JPS6313125B2 - - Google Patents
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- Publication number
- JPS6313125B2 JPS6313125B2 JP4109881A JP4109881A JPS6313125B2 JP S6313125 B2 JPS6313125 B2 JP S6313125B2 JP 4109881 A JP4109881 A JP 4109881A JP 4109881 A JP4109881 A JP 4109881A JP S6313125 B2 JPS6313125 B2 JP S6313125B2
- Authority
- JP
- Japan
- Prior art keywords
- zirconium
- layer
- wall thickness
- zirconium alloy
- composite
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B17/00—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
- G01B17/02—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations for measuring thickness
- G01B17/025—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations for measuring thickness for measuring thickness of coating
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Length Measuring Devices Characterised By Use Of Acoustic Means (AREA)
Description
本発明は原子炉の中枢部を構築するのに用いら
れる純ジルコニウム(以下ジルコニウムという)
とジルコニウム合金の複合材、特に核燃料を封入
するジルコニウム合金よりなる管状被覆材(以下
被覆管という)の内面にジルコニウム層の金属障
壁を内張りした複合材の肉厚を測定する方法に関
する。
現在設計され、製造され又は運転されている動
力炉用原子炉の核燃料要素は、耐食性、非反応性
かつ良熱伝導性を備えた被覆管の内部に核燃料物
質を封入するのが現状である。このような核燃料
要素を一定間隔に格子状に組立てて核燃料集合体
とし、これら核燃料集合体を適当数組合せて自己
持続型核分裂反応の可能な核分裂連鎖反応集合体
や炉心が形成されており、この炉心は冷却剤が通
過する原子炉容器内に収められる。
このような原子炉の中枢部に、核燃料を収める
被覆管が用いられる主要な目的は、第一に核燃料
と冷却剤又は核燃料と減速剤との化学反応を防止
することにあり、第二には一部が気体である放射
性核分裂生成物が、燃料から冷却剤又は減速剤の
中に漏れ出るのを防止することにある。普通に用
いられている被覆管は、ステンレス鋼やジルコニ
ウム合金が主要なものとされている。
被覆管として、ある種の金属又は合金を使用し
て、核燃料要素の製造や運転をする場合、特定の
条件下でこれらの被覆管に機械的又は化学的反応
が生ずることから種々の問題が起つている。ジル
コニウム及びその合金は、定常条件下では優秀な
核燃料被覆管である。その理由は、ジルコニウム
及びその合金は、中性子吸収断面積が小さく、更
に、約400℃以下の温度では、原子炉冷却剤及び
減速剤として普通に使用される純水又は水蒸気の
存在下にあつても強度に優れ、延在を有し、極め
て安定であつて、かつ非反応性を具備しているた
めである。
しかし、核燃料要素の挙動として、核燃料、被
覆管及び核分裂反応中に生成される核分裂生成物
間の相互作用により、被覆管が脆化し、ついには
割れが生じるという問題が明らかになつた。この
望ましくない挙動は、更に燃料と被覆管との熱膨
張差に基づく局部的な機械的応力によつて促進さ
れることが確められた。原子炉の運転中に、核分
裂反応によつて核分裂生成物が核燃料から放出さ
れ、それが被覆管の表面に存在し、ヨウ素やカド
ミウムなどの特定核分裂生成物が存在するとき、
被覆管は局部応力及び歪みの作用により応力腐食
割れが生じるのである。
このような障害を防止する方策として、被覆管
とその内部に封入される核燃料との間に金属障壁
を設ける試みがなされている。この金属障壁とし
ては、適度は純度のジルコニウムが用いられ、そ
れをジルコニウム合金よりなる被覆管の内部に内
張りした複合型被覆管が最も有望視されている。
この場合、ジルコニウム層障壁の厚さは複合型被
覆管の厚さの約5〜30%とされている。ジルコニ
ウムはジルコニウム合金に比べて、照射中でも軟
かさを維持するので、核燃料要素内の局部歪みを
減じ、応力腐食割れ又は液体金属脆化から被覆管
を保護するだけでなく、中性子捕獲ペナルテイ、
