JP2541666B2 - Air carrier for irradiation - Google Patents
Air carrier for irradiationInfo
- Publication number
- JP2541666B2 JP2541666B2 JP1252326A JP25232689A JP2541666B2 JP 2541666 B2 JP2541666 B2 JP 2541666B2 JP 1252326 A JP1252326 A JP 1252326A JP 25232689 A JP25232689 A JP 25232689A JP 2541666 B2 JP2541666 B2 JP 2541666B2
- Authority
- JP
- Japan
- Prior art keywords
- irradiation
- pen
- polyethylene
- air carrier
- present
- 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.)
- Expired - Lifetime
Links
- 239000012535 impurity Substances 0.000 claims description 7
- 239000003054 catalyst Substances 0.000 claims description 5
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052719 titanium Inorganic materials 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- 239000000654 additive Substances 0.000 claims description 2
- 230000000996 additive effect Effects 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims description 2
- 239000002184 metal Substances 0.000 claims description 2
- 238000011160 research Methods 0.000 description 12
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 11
- 229920000642 polymer Polymers 0.000 description 10
- 239000000463 material Substances 0.000 description 9
- 238000012360 testing method Methods 0.000 description 9
- -1 polyethylene Polymers 0.000 description 8
- 230000005855 radiation Effects 0.000 description 8
- 239000004698 Polyethylene Substances 0.000 description 6
- 230000000052 comparative effect Effects 0.000 description 6
- 238000009863 impact test Methods 0.000 description 6
- 229920000573 polyethylene Polymers 0.000 description 6
- QPFMBZIOSGYJDE-UHFFFAOYSA-N 1,1,2,2-tetrachloroethane Chemical compound ClC(Cl)C(Cl)Cl QPFMBZIOSGYJDE-UHFFFAOYSA-N 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- IMNFDUFMRHMDMM-UHFFFAOYSA-N N-Heptane Chemical compound CCCCCCC IMNFDUFMRHMDMM-UHFFFAOYSA-N 0.000 description 3
- MUBZPKHOEPUJKR-UHFFFAOYSA-N Oxalic acid Chemical compound OC(=O)C(O)=O MUBZPKHOEPUJKR-UHFFFAOYSA-N 0.000 description 3
- DNIAPMSPPWPWGF-UHFFFAOYSA-N Propylene glycol Chemical compound CC(O)CO DNIAPMSPPWPWGF-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 150000003609 titanium compounds Chemical class 0.000 description 3
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- 101000579647 Penaeus vannamei Penaeidin-2a Proteins 0.000 description 2
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 2
- KKEYFWRCBNTPAC-UHFFFAOYSA-N Terephthalic acid Chemical compound OC(=O)C1=CC=C(C(O)=O)C=C1 KKEYFWRCBNTPAC-UHFFFAOYSA-N 0.000 description 2
- WNLRTRBMVRJNCN-UHFFFAOYSA-N adipic acid Chemical compound OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 125000005907 alkyl ester group Chemical group 0.000 description 2
- 230000002238 attenuated effect Effects 0.000 description 2
- UJMDYLWCYJJYMO-UHFFFAOYSA-N benzene-1,2,3-tricarboxylic acid Chemical compound OC(=O)C1=CC=CC(C(O)=O)=C1C(O)=O UJMDYLWCYJJYMO-UHFFFAOYSA-N 0.000 description 2
- WPYMKLBDIGXBTP-UHFFFAOYSA-N benzoic acid Chemical compound OC(=O)C1=CC=CC=C1 WPYMKLBDIGXBTP-UHFFFAOYSA-N 0.000 description 2
- YHWCPXVTRSHPNY-UHFFFAOYSA-N butan-1-olate;titanium(4+) Chemical compound [Ti+4].CCCC[O-].CCCC[O-].CCCC[O-].CCCC[O-] YHWCPXVTRSHPNY-UHFFFAOYSA-N 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- QQVIHTHCMHWDBS-UHFFFAOYSA-N isophthalic acid Chemical compound OC(=O)C1=CC=CC(C(O)=O)=C1 QQVIHTHCMHWDBS-UHFFFAOYSA-N 0.000 description 2
