to reduce friction there, to counteract wear and damage and to avoid impairments of flexibility caused by friction.
- Sliding layers can be provided in all such juxtaposition situations, alternatively only in a part of such juxtaposition situations regarded as more important, in the lower limit case only in a single such juxtaposition situation.
- the respective sliding layer may be a separate layer of its own, for.
- polytetrafluoroethylene film or - preferably light and pliable - fabric made of polyamide or polyester or other plastic fibers or glass fibers.
- the sliding layer can be a stamped part punched out with the desired contour.
- the following possibilities are preferred: combination only in the upper edge region of the sliding layer and / or in the two lateral edge regions or additionally also in the lower edge region. Sewing and gluing are the preferred methods of joining.
- the sliding layer can be combined over a large area or over the entire surface with a radiation protection component, preferably by laminating or in the form of a tissue that is combined with a radiation protection material layer.
- Polytetrafluoroethylene film and preferably soft and pliable fabric of polyamide or polyester or other plastic fibers or glass fibers are preferred.
- the respective sliding layer when combined with the respective radiation protection material layer over a large area or over the entire surface, can additionally function as a reinforcing layer or carrier layer or be the sole reinforcing layer or carrier layer of this radiation protection material layer.
- radiation protection material with at least one described sliding layer is a separate invention and can be advantageously realized even without the features of claim 1, even with lead-containing radiation protection materials and / or with radiation protection materials which do not have a structure with secondary radiation layer (s) and barrier layer (US Pat. en).
- all features disclosed in the application can be used individually or in combination as preferred features together with the sliding layer.
- a single composite layer has a protective value of about 0.25 mm, 0.20 mm, 0.175 mm, or about 0.125 mm Pb rating.
- a single composite layer from which the usual protective values can be built up have a protective value of between 0.05 mm Pb to 0.15 mm Pb nominal value. The smaller the protective value, the thinner and the easier it is to knit
- the individual individual composite layers are produced, and the lighter and also more elastic the corresponding radiation protection garment, since the individual layers each have a low rigidity.
- the individual composite layers may each be essentially identical. Suffice a single type of single composite layer to produce the desired radiation protection material.
- a protective apron with 0.5 mm Pb nominal value can be constructed from 5 identical individual composite layers per 0.100 mm nominal value for the purpose of achieving high wearing comfort (flexibility). It is also possible to use individual composite layers with a different nominal value, eg. B. 0.125 and 0.100 mm Pb are combined to achieve a certain total nominal value of the protective clothing. Thus, a protective layer with a protective value of 0.25 mm Pb nominal value may be made of two individual layers of about 0.125 mm Pb nominal value. But you could also z. B. superior three composite layers with a protective value of slightly less than 0.1 mm Pb nominal value.
- a radiation protection clothing is on the outside and / or inside of the radiation protection material, a cover layer, for.
- the cover layer may be coated with a high-Z material, especially on the inside, be occupied.
- it may be coated with a secondary radiation layer further inside than the barrier layer of high Z material.
- the following secondary radiation layer can also be provided separately from the occupied cover layer and can also have its own reinforcement layer. Several such secondary radiation layers may follow each other separately or integrally. In such a layer sequence, one or more individual composite layer (s) may be provided - but not necessarily.
- a cover layer optionally again occupied, may be provided.
- the single composite layer has a reinforcing layer.
- the reinforcing layer may be disposed between the barrier layer and the secondary beam layer. Alternatively, it may also be arranged on one side of the barrier layer and the secondary radiation layer.
- the reinforcing layer should be relatively tear-resistant in its layer plane and can not easily stretch, in order to avoid that under appropriate tensile load, the relatively thin secondary radiation layer, but in particular the even thinner barrier layer not locally stretched and thereby thinned or even break in extreme cases.
- a film material may be provided as a reinforcing layer.
- the reinforcing layer may comprise a thin, tear-resistant fabric.
- the reinforcing layer may comprise an aramid or a glass fiber material.
- other fiber materials such as plastic, carbon or ceramic fibers or metal filaments, for.
- copper or tungsten filaments may be provided. Tissue can be made from all of these fibers or filaments.
- a material which is particularly well suited to absorbing X-rays, such as copper or tungsten in particular has the additional advantage that it on the one hand increases the absorption effect and on the other hand at the same time provides rigidity.