熱伝達ペナルテイ又は材料の非両立問題を惹起し
ない点においても優れている。
このような複合型被覆管は、通常第1図に示す
工程を経て製造される。即ち、ジルコニウムとジ
ルコニウム合金のブリケツトを各別に溶解し、そ
れぞれインゴツトを製造し、ジルコニウム合金の
ものを大径とし、ジルコニウムのものを小径とな
した中空ビレツトを製作し、次にジルコニウム合
金の中空ビレツト中にジルコニウムの中空ビレツ
トを挿入し、爆接又は拡散接合などによつて一体
化して複合ビレツトとする。次いで、この複合ビ
レツトを通常の熱間押出法により押出複合素管と
し、この押出複合素管の通状の製管加工を施して
所望寸法の複合型被覆管に仕上げるのである。こ
のようにして製造した複合型被覆管は、基材たる
ジルコニウム合金層の部分と金属障壁となるジル
コニウム層の部分とが相互の境界面において金属
結合されている。
このようにして得られた複合型被覆管を原子炉
の中枢部に用るについて最も重要なことは、障壁
となるジルコニウム層の厚さが所要の寸法範囲内
にあるように正確に製作されていることと、ジル
コニウム層と基材たるジルコニウム合金層とが相
互の境界面の全面にわたつて完全に金属結合され
ていなければならないということである。故に複
合型被覆管は、その各部についてジルコニウム層
の厚さを検査する必要にせまられる所以である。
ところが、ジルコニウム層とジルコニウム合金層
とが完全に金属結合されていることに加えて、両
者の材質が極めて近似しているため、ジルコニウ
ム層の厚さを非破壊的に正確に測定することは従
来不可能なものとされていた。例えば、ジルコニ
ウム98%を主成分とするASTM規格B353グレー
ドのR60802に適合する標準ジルカロイ―2
(Sn1.47%,Fe0.123%,Cr0.087%,Ni0.056%)
の基材層と、実質的純ジルコニウム99.9%
(Sn0.0021%,Fe0.034%,Cr0.014%,Ni0.001
%)の障壁層とからなる複合型被覆管の場合は、
熱伝導度、透磁率、音響インピーダンス等いずれ
の物理的性質においても酷似しているため、超音
波検査法、電磁気的検査法、放射線検査法等いず
れの検査法によつても障壁層の厚さを測定するこ
とは不可能であつた。
従来の水浸超音波検査装置で障壁層の厚さを測
定しようとする場合を第2図について述べると、
探触子6から超音波が発せられるとブラウン管8
には、まず送信エコーTが表われ、超音波が複合
型被覆管1の外表に達したときに外面エコーSが
表われるが、超音波が管の肉厚内に伝播されてジ
ルコニウム合金基材層2とジルコニウム障壁層4
の境界面3に達しても、両層間の音響インピーダ
ンスは変らないからそのまま素通りし、ブラウン
管8には何らのエコーも表われず、障壁層内面に
当つて反射された内面反射エコーB,B′が表わ
れるだけである。この表面エコーSと内面反射エ
コーB間の伝播時間によつて複合型被覆管1の全
肉厚を測定することは可能であるが、超音波が境
界面3を素通りする以上、障壁層4の厚さは到底
これを測定すべくもなかつた。なお同図において
5は水槽、7は超音波検査装置である。
上記の複合型被覆管は、機械的性質の良好な点
が注目されて沸湯水型や負荷追随型原子炉の操業
に使用可能な核燃料被覆管として世界的に研究開
発が進められてはいるが未だ実用化されるには至
つておらず、その原因は障壁層の品質保証に課題
があり、特に障壁層の肉厚寸法を正確に測定し得
なかつたことが実用化を遅らせている大きな原因
となつていた。
本発明は前記の問題を解決することを目的とす
るものであつて、実質的純ジルコニウム層とジル
コニウム合金層とが金属結合されてなる複合材を
再結晶温度以上の温度で熱処理することにより前
記純ジルコニウム層とジルコニウム合金層の境界
面で両層間に明確な粒度差のある結晶を生成せし
該熱処理後の複合材に対して周波数が10MHz域の
超音波(a)と周波数100〜500MHzの超音波(d)とをジ
ルコニウム合金層側から同時に又は相前後して入
射し、前記超音波(a)による反射エコーに基いて複
合材の全肉厚値を求め、前記超音波(b)による反射
エコーに基いてジルコニウム合金層の肉厚値を求
め、複合材の全肉厚値とジルコニウム合金層の肉
厚値との差により前記純ジルコニウム層の肉厚値
を検知することを要旨とするものである。ここに
複合材とは、純ジルコニウム層とジルコニウム合
金層とが金属結合されたものであれば、その形状
において、管材であると、板材であると、条材で
あるとを問わず、あるいは容器の如きものであつ
てもよい。
以下に、複合材を、核燃料が封入される複合型
被覆管を例にあげて本発明の実施例を説明する。
複合型被覆管の基材層となるジルコニウム合金
(ジルカロイ)と障壁層となる純純ジルコニウム
(純Zr)の化学組成は表1の如くである。
The present invention is based on pure zirconium (hereinafter referred to as zirconium) used to construct the core of a nuclear reactor.