- CKFGINPQOCXMAZ-UHFFFAOYSA-N methanediol Chemical compound OCO CKFGINPQOCXMAZ-UHFFFAOYSA-N 0.000 description 2
- 239000012046 mixed solvent Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- RXOHFPCZGPKIRD-UHFFFAOYSA-N naphthalene-2,6-dicarboxylic acid Chemical compound C1=C(C(O)=O)C=CC2=CC(C(=O)O)=CC=C21 RXOHFPCZGPKIRD-UHFFFAOYSA-N 0.000 description 2
- XNGIFLGASWRNHJ-UHFFFAOYSA-N phthalic acid Chemical compound OC(=O)C1=CC=CC=C1C(O)=O XNGIFLGASWRNHJ-UHFFFAOYSA-N 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 238000006068 polycondensation reaction Methods 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- YPFDHNVEDLHUCE-UHFFFAOYSA-N propane-1,3-diol Chemical compound OCCCO YPFDHNVEDLHUCE-UHFFFAOYSA-N 0.000 description 2
- VZGDMQKNWNREIO-UHFFFAOYSA-N tetrachloromethane Chemical compound ClC(Cl)(Cl)Cl VZGDMQKNWNREIO-UHFFFAOYSA-N 0.000 description 2
- ARCGXLSVLAOJQL-UHFFFAOYSA-N trimellitic acid Chemical compound OC(=O)C1=CC=C(C(O)=O)C(C(O)=O)=C1 ARCGXLSVLAOJQL-UHFFFAOYSA-N 0.000 description 2
- LNETULKMXZVUST-UHFFFAOYSA-M 1-naphthoate Chemical compound C1=CC=C2C(C(=O)[O-])=CC=CC2=C1 LNETULKMXZVUST-UHFFFAOYSA-M 0.000 description 1
- 239000005711 Benzoic acid Substances 0.000 description 1
- 229920000339 Marlex Polymers 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 235000011037 adipic acid Nutrition 0.000 description 1
- 239000001361 adipic acid Substances 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229920005601 base polymer Polymers 0.000 description 1
- 235000010233 benzoic acid Nutrition 0.000 description 1
- OEERIBPGRSLGEK-UHFFFAOYSA-N carbon dioxide;methanol Chemical compound OC.O=C=O OEERIBPGRSLGEK-UHFFFAOYSA-N 0.000 description 1
- 125000003178 carboxy group Chemical group [H]OC(*)=O 0.000 description 1
- 239000007795 chemical reaction product Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000001739 density measurement Methods 0.000 description 1
- 150000001991 dicarboxylic acids Chemical class 0.000 description 1
- GYUVMLBYMPKZAZ-UHFFFAOYSA-N dimethyl naphthalene-2,6-dicarboxylate Chemical compound C1=C(C(=O)OC)C=CC2=CC(C(=O)OC)=CC=C21 GYUVMLBYMPKZAZ-UHFFFAOYSA-N 0.000 description 1
- USIUVYZYUHIAEV-UHFFFAOYSA-N diphenyl ether Natural products C=1C=CC=CC=1OC1=CC=CC=C1 USIUVYZYUHIAEV-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000005886 esterification reaction Methods 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 235000019256 formaldehyde Nutrition 0.000 description 1
- 125000000524 functional group Chemical group 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000009477 glass transition Effects 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- XXMIOPMDWAUFGU-UHFFFAOYSA-N hexane-1,6-diol Chemical compound OCCCCCCO XXMIOPMDWAUFGU-UHFFFAOYSA-N 0.000 description 1
- 229920001519 homopolymer Polymers 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 229920005684 linear copolymer Polymers 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- WPUMVKJOWWJPRK-UHFFFAOYSA-N naphthalene-2,7-dicarboxylic acid Chemical class C1=CC(C(O)=O)=CC2=CC(C(=O)O)=CC=C21 WPUMVKJOWWJPRK-UHFFFAOYSA-N 0.000 description 1