- the metal filaments, and in particular woven metal filaments have the advantage of providing particularly high strength, but also the advantage of having a certain inherent rigidity, which is particularly important for applications in which the radiation protection material is to be shaped and shaped Form should remain during the application, such as gonadal protection, etc ..
- overprotective devices are used when carrying out very delicate work, which is complicated by the use of radiation protection gloves.
- a so-called over-hand protection is used, which is attached, for example, to the arm of the surgeon or also to the patient and which the surgeon can deform for the respective application in such a way that his unprotected hands are sufficiently protected underneath.
- the reinforcing layer may also be arranged on the outside of a single composite layer or on both outer sides of a single composite layer in each case one reinforcing layer. It is also possible to simultaneously form the reinforcing layer as a sliding-promoting layer.
- the low-Z material of the secondary radiation layer is preferably selected such that it has as uniform as possible a high absorption over the desired energy range of 60 to 125 kV, in particular together with the barrier layer, the selection being independent of the generation of secondary radiation can be done. Especially with radiation protection material, which is to be used only for certain applications that have a somewhat more limited energy range, the selection can also be optimized for this limited energy range.
- the high-Z material of the secondary radiation layer is desirably chosen so that, as far as possible, it provides the maximum absorption for the typical secondary radiation of the secondary radiation layer whose energy is essentially determined from the X-ray emission spectra of the elements of the secondary radiation layer.
- the basis weight of the material is taken into account, in which the desired absorption coefficient is obtained. enough.
- aspects such as manufacturability, miscibility with the matrix material, etc. may also be considered.
- the boundary between low-Z material and high-Z material is approximately at EI- elements of an atomic number Z of 60, the low-Z material having an atomic number of about 39 to 60 and the high-Z material has an atomic number greater than 60, preferably greater than 70. Although the two atomic number ranges 60 overlap, the high Z material is always different from the low Z material to accommodate the different absorption requirements.
- the individual elements of the low-Z material or the high-Z material may be provided in the radiation protection material in the form of a thin film. Typically, however, they will be dispersed in powder form in a matrix material.
- matrix material are rubber, latex, synthetic, flexible or solid polymers or silicone materials.
- the low-Z material may comprise at least one of tin, antimony, iodine, cesium, barium, lanthanum, cerium, praseodymium, neodymium.
- the high Z material of the barrier layer may comprise at least one of the following materials: tantalum, tungsten, bismuth.
- a particularly preferred embodiment contains bismuth in the barrier layer and tin and at least one of the elements lanthanum, cerium or gadolinium in the secondary radiation layer.
- the 0.25 mm nominal Pb radiation protection material is formed from two individual composite layers, while the 0.35 mm Pb nominal radiation protection material is formed from three individual composite layers.
- the individual NEN layers can directly in plant, z. B. adjacent to each other or connected to each other, be provided together. It is also possible to separate the individual layers from one another, for example, by means of an air gap, a woven fabric or another intermediate layer. This generally applies independent of the Pb nominal value.
- the radiation protection material which is formed from three individual compound layers, is constructed asymmetrically, with two barrier layers arranged on the outside and one inside. As a result, it has a surface located closer to the inboard barrier layer than the second surface. With several barrier layers in succession, the next inner barrier layer also contributes to the absorption of secondary radiation from the lower secondary radiation layers.
- the surface closer to the inner barrier layer may be used as the proximal layer facing the examiner in a radiation protective garment. It may therefore be provided to mark three-day radiation protection material and radiation protection material, so that a correct installation is ensured in the radiation protection clothing.
- the tag may be identified by a label, e.g. be colored, or provided by a label.
- the invention further relates to radiation protection clothing comprising a radiation protection material according to the invention and in particular a Strahlenschklei- fertilg, wherein in an asymmetrical structure of the radiation protection material that surface is disposed closer to the body to be protected, in the vicinity of more barrier layers are provided.
- FIG. 1 shows a single compound layer for a radiation protection material according to the present invention
- FIG. 4 shows a schematic representation of a test setup for determining the efficiency of the radiation protection material according to the present invention.
- Fig. 5, 6 and 7 three embodiments of radiation protection materials with sliding layers in section.
- the barrier layer consists of a layer of 0.5 kg / m 2 of bismuth including the associated elastomer matrix and the secondary radiation layer of a layer with 0, 9 kg / m 2 of a tin / gadolinium filling including elastomer matrix.
- the basis weight for tin is 0.7 kg / m 2 and the weight per unit area for gadolinium is 0.2 kg / m 2 , which gives the total surface weight for the secondary blasting layer about 0.9 kg / m 2 .