The present invention relates to a method for measuring the wall thickness of a composite material made of a zirconium alloy and a zirconium alloy, particularly a composite material in which the inner surface of a tubular cladding material (hereinafter referred to as cladding tube) made of a zirconium alloy that encloses nuclear fuel is lined with a metal barrier of a zirconium layer. Nuclear fuel elements of power reactors currently designed, manufactured, or operated currently enclose nuclear fuel material inside a cladding tube that is corrosion-resistant, non-reactive, and has good thermal conductivity. Nuclear fuel assemblies are assembled by assembling such nuclear fuel elements in a lattice pattern at regular intervals, and by combining an appropriate number of these nuclear fuel assemblies, nuclear fission chain reaction assemblies and reactor cores capable of self-sustaining nuclear fission reactions are formed. The core is contained within a reactor vessel through which coolant passes. The main purpose of using a cladding tube to contain nuclear fuel in the core of such a nuclear reactor is, first, to prevent chemical reactions between the nuclear fuel and the coolant or between the nuclear fuel and the moderator; The purpose is to prevent radioactive fission products, which are partially gaseous, from escaping from the fuel into the coolant or moderator. The main cladding tubes commonly used are stainless steel and zirconium alloys. When manufacturing and operating nuclear fuel elements using certain metals or alloys as cladding tubes, various problems arise due to mechanical or chemical reactions that occur in these cladding tubes under certain conditions. It's on. Zirconium and its alloys are excellent nuclear fuel cladding under steady-state conditions. The reason for this is that zirconium and its alloys have a small neutron absorption cross section, and furthermore, at temperatures below about 400°C, zirconium and its alloys cannot be used in the presence of pure water or steam, commonly used as reactor coolants and moderators. This is because it has excellent strength, elongation, is extremely stable, and is non-reactive. However, it has become clear that the behavior of nuclear fuel elements is such that the interaction between the nuclear fuel, the cladding, and the fission products produced during the fission reaction causes the cladding to become brittle and eventually crack. It has been determined that this undesirable behavior is further exacerbated by local mechanical stresses due to differential thermal expansion between the fuel and the cladding. During the operation of a nuclear reactor, fission products are released from the nuclear fuel due to the fission reaction, and when they are present on the surface of the cladding tube and certain fission products such as iodine and cadmium are present,
Stress corrosion cracking occurs in cladding tubes due to the effects of local stress and strain. As a measure to prevent such troubles, attempts have been made to provide a metal barrier between the cladding tube and the nuclear fuel sealed therein. As this metal barrier, zirconium of moderate purity is used, and a composite cladding tube made of a zirconium alloy and lined with zirconium alloy is considered to be the most promising.
In this case, the thickness of the zirconium layer barrier is approximately 5 to 30% of the thickness of the composite cladding. Compared to zirconium alloys, zirconium remains soft during irradiation, reducing local strain within the nuclear fuel element and protecting the cladding from stress corrosion cracking or liquid metal embrittlement, as well as reducing neutron capture penalties.