- SLCVBVWXLSEKPL-UHFFFAOYSA-N neopentyl glycol Chemical compound OCC(C)(C)CO SLCVBVWXLSEKPL-UHFFFAOYSA-N 0.000 description 1
- 235000006408 oxalic acid Nutrition 0.000 description 1
- WXZMFSXDPGVJKK-UHFFFAOYSA-N pentaerythritol Chemical compound OCC(CO)(CO)CO WXZMFSXDPGVJKK-UHFFFAOYSA-N 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000005809 transesterification reaction Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Landscapes
- Polyesters Or Polycarbonates (AREA)
Description
【発明の詳細な説明】 産業上の利用分野 本発明は放射線照射用に適したポリエチレン−2,6−
ナフタレンカルボキシレート製気送子に関するものであ
る。より詳細には、各種物質への放射線照射のため、個
体状の物質の場合にはそのまま入れることができ、液体
状又は気体状の物質又はそれらの混合物の場合にはガラ
スアンプル又はプラスチックアンプルに封入したものを
入れることによって、被照射物質の耐放射線性,化学反
応域は物理的変化を研究するのに必要な容器(気送子)
に関するものである。TECHNICAL FIELD OF THE INVENTION The present invention relates to polyethylene-2,6-
The present invention relates to a naphthalenecarboxylate air carrier. More specifically, for irradiation of various substances, it can be put as it is in the case of solid substances, and enclosed in glass or plastic ampoules in the case of liquid or gaseous substances or mixtures thereof. A container (air carrier) necessary for studying physical changes in radiation resistance and chemical reaction area of irradiated material
It is about.
従来技術とその問題点 従来、プラスチックからなる気送子の材料としてポリ
エチレンが使われている。ポリエチレン容器の場合、こ
の重合体は放射線には比較的弱く、照射によって比較的
短時間で劣化して脆くなり、特に原子炉照射のような高
線量の照射条件下では短時間で使用に耐えなくなるとい
う問題があった。Conventional technology and its problems Conventionally, polyethylene has been used as a material for a pneumatic carrier made of plastic. In the case of polyethylene containers, this polymer is relatively vulnerable to radiation, and upon irradiation it deteriorates and becomes brittle in a relatively short time, making it unusable in a short time, especially under high dose irradiation conditions such as reactor irradiation. There was a problem.
そして、長時間の高線量放射線の照射に耐えるもの、
或は更に繰り返し使用に耐えるもの及び変性しない材料
よりなる気送子が必要とされている。And ones that can withstand high dose radiation for a long time,
Alternatively or additionally, there is a need for an air carrier made of a material that withstands repeated use and does not denature.
また、気送子入りの材料をたとえば原子炉内で中性子
線により照射すると、気送子に含まれている元素が放射
化されることがある。この現象を回避するため、被照射
物質を照射後気送子から直ちに取り出して他のテストに
供するような場合には現実の問題として非常に不便であ
り、気送子そのものは放射化されない又は放射化された
としても、放射能が短時間で減衰するような材料が切望
されている。Further, when a material containing an air carrier is irradiated with a neutron beam in a nuclear reactor, for example, an element contained in the air carrier may be activated. In order to avoid this phenomenon, it is very inconvenient as a real problem when the irradiated substance is immediately taken out from the air carrier after irradiation and used for other tests, and the air carrier itself is not activated or emitted. Even if it is made into a material, there is a long-felt need for a material whose radioactivity decays in a short time.
問題点を解決する手段 本発明者は前記欠点のない放射線照射気送子を提供す
べく研究を行ない、特定の特性をもつようにしたポリエ
チレン−2,6−ナフタレンジカルボキシレート(以下PEN
−2,6と略記する)よりなる気送子が照射用容器として
極めて適していることを見出し、本発明に到達したもの
である。Means for Solving the Problems The present inventor has conducted research to provide an irradiation carrier which does not have the above-mentioned drawbacks, and has made polyethylene-2,6-naphthalenedicarboxylate (hereinafter referred to as PEN) having specific characteristics.