- the pure matrix weight is 10 to 20%, preferably 12 to 15% of the total basis weight.
- the thickness of a single composite layer of about 0.125 mm Pb rating is between about 0.3 to 0.6 mm, more specifically about 0.40 mm.
- a protective apron with a nominal value of 0.50 mm Pb can be constructed, which has the same weakening as the corresponding lead apron.
- the lead apron with 0.5 mm Pb nominal value then weighs 5.6 kg / m 2 .
- the corresponding lead apron has a pure lead weight of 5.7 kg / m 2 . in addition comes the weight of oxygen when it comes to lead oxide and the weight of the matrix. Therefore, lead aprons with 0.5 mm Pb nominal value usually weigh 7 kg / m 2 .
- the lead-free apron has a weight advantage of 20% compared to a lead apron.
- the reinforcing layer which according to the embodiment is made of a very thin, tear-resistant fabric, for example of glass fibers or aramid.
- the basis weight of a glass filament fabric used is about 25 g / m 2 and thus increases the Schürzenten only insignificantly.
- the entire single composite layer 2 can thus be designed relatively thin and very light. Thus, it has a basis weight of about 1.4 kg / m 2 .
- the three layers of a single composite layer 2 are joined together in the production process.
- the secondary radiation layer 8 can be applied to the reinforcement layer 6 in a first step
- the barrier layer 4 can be applied to the other side of the reinforcement layer 6 in a second operation.
- the single composite layer itself has a relatively high flexibility.
- the choice of matrix material essentially determines the flexibility of the single barrier layer.
- the material of the reinforcing layer also influences the flexibility / rigidity of an individual composite layer. So the glass fiber material is particularly favorable because of its high flexibility. In addition, it is chemically harmless. Aramid material would be conceivable as an alternative to glass fiber. This has rather a somewhat higher rigidity, which may be disadvantageous in particular for use as radiation protection clothing.
- carbon fibers can be used in the reinforcing layer.
- the carbon fibers may additionally or exclusively be embedded in the matrix material.
- FIG. 2 various radiation protection materials 10, 12 and 14 are shown.
- the uppermost radiation protection material 10 is formed from two individual composite layers. 1 shows the layer structure of barrier layer 4, reinforcement layer 6 and secondary radiation layer 8 of the two layer sequences.
- the radiation protection material produced from two individual composite layers 2 is shown in FIG. al 10 is symmetrical.
- the gap 16 shown between the two secondary radiation layers 8 indicates that the two individual composite layers do not necessarily have to be firmly connected to one another in a flat manner.
- each of the two surfaces 18, 20 of the two-layer radiation protection material 10 is formed by a barrier layer 4.
- a three-layer radiation protection material is shown by reference numeral 12. Essentially, what has been said for the two-layer radiation protection material 10 applies. Thus, it can be seen that a third single compound layer has been added from below compared to the two-layer radiation protection material 10, so that a second barrier layer 8 'disposed inside the radiation protection material 12 is closer to the lower surface 20 than the upper surface 18 , In this asymmetrical arrangement, it is preferable to provide the lower surface 20 closer to the skin.
- a four-layer radiation protection material 14 is also shown. Compared with the three-layer radiation protection material 12, a further single composite layer 2 is placed on top of the three-layer layer sequence.
- radiation protection material with different protective values can thus be produced with a relatively low production cost by using only a single single composite layer 2 as the starting material for radiation protection material of various protective values.
- two-layer radiation protection material 10 having a nominal thickness of 0.25 mm Pb, three-layer radiation protection material 12 having a nominal thickness of 35 mm Pb and four-layer radiation protection material 14 having a nominal thickness of 0.50 mm Pb can be produced by multilayering produce.
- Such radiation protection material is suitable for the uses mentioned above.
- it can be used to make radiation protection clothing, in particular aprons, gloves, thyroid protection, gonadal protection, ovarian protection, etc., but also eye protection, shields, etc.
- Such protective curtains can be used stationary or on imageable or mobile racks.
- FIG. 3 shows the individual X-ray components and the effect of a radiation protection clothing with a radiation protection material 10 according to the invention in a schematic representation.
- a radiation protection clothing with a radiation protection material 10 according to the invention in a schematic representation.