It is also superior in that it does not cause heat transfer penalties or material incompatibility problems. Such a composite cladding tube is usually manufactured through the steps shown in FIG. That is, zirconium and zirconium alloy briquettes are melted separately to produce ingots, hollow billets of zirconium alloy with a large diameter and zirconium with a small diameter are produced, and then the zirconium alloy hollow billets are made into ingots. A hollow billet of zirconium is inserted inside and integrated by explosion welding or diffusion bonding to form a composite billet. Next, this composite billet is made into an extruded composite tube by a conventional hot extrusion method, and the extruded composite tube is processed into a continuous tube to form a composite cladding tube of desired size. In the composite cladding tube manufactured in this manner, the zirconium alloy layer portion serving as the base material and the zirconium layer portion serving as the metal barrier are metallically bonded at the mutual interface. The most important thing when using the composite cladding obtained in this way in the central part of a nuclear reactor is that the thickness of the zirconium layer that serves as a barrier is manufactured accurately so that it is within the required dimensional range. The zirconium layer and the zirconium alloy layer serving as the base material must be completely metallically bonded over the entire boundary surface between them. This is why it is necessary to inspect the thickness of the zirconium layer in each part of the composite cladding tube.
However, because the zirconium layer and zirconium alloy layer are completely metallically bonded and their materials are extremely similar, it has been difficult to accurately measure the thickness of the zirconium layer non-destructively. It was considered impossible. For example, standard Zircaloy-2, which complies with ASTM standard B353 grade R60802, whose main component is 98% zirconium.
(Sn1.47%, Fe0.123%, Cr0.087%, Ni0.056%)
base material layer and substantially pure zirconium 99.9%
(Sn0.0021%, Fe0.034%, Cr0.014%, Ni0.001
In the case of a composite cladding consisting of a barrier layer of
Since the physical properties such as thermal conductivity, magnetic permeability, and acoustic impedance are very similar, the thickness of the barrier layer cannot be determined by any inspection method such as ultrasonic inspection, electromagnetic inspection, or radiographic inspection. It was impossible to measure. Referring to Figure 2, the case where the thickness of a barrier layer is measured using a conventional water immersion ultrasonic inspection device is as follows.
When ultrasonic waves are emitted from the probe 6, the cathode ray tube 8
, a transmitted echo T appears first, and when the ultrasonic wave reaches the outer surface of the composite cladding tube 1, an outer surface echo S appears, but the ultrasonic wave is propagated within the thickness of the tube and the zirconium alloy base material Layer 2 and zirconium barrier layer 4
Even if it reaches the boundary surface 3 of the barrier layer, the acoustic impedance between the two layers does not change, so it passes through as it is, and no echo appears on the cathode ray tube 8, and the internal reflection echoes B and B' that hit the inner surface of the barrier layer and are reflected. only appears. Although it is possible to measure the total wall thickness of the composite cladding tube 1 based on the propagation time between the surface echo S and the internal reflection echo B, since the ultrasonic waves pass through the boundary surface 3, it is difficult to measure the thickness of the barrier layer 4. There was no way I could measure the thickness. In the figure, 5 is a water tank and 7 is an ultrasonic inspection device. The above-mentioned composite cladding tube has attracted attention for its good mechanical properties, and research and development is progressing worldwide as a nuclear fuel cladding tube that can be used in the operation of boiling water type and load-following type nuclear reactors. It has not yet been put into practical use, and the reason for this is that there are issues with quality assurance of the barrier layer, and in particular, it has not been possible to accurately measure the wall thickness of the barrier layer, which is a major reason for the delay in practical application. It was becoming. The present invention aims to solve the above-mentioned problems by heat-treating a composite material in which a substantially pure zirconium layer and a zirconium alloy layer are metallically bonded at a temperature higher than the recrystallization temperature. At the interface between the pure zirconium layer and the zirconium alloy layer, crystals with a clear grain size difference are generated between the two layers, and the composite material after heat treatment is subjected to ultrasonic waves (a) with a frequency in the 10 MHz range and with a frequency of 100 to 500 MHz. Ultrasonic waves (d) are applied from the zirconium alloy layer side at the same time or in succession, and the total thickness value of the composite material is determined based on the echoes reflected by the ultrasonic waves (a). The gist is to obtain the thickness value of the zirconium alloy layer based on the reflected echo, and to detect the thickness value of the pure zirconium layer based on the difference between the total thickness value of the composite material and the thickness value of the zirconium alloy layer. It is something. Here, a composite material is defined as a material in which a pure zirconium layer and a zirconium alloy layer are metallurgically bonded, regardless of its shape, whether it is a pipe, a plate, a strip, or a container. It may be something like. Embodiments of the present invention will be described below using a composite material as an example of a composite cladding tube in which nuclear fuel is sealed.