The present invention has been accomplished by finding that an air carrier made of (abbreviated as -2, 6) is extremely suitable as an irradiation container.
即ち、本発明は、極限粘度数が0.45〜0.90のポリエチ
レン−2,6−ナフタレンジカルボキシレートよりなり、
密度が1.345g/cm3以下であり、かつ触媒残渣又は添加剤
としてチタニウムを50ppm以下の濃度で含み、実質的に
他の金属不純物を含まない放射線照射用気送子である。That is, the present invention has an intrinsic viscosity of 0.45 to 0.90 polyethylene-2,6-naphthalenedicarboxylate,
It is an air carrier for irradiation which has a density of 1.345 g / cm 3 or less, contains titanium as a catalyst residue or an additive at a concentration of 50 ppm or less, and is substantially free of other metal impurities.
発明の気送子を構成する素材である重合体は、その構
成単位が実質的にエチレン−2,6−ナフタレンジカルボ
キシレートから構成されているものであればよく、PEN
−2,6のみならず、少量例えば10モル%以下、好ましく
は5モル%以下の第3成分によって変性されたエチレン
−2,6−ナフタレンカルボキシレート変性重合体も含ま
れる。PEN−2,6は一般にナフタレン−2,6−ジカルボン
酸又はその機能的誘導体、及びエチレングリコール又は
その機能的誘導体を、触媒の存在下で、適当な反応条件
の下に結合せしめることによって合成される。また、変
性重合体としてはこのPEN−2,6の重合完結前に適当な1
種又は2種以上の第3成分変性剤を添加し共重合又は混
合ポリエステルとしたものが挙げられる。The polymer, which is the material constituting the pneumatic carrier of the invention, may be any polymer whose structural unit is substantially composed of ethylene-2,6-naphthalene dicarboxylate, and PEN
Not only -2,6 but also a small amount, for example, 10 mol% or less, preferably 5 mol% or less, of an ethylene-2,6-naphthalenecarboxylate-modified polymer modified with a third component are included. PEN-2,6 is generally synthesized by combining naphthalene-2,6-dicarboxylic acid or its functional derivative and ethylene glycol or its functional derivative in the presence of a catalyst under suitable reaction conditions. It In addition, as a modified polymer, it is necessary to prepare a suitable polymer before completion of the polymerization of PEN-2,6.
One or two or more types of third component modifiers are added to form a copolymerized or mixed polyester.
適当な第3成分としては、2価のエステル形成官能基
を有する化合物、例えばシュウ酸,アジピン酸,フタル
酸,イソフタル酸,テレフタル酸,ナフタレン−2,7−
ジカルボン酸,ジフエニルエーテルカルボン酸等のジカ
ルボン酸又はその低級アルキルエステル:P−オキシ安息
香酸,P−オキシエトキシ安息香酸の如きオキシカルボン
酸又はその低級アルキルエステル:あるいはプロピレン
グリコール,トリメチレングリコール,テトラメチレン
グリコール,ヘキサメチレングリコール,ネオペンチル
グリコールの如き2価アルコール類等の化合物があげら
れる。Suitable third component is a compound having a divalent ester-forming functional group such as oxalic acid, adipic acid, phthalic acid, isophthalic acid, terephthalic acid, naphthalene-2,7-
Dicarboxylic acids such as dicarboxylic acids and diphenyl ether carboxylic acids or lower alkyl esters thereof: oxycarboxylic acids such as P-oxybenzoic acid and P-oxyethoxybenzoic acid or lower alkyl esters thereof: propylene glycol, trimethylene glycol, tetra Examples thereof include compounds such as dihydric alcohols such as methylene glycol, hexamethylene glycol and neopentyl glycol.