- the primarily radiated by the patient 22 radiated radiation 24 strikes the radiation protective clothing 26, typically the radiation protection apron of the examiner 28 and there stimulates fluorescence or secondary radiation, which partially, see arrow 30, is scattered back towards the patient.
- On the side of the examiner 28, 32 denotes the transmitted primary radiation component and 34 shows the secondary radiation on the investigator side. From the schematically shown size dimensions of the individual arrows (which are not true to scale) can be seen that the primary radiation, but also the secondary radiation is not completely absorbed by the radiation protection material, but only a considerable reduction.
- the secondary radiation 30, 34 contains different components from the secondary radiation layer 8, for example the classical scattered radiation, the Compton scattering and the fluorescence radiation.
- the fluorescence radiation makes up the majority of this secondary radiation.
- the energy of the fluorescence radiation K radiation
- This low-energy X-ray mainly pollutes the skin and organs close to the skin.
- the focus here is on the female mammary gland tissue, which is relatively susceptible to radiation, as are the testes in man and the thyroid gland.
- the high-Z radiation protection material of the barrier layer 4 develops only relatively little fluorescence radiation or secondary radiation, since its K absorption edge lies in the high energy range, typically at 70 to 90 keV and consequently is not or only slightly excited in the usual range of application from 60 to 125 kV tube voltage of the X-ray source.
- the two outer barrier layers 4 thus provide effective shielding of the secondary radiation also to the patient 22 body.
- the described effect could be confirmed by measurements as shown in the schematic illustration in FIG. 4.
- 36 denotes the X-ray tube and 38 denotes the diaphragm.
- the X-ray beam goes in the direction of the examiner body represented by a water phantom 40.
- 42 a measuring chamber is referred to, which is spaced at a distance from the radiation protection clothing 26.
- 4 again designates the patient-side and the examiner-side barrier layer, wherein the secondary radiation layer is again denoted by 8.
- the water phantom 40 with a water content of 25 ⁇ 25 ⁇ 15 cm 3 simulates the scattered radiation properties of the body of the examiner.
- the secondary radiation layer of the radiation protection clothing 26 was formed from lead-free material, in particular tin, with a basis weight of 2.0 kg / m 2 .
- the dose was measured with an air kerma measuring chamber 42 at a distance of 0 (body contact), 5, 10, 20 and 30 cm in front of the radiation protection clothing 26, once with a barrier layer of 0.7 kg / m 2 Bismuth once on the patient side and once on the examiner side.
- the difference between the two measurements corresponds to the dose increase due to the secondary radiation generated in the material (eg tin-K radiation). This additional radiation would be applied to the patient when his body surface was at the location of the measuring chamber 42.
- a measuring location between the radiation protection clothing 26 and the water phantom 40 (corresponding to the body of the examiner) was chosen, since the examiner has placed the apron directly on the surface of the body. che carries.
- the barrier layer of 0.7 kg / m 2 bismuth is again arranged on the patient side and once on the examiner side. The difference between the two measurements corresponds to the relative dose decrease due to secondary radiation. Accordingly, the secondary radiation can be reduced to one third by means of a barrier layer on the examiner side - as well as on the patient side.
- the attachment of a double-sided barrier layer as in the radiation protection material 10, 12, 14 according to the present invention combines these two attenuation effects and leads to a significant reduction of the secondary radiation both on the examiner side and on the patient side.
- the radiation protection clothing 26 usually contains the radiation protection material in powder form. If in each case only the elements are mentioned in connection with the embodiment, this relates in particular in each case to the powder form or compounds of the element or of the elements in powder form.
- Radiation protection material with a sliding layer or several sliding layers will be explained in more detail with reference to the exemplary embodiments according to FIGS. 5, 6 and 7.
- the radiation protection material 2 shown in FIG. 5 has three radiation protection components or individual radiation protection layers, namely a barrier layer 4 on the side facing the patient in FIG. 5, a central secondary radiation layer 8, and a barrier layer 4 on the in FIG Fig. 5 right, the examiner closer side.
- Each of the layers 4 and 8 has a reinforcing layer 6, which may be provided anywhere in the middle region of the layer, but also in the region of a surface of the relevant layer.
- a left cover layer 50 and a right cover layer 52 are seen.
- the left cover layer 50 is preferably formed of a strong synthetic fabric with a coating of preferably polyurethane on its left surface to protect the fabric from counter-injected liquid.