Table 1 shows the chemical compositions of the zirconium alloy (Zircaloy) that will be the base material layer of the composite cladding tube and the pure zirconium (pure Zr) that will be the barrier layer.
【表】
表1の化学組成になるジルカロイ層とジルコニ
ウム層を有する複合型被覆管は、前記第1図を参
照して説明した製管工程を経て製造され、基材た
るジルコニウム合金層とその内面側に内張りされ
た障壁たるジルコニウム層とは、相互の境界面に
おいて完全に金属結合されており、このような複
合型被覆管を真空焼鈍炉内に装入し、再結晶温度
以上の温度において0.5〜3Hrの適宜時間で熱処
理を施すと、ジルカロイ層とジルコニウム層との
間には結晶粒の成長度に明確な差が生じる。この
現象は、両層に含有される元素の挙動によるもの
であり、一般に合金元素の種類の多い程、又それ
ら元素の含有量が高いもの程細粒化する傾向にあ
るが、特に結晶粒の大きさに影響を及ぼすものは
Snである。そして両層の結晶粒度の差は、両層
間が完全に金属結合されているにもかかわらず、
相互の境界面において截然としており、その状態
は第3図の顕微鏡写真に示す如くである。熱処理
温度を種々変化せしめた場合のジルカロイ層とジ
ルコニウム層の結晶粒度は、第2表に示す如くで
あつた。但し、複合型被覆管の素管段階から、数
回の製管加工を施し、かつ各製管加工の間に焼鈍
工程を介在させて成品管に至るまでの総合加工度
は、断面減少率で86%であり、熱処理時間は2Hr
とした。又粒度表示はASTM規格によつた。[Table] A composite cladding tube having a zircaloy layer and a zirconium layer having the chemical composition shown in Table 1 is manufactured through the tube manufacturing process explained with reference to Fig. 1 above, and consists of a zirconium alloy layer as a base material and its inner surface. The zirconium layer, which is a barrier lined on the side, is completely metallically bonded at the mutual interface, and when such a composite cladding tube is placed in a vacuum annealing furnace, the zirconium layer is 0.5 at a temperature higher than the recrystallization temperature. When heat treatment is performed for an appropriate time of ~3 hours, a clear difference in the degree of grain growth occurs between the zircaloy layer and the zirconium layer. This phenomenon is due to the behavior of the elements contained in both layers, and generally speaking, the more types of alloying elements there are, or the higher the content of those elements, the finer the grains become. What affects the size
Sn. The difference in grain size between the two layers is due to the fact that the two layers are completely metallically bonded.
The mutual boundary surfaces are clearly defined, as shown in the micrograph of FIG. 3. The crystal grain sizes of the zircaloy layer and the zirconium layer were as shown in Table 2 when the heat treatment temperature was varied. However, the overall degree of processing from the raw pipe stage of a composite cladding tube to the finished pipe by performing several tube manufacturing processes and intervening an annealing process between each tube manufacturing process is determined by the area reduction rate. 86%, heat treatment time is 2Hr
And so. Particle size display was based on ASTM standards.