またPEN−2,6又はその変性重合体は、例えば、安息香
酸,メトキシポリアルキレングリコールなどの一官能性
化合物によって、末端の水酸基及び/又はカルボキシル
基を封鎖したものであってもよく、あるいは、例えば極
く少量のグリセリン,ペンタエリストールの如き三官能
以上の多官能エステル形成化合物で実質的に線状の共重
合体が得られる範囲内で変性されたものでもよい。本発
明における基体ポリマーはテトラクロルエタン/フェノ
ール[6/4(重合比)]混合溶媒中にて35℃で測定した
極限粘度数が0.45〜0.90のものである。特に極限粘度数
が0.55〜0.70のものが物性上すぐれているので好まし
い。Further, PEN-2,6 or a modified polymer thereof may be, for example, benzoic acid, a monofunctional compound such as methoxypolyalkylene glycol in which a terminal hydroxyl group and / or a carboxyl group is blocked, or For example, it may be modified with a very small amount of a trifunctional or higher-functional polyfunctional ester-forming compound such as glycerin or pentaerythritol within the range where a substantially linear copolymer is obtained. The base polymer in the present invention has an intrinsic viscosity of 0.45 to 0.90 measured at 35 ° C. in a tetrachloroethane / phenol [6/4 (polymerization ratio)] mixed solvent. Particularly, those having an intrinsic viscosity of 0.55 to 0.70 are preferable because they have excellent physical properties.
本発明におけるPEN−2,6は例えば次のようにして合成
することができる。PEN-2,6 in the present invention can be synthesized, for example, as follows.
ジメチル−2,6−ナフタレンジカルボキシレートと
エチレングリコールを反応槽内でチタン化合物を触媒と
して常法もしくは加圧下でエステル交換反応を行ないさ
らに減圧下にて重縮合反応を行なってPEN−2,6を得る方
法、 2,6−ナフタレンジカルボン酸とエチレングリコー
ルをチタン化合物を触媒として常法もしくは加圧下で直
接エステル化反応を行ない、さらに減圧下にて重縮合反
応を行なってPEN−2,6を得る方法。Dimethyl-2,6-naphthalenedicarboxylate and ethylene glycol were used in a reaction vessel with a titanium compound as a catalyst to carry out a transesterification reaction under a conventional method or under pressure, and then a polycondensation reaction under reduced pressure to perform PEN-2,6. To obtain PEN-2,6 by subjecting 2,6-naphthalenedicarboxylic acid and ethylene glycol to a titanium compound as a catalyst for a direct esterification reaction under a conventional method or under pressure, and further performing a polycondensation reaction under reduced pressure. How to get.
なおチタン化合物としてはテトラブチルチタネートあ
るいはトリメリット酸,ヘミメリット酸等とチタンテト
ラブトキシド等の反応生成物であるカルボン酸チタン等
が挙げられる。Examples of the titanium compound include tetrabutyl titanate, trimellitic acid, hemimellitic acid, and titanium carboxylate which is a reaction product of titanium tetrabutoxide and the like.
本発明は、前記の如きポリマーから成形された気送子
である。The present invention is a pneumatic carrier molded from the polymer as described above.
前記ポリマーから本発明における気送子を作成するに
は従来公知の溶融射出成形法を用いることができる。A conventionally known melt injection molding method can be used to form the pneumatic carrier in the present invention from the polymer.
即ち、ホモポリマー又は変性重合体からなるPEN−2,6
を280℃〜310℃の温度で溶融し、金型内に射出して、冷
却固化して密度が1.345g/cm3以下となるように成形する
のが1つの方法である。That is, PEN-2,6 consisting of a homopolymer or a modified polymer
Is melted at a temperature of 280 ° C. to 310 ° C., injected into a mold, solidified by cooling, and molded to have a density of 1.345 g / cm 3 or less.
このようにして成形時の結晶化を抑制して耐照射性を
高め、外径15〜20mm、長さ約60mm〜80mm、厚み約1.5〜2
m程度の寸法からなる円筒状の容器を形成する。In this way, crystallization during molding is suppressed and irradiation resistance is increased, with an outer diameter of 15 to 20 mm, a length of about 60 mm to 80 mm, and a thickness of about 1.5 to 2
A cylindrical container having a size of about m is formed.