- the right-hand cover layer 52 is preferably likewise formed from a strong synthetic fiber fabric, in which case a coating preferably made of polyurethane is optionally provided on the left side of the cover layer 52 in FIG. 5 or on the right side of the cover layer 52 in FIG can.
- Layer spacings where the sliding layers 54 are located are designated in exaggerated size for the sake of clarity. In fact, these distances are in relation to the layer thicknesses small, so that the respective sliding layer 54 is more or less completely in physical contact with the two neighboring layers.
- the sliding layers 54 are each sewn or glued together only in the region of their upper edge with the other radiation protection material. Additional union along the two side edges, namely behind the plane of the drawing and in front of the plane of the drawing, and / or in the area of the lower edge are optionally possible. In addition, it is possible to laminate each of the sliding layers 54 to one of the two adjacent layers.
- the reinforcing layers 6 are optional and do not necessarily have to be present. It is further emphasized that there are embodiments of the radiation protection material 2 in which the left barrier layer 4 is not present. It is further emphasized that, alternatively, the left barrier layer 4 and the secondary radiation layer 8 may be combined to form a single composite layer, preferably in a construction as described in the present application. It is also possible to work with a construction of several such individual composite layers, as described in the present application. A further alternative is the provision of two secondary radiation layers 8 instead of the one drawn secondary radiation layer 8.
- a sliding layer 54 is dispensable, in particular, when the right cover layer 52 is coated on its left side.
- FIG. 6 illustrates that-optionally in a part of the contiguous situations or in all contiguous situations-the sliding layer 54, if a sliding layer 54 is provided at all, is realized in the form of a layer which is combined over a large area or over the entire surface with a component of the radiation protection material 2 can be.
- the left barrier layer 4 is now provided with a sliding layer 54 on its left side
- the secondary radiation layer 8 is with a sliding layer 54 on its right side
- the right barrier layer 4 is provided with a sliding layer on its right side.
- the sliding layers 54 which are combined with a radiation protection component over a large area or over the entire surface are preferably formed by a light, pliable fabric, preferably polyamide fabric or polyester fabric.
- a light, pliable fabric preferably polyamide fabric or polyester fabric.
- Such fabrics are available in basis weights of about 30 g / m2 and above.
- viscous material for. B. mixture of matrix material (in particular polyurethane or rubber) with low-Z material or with high-Z material, has been applied to the fabric and has then come by chemical reaction in the matrix material in the ready state.
- the exemplary embodiment according to FIG. 7 differs from the exemplary embodiment according to FIG. 6 in that the secondary beam layer 8 and the right barrier layer each have their directly assigned sliding layer 54 on the left (instead of the right) surface in FIG. 7 and that the "free Sliding layer 54 of FIG. 6 is not present.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- High Energy & Nuclear Physics (AREA)
- Apparatus For Radiation Diagnosis (AREA)
- Laminated Bodies (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006028958A DE102006028958B4 (de) | 2006-06-23 | 2006-06-23 | Geschichtetes Bleifrei-Röntgenschutzmaterial |
PCT/EP2007/005610 WO2007147642A1 (de) | 2006-06-23 | 2007-06-25 | Geschichtetes bleifrei-röntgenschutzmaterial |
Publications (2)
Publication Number | Publication Date |
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EP2033198A1 true EP2033198A1 (de) | 2009-03-11 |
EP2033198B1 EP2033198B1 (de) | 2014-03-05 |
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EP07764839.2A Active EP2033198B1 (de) | 2006-06-23 | 2007-06-25 | Geschichtetes bleifrei-röntgenschutzmaterial |
Country Status (6)
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US (1) | US7897949B2 (de) |
EP (1) | EP2033198B1 (de) |
JP (1) | JP5461177B2 (de) |
CN (1) | CN101479809B (de) |
DE (1) | DE102006028958B4 (de) |
WO (1) | WO2007147642A1 (de) |
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Also Published As
Publication number | Publication date |
---|---|
JP2009541720A (ja) | 2009-11-26 |
CN101479809B (zh) | 2012-04-18 |
EP2033198B1 (de) | 2014-03-05 |
DE102006028958B4 (de) | 2008-12-04 |
JP5461177B2 (ja) | 2014-04-02 |
US20090272921A1 (en) | 2009-11-05 |
US7897949B2 (en) | 2011-03-01 |
WO2007147642A1 (de) | 2007-12-27 |
CN101479809A (zh) | 2009-07-08 |
DE102006028958A1 (de) | 2007-12-27 |
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