【表】
次に、超音波検査法による肉厚測定に関して
は、一般に金属組織の結晶粒度と超音波の散乱度
との間には密接な関係のあることが知られてい
る。即ち、結晶粒が大きくなればなる程超音波の
散乱度は大となり、従つて超音波は被検査材を透
過し難いものとなる。又超音波の散乱度は、超音
波自体の周波数とも密接な関係があり、周波数が
高くなればなる程散乱度も大となり、従つて、一
旦探触子から発射された超音波が再び探触子に戻
つてくる率も高くなることが知られている。この
ような一般的現象が複合型被覆管にはどのように
表われるかを実験した。この実験例では、前記表
2に示す供試材番号No.2のものについて、周波数
10MHz域の超音波を入射せしめたところ、ジルカ
ロイ層及び純ジルコニウム層にわたつて超音波は
素通りすることを確認した。従つて、この周波数
域の超音波を使用すすれば、複合型被覆管の全肉
厚を測定することが可能であることがわかつた。
ところが、純ジルコニウム層の肉厚を検知するた
めには、その外層部にあるジルカロイは通過して
もジルコニウム層は通過せずして相互の境界面で
反射し、再び探触子に戻つてくる周波数の超音波
を探求しなければならない。そのため複合型被覆
管の外面側、即ちジルコニウム層の側から、種々
周波数の異なる超高域の超音波を入射して、それ
らがジルカロイ層とジルコニウム層の境界面で反
射し、探触子に戻つてくる率を調べた。その結果
は第4図に示す如くであつた。即ち、周波数50M
Hzのものは殆んど境界面から反射して戻つてくる
ことはなかつたが、100MHzのものの反射率は40
%であり、200MHzのものは80%を超えており、
220MHzではほぼ100%に達することが認められ
る。探触子に戻つてくる超音波の率が40%以上あ
れば、その反射エコーによつてジルカロイ層の肉
厚を測定することが可能となるため、周波数は
100MHz以上の超音波を使用する。しかし、周波
数が高すぎるとS/N比が悪くなるので、検出可
能なS/N比(2以上)を得るためには、周波数
を500MHz以下に抑える必要がある。要するに、
測定に十分な反射エコーと検出に支障のないS/
N比を得るために、周波数を100〜500MHzの範囲
に設定してジルカロイ層の肉厚を測定する。前記
の如くして複合型被覆管の全肉厚と、そのうちの
ジルカロイ層の肉厚が検知できれば、両の肉厚の
差によりジルコニウム層の肉厚を検知し得ること
はいうまでもない。このことは、叙上の技術的趣
旨よりして、複合型被覆管に限らず、複合型板そ
の他の複合材にも通じ得ることは勿論である。
前記の肉厚測定方法の実施に使用する超音波肉
厚測定装置の概略を第5図に示す。同図において
探触子6、複合型被覆管1、基材層(ジルカロイ
層又はジルコニウム合金層)2、境界面3、障壁
層(ジルコニウム層又は純ジルコニウム層)4、
水槽5は第2図のものと同様である。11は周波
数10MHz域の超音波(a)を使用する超音波検査装置
であり、これにブラウン管12が接続されてい
る。一方13は周波数100〜500MHz範囲の超音波
(b)を使用する超音波検査装置であり、これにブラ
ウン管14が接続されている。そして15はブラ
ウン管12,14によつて得らた全肉厚値に相当
する信号と基材層の肉厚値に相当する信号を入力
して両者の差即ち障壁層の肉厚値を求める演算器
であり、よつて得られた信号値は表示器16に出
力されて障壁層4の肉厚値を表示することとな
る。超音波検査装置11,13から発射される
10MHz域と100〜500MHz域の超音波(a),(b)は、複
合型被覆管1の表面に対して垂直になるように
し、同一個所より管の肉厚方向へ入射される。こ
れは同時になされてもよく又は相前後してなされ
てもよい。超音波検査装置11,13にはそれぞ
れの周波数のみに対応し得るフイルタが装備され
ている。超音波(a)の反射波はブラウン管12に送
信エコーT、複合型被覆管1の外表面の反射に係
る外面エコーS、障壁層4の内面からの反射に係
る内面エコーBが表われる。そして、t0は複合型
被覆管1の全肉厚に相当する。超音波(b)の反射波
はブラウン管14に、ブラウン管12の場合と同
様に送信エコーT、外面エコーSが表われるが、
境界面3を通過することなく該境界面3からの反
射エコーFが表われる。そしてt1は基材層2の肉
厚に相当する。t0の信号とt1の信号は演算器15
に入力され(t0―t1)を演算して障壁層4の肉厚
値を得、これが表示器16に表示されるのであ
る。
以上詳述したように本発明の肉厚測定方法によ
れば、従来不可能とされていたジルコニウム合金
を基材層とし、その内面側に純ジルコニウムの障
壁層が金属結合された複合型被覆管の全肉厚は勿
論、基材層及び障壁層の肉厚をも測定することが
可能となり、原子炉中枢部に使用される材料の設
計に寄与すること大であり、応力腐食割れや液体
金属脆化に耐え得る複合被覆管の品質保証度を大
幅に向上せしめることができる。[Table] Next, regarding wall thickness measurement by ultrasonic testing, it is generally known that there is a close relationship between the crystal grain size of the metal structure and the degree of scattering of ultrasonic waves. That is, the larger the crystal grains, the greater the degree of scattering of ultrasonic waves, and therefore the more difficult it is for ultrasonic waves to pass through the material to be inspected. The degree of scattering of ultrasonic waves is also closely related to the frequency of the ultrasonic waves themselves; the higher the frequency, the greater the degree of scattering. It is known that the rate of children returning to their offspring is also high. We conducted an experiment to see how this general phenomenon appears in composite cladding tubes. In this experimental example, the frequency of sample material No. 2 shown in Table 2 was