本発明の効果 本発明のPEN−2,6よりなる気送子を放射線照射用とし
て用いる場合、以下に掲記するような利点がある。EFFECTS OF THE INVENTION When the pneumatic carrier made of PEN-2,6 of the present invention is used for irradiation, it has the following advantages.
1.ポリエチレンよりなる気送子よりも劣化が著しく少な
いので、高線量率の照射下での使用が可能である。特に
原子炉照射用の気送子に適している。1. Since it is remarkably less deteriorated than an air carrier made of polyethylene, it can be used under irradiation with a high dose rate. In particular, it is suitable as a pneumatic carrier for nuclear reactor irradiation.
2.本発明よりなる気送子は照射化された場合放射能の減
衰が極めて大きいので、被照射物の照射後の取扱いが容
易になる利点がある。2. The air carrier according to the present invention has an extremely large attenuation of radioactivity when irradiated, and therefore has an advantage of facilitating handling after irradiation of the irradiated object.
3.低温下、例えばドライアイスメタノール系の温度条件
下でも脆化しないので、低温下での使用が可能である。3. It can be used at low temperature because it does not become brittle even under low temperature, for example, dry ice methanol temperature conditions.
4.ガラス転位温度が高いので100℃程度の比較的高い温
度での使用も可能である。4. Since the glass transition temperature is high, it can be used at a relatively high temperature of about 100 ° C.
実施例 以下、実施例を挙げて本発明を更に説明する。なお、
本発明における特性は次のようにして測定したものであ
る。EXAMPLES Hereinafter, the present invention will be further described with reference to examples. In addition,
The characteristics in the present invention are measured as follows.
(イ) 極限粘度数 本発明において言う極限粘度数とはテトラクロルエタ
ン/フェノールの重量比が6:4の混合溶媒中で35℃で測
定した値から算出したものである。(A) Intrinsic viscosity number In the present invention, the intrinsic viscosity number is calculated from the value measured at 35 ° C. in a mixed solvent of tetrachloroethane / phenol in a weight ratio of 6: 4.
(ロ) 密度 成形品から小片を切りとり密度測定用のサンプルとし
た。密度は四塩化炭素〜n−ヘプタン系の密度勾配管に
より25℃にて測定した。(B) Density A small piece was cut from the molded product and used as a sample for density measurement. The density was measured at 25 ° C. with a density gradient tube of carbon tetrachloride to n-heptane system.
(ハ) 耐放射線性テスト PEN−2,6並びに他の比較材料よりなるテストピース又
は気送子を作成し日本原子力研究所のJRR−2気送管を
用い照射孔の中性子線束5.5×1013〜8.0×1013n/cm2・s
ecで照射した。中性子照射されたテストピースの放射能
は電離箱型線量率計(IC−247)又はGM線量率計で測定
した。(C) Radiation resistance test PEN-2, 6 and a test piece or pneumatic element made of other comparative materials were prepared and the neutron flux of the irradiation hole was 5.5 × 10 13 using the JRR-2 pneumatic tube of the Japan Atomic Energy Research Institute. ~ 8.0 × 10 13 n / cm 2・ s
irradiated with ec. The radioactivity of the neutron-irradiated test piece was measured by an ionization chamber type dose rate meter (IC-247) or a GM dose rate meter.
(ニ) 衝撃試験 JIS K−7111に準じてテストピースを作成し衝撃テ
ストを実施した。(D) Impact test A test piece was prepared according to JIS K-7111 and an impact test was performed.
その際試験装置として東洋製機製作所製のシャルピー
・衝撃試験機を用いた。At that time, a Charpy / impact tester manufactured by Toyo Seisakusho was used as a test device.
実施例及び比較例 不純物の含有量としてチタニウム15ppmを含み他の不
純物は実質的に含まないポリエチレン−2,6−ナフタレ
ンジカルボキシレートを合成した。また、不純物含有量
として亜鉛55ppmを含む他の不純物は実質的に含まない
ポリエチレン−2,6−ナフタレンジカルボキシレートを
合成した。更に不純物含有量としてアンチモン302ppm,
コバルト49ppm,リン83ppmを含むポリエチレン−2,6−ナ
フタレンジカルボキシレートを合成した。これらPEN−
2,6以外にポリエチレンMarlex50を用いた。PEN−2,6を3
00℃にて溶融し、所定温度に保持した金型中に押出し、
厚み3.2mm,幅13mm,長さ64mm,ノッチ付きの形状のテスト
ピースを作った。Examples and Comparative Examples Polyethylene-2,6-naphthalenedicarboxylate containing 15 ppm of titanium as an impurity content and substantially free of other impurities was synthesized. In addition, polyethylene-2,6-naphthalenedicarboxylate containing 55 ppm of zinc as an impurity content and substantially free of other impurities was synthesized. Furthermore, as an impurity content, antimony 302 ppm,
Polyethylene-2,6-naphthalenedicarboxylate containing 49ppm cobalt and 83ppm phosphorus was synthesized. These PEN−
In addition to 2,6, polyethylene Marlex 50 was used. PEN-2, 6 to 3
It is melted at 00 ℃ and extruded into a mold kept at a predetermined temperature.
A test piece with a thickness of 3.2 mm, a width of 13 mm, a length of 64 mm, and a notch was made.
一方、市販のポリエチレンMalex50(溶融指数約5)
を190℃で溶融し、上記と同様の方法で同じ形状の気送
管を作った。On the other hand, commercially available polyethylene Malex50 (melting index about 5)
Was melted at 190 ° C., and a pneumatic tube of the same shape was made by the same method as above.
これらの成形品を原子炉照射部に送り込み所定線量で
所定時間照射した後、各種テストに供した。These molded products were sent to a reactor irradiation part and irradiated with a predetermined dose for a predetermined time, and then subjected to various tests.
表1に結果を示した。実施例1に示した本発明の気送
子は高い照射線量においても衝撃試験値の低下が少なく
放射線量率の減衰が大きく、実用に充分耐えるものであ
った。比較例1は実施例1と同一の組成のPEN−2,6を用
いたものであるが、テストピースの密度が大きいため
(結晶化が進んでいるため)衝撃試験値の低下が著しか
った。 The results are shown in Table 1. The pneumatic carrier of the present invention shown in Example 1 showed a small decrease in the impact test value even at a high irradiation dose, a large attenuation of the radiation dose rate, and was sufficiently durable for practical use. Comparative Example 1 uses PEN-2,6 having the same composition as that of Example 1, but the impact test value was significantly lowered because the density of the test piece was large (because crystallization progressed).
比較例2は衝撃試験値の低下は少ないが、放射線量率
の減衰が起こりにくいので本発明の目的を達成すること
ができない。比較例3は放射線量率が大きく取扱いがで
きず衝撃テストは中止した。比較例4は従来使用されて
いるポリエチレンである。放射線の線量率は減衰が大き
いが、極めて短時間で材料が脆化するという欠点があ
る。In Comparative Example 2, the impact test value does not decrease much, but the radiation dose rate is less likely to be attenuated, so that the object of the present invention cannot be achieved. In Comparative Example 3, the radiation dose rate was too high to handle, and the impact test was stopped. Comparative Example 4 is a conventionally used polyethylene. Although the radiation dose rate is greatly attenuated, there is a drawback that the material becomes brittle in an extremely short time.
なお、実施例1に示した特性をもつ気送子を作成し、
原子炉で中性子を2.6×1018照射したが脆化することは
なく、実用に供することができるものであることがわか
った。上記の如く本発明の放射線照射用気送子は極めて
有用なものである。In addition, by creating an air carrier having the characteristics shown in Example 1,
The reactor was irradiated with neutrons at 2.6 × 10 18 , but it did not become brittle, and it was found that it could be put to practical use. As described above, the pneumatic carrier for irradiation of the present invention is extremely useful.