When ultrasonic waves in the 10 MHz range were applied, it was confirmed that the ultrasonic waves passed through the Zircaloy layer and the pure zirconium layer. Therefore, it was found that by using ultrasonic waves in this frequency range, it is possible to measure the total wall thickness of a composite cladding tube.
However, in order to detect the thickness of a pure zirconium layer, even though the zircaloy in the outer layer passes through, it does not pass through the zirconium layer and is reflected at the mutual interface and returns to the probe. Must explore ultrasonic frequencies. Therefore, ultrahigh-frequency ultrasonic waves with various frequencies are incident on the outer surface of the composite cladding tube, that is, from the zirconium layer side, and they are reflected at the interface between the zircaloy layer and the zirconium layer and returned to the probe. I checked the rate of return. The results were as shown in FIG. i.e. frequency 50M
The Hz signal hardly reflected from the boundary surface and did not come back, but the 100 MHz signal had a reflectance of 40
%, and the one at 200MHz exceeds 80%,
It is recognized that it reaches almost 100% at 220MHz. If the rate of ultrasonic waves returning to the probe is 40% or more, it is possible to measure the thickness of the Zircaloy layer by the reflected echo, so the frequency is
Uses ultrasound of 100MHz or higher. However, if the frequency is too high, the S/N ratio deteriorates, so in order to obtain a detectable S/N ratio (2 or more), it is necessary to suppress the frequency to 500 MHz or less. in short,
Sufficient reflected echo for measurement and S/ that does not interfere with detection
To obtain the N ratio, the thickness of the Zircaloy layer is measured with the frequency set in the range of 100 to 500 MHz. It goes without saying that if the total thickness of the composite cladding tube and the thickness of the zircaloy layer among them can be detected as described above, the thickness of the zirconium layer can be detected from the difference between the two thicknesses. Of course, this is applicable not only to composite cladding tubes, but also to composite templates and other composite materials, in view of the technical purpose described above. FIG. 5 schematically shows an ultrasonic wall thickness measuring device used to carry out the above wall thickness measuring method. In the same figure, a probe 6, a composite cladding tube 1, a base material layer (zircaloy layer or zirconium alloy layer) 2, a boundary surface 3, a barrier layer (zirconium layer or pure zirconium layer) 4,
The water tank 5 is similar to that in FIG. Reference numeral 11 denotes an ultrasonic inspection device that uses ultrasonic waves (a) in the frequency range of 10 MHz, and a cathode ray tube 12 is connected to this. On the other hand, 13 is an ultrasonic wave with a frequency range of 100 to 500 MHz.