フロントページの続き (72)発明者 有金 賢次 茨城県那珂郡東海村白方字白根2番地の 4 日本原子力研究所東海研究所内 (72)発明者 信田 重夫 茨城県那珂郡東海村白方字白根2番地の 4 日本原子力研究所東海研究所内 (72)発明者 藁谷 兵太 茨城県那珂郡東海村白方字白根2番地の 4 日本原子力研究所東海研究所内 (72)発明者 瀬口 忠男 群馬県高崎市綿貫町1233番地 日本原子 力研究所高崎研究所内 (72)発明者 青山 功 茨城県那珂郡東海村白方字白根2番地の 4 日本原子力研究所東海研究所内 (56)参考文献 特開 平2−278200(JP,A) 特開 平3−188399(JP,A)Front Page Continuation (72) Inventor Kenji Arikane 2 Shirane, Shikata, Tokai-mura, Naka-gun, Ibaraki Prefecture 4 Inside the Tokai Research Institute, Japan Atomic Energy Research Institute (72) Shigeo Shinda Shirahone, Shikata-kata, Naka-gun, Ibaraki Prefecture No. 2 4 Inside the Japan Atomic Energy Research Institute Tokai Research Institute (72) Inventor Hyota Waraya, Shirahane, Shirahane, Tokai-mura, Naka-gun, Ibaraki Prefecture 4 No. 4 Inside the Japan Atomic Energy Research Institute Tokai Research Institute (72) Inventor Tadao Seguchi Takasaki Gunma Prefecture 1233, Watanuki-cho, Japan Inside the Takasaki Research Institute, Japan Atomic Energy Research Institute (72) Inventor Isao Aoyama 4 Shirane, Shirahane, Tokai-mura, Naka-gun, Ibaraki Prefecture 4 Inside the Tokai Research Institute, Japan Atomic Energy Research Institute (56) -278200 (JP, A) JP-A-3-188399 (JP, A)
Claims (1)
キシレートよりなる成形品であって、極限粘度数が0.45
〜0.90かつ密度が1.345g/cm3以下であり、触媒残渣又は
添加剤としてチタニウムを50ppm以下の濃度で含み、実
質的に他の金属不純物を含まない放射線照射用気送子。1. A molded article made of polyethylene-2,6-naphthalene dicarboxylate having an intrinsic viscosity of 0.45.
A gas atomizer for irradiation, which has a density of up to 0.90 and a density of 1.345 g / cm 3 or less, contains titanium as a catalyst residue or an additive at a concentration of 50 ppm or less, and is substantially free of other metal impurities.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1252326A JP2541666B2 (en) | 1989-09-29 | 1989-09-29 | Air carrier for irradiation |
DE69015257T DE69015257T2 (en) | 1989-04-20 | 1990-04-18 | Sample container for radiation. |
EP90107372A EP0400315B1 (en) | 1989-04-20 | 1990-04-18 | Sample container for radiation |
US07/510,688 US5112659A (en) | 1989-04-20 | 1990-04-18 | Rabbit for radiation |
KR1019900005598A KR0124807B1 (en) | 1989-04-20 | 1990-04-20 | Rabbit for radiation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1252326A JP2541666B2 (en) | 1989-09-29 | 1989-09-29 | Air carrier for irradiation |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH03188400A JPH03188400A (en) | 1991-08-16 |
JP2541666B2 true JP2541666B2 (en) | 1996-10-09 |
Family
ID=17235709
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1252326A Expired - Lifetime JP2541666B2 (en) | 1989-04-20 | 1989-09-29 | Air carrier for irradiation |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2541666B2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7487043B2 (en) | 2004-08-30 | 2009-02-03 | Adams Phillip M | Relative positioning system |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07119840A (en) * | 1993-10-26 | 1995-05-12 | Tanken Seal C-Kou:Kk | Segment ring and segment seal |
-
1989
- 1989-09-29 JP JP1252326A patent/JP2541666B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH03188400A (en) | 1991-08-16 |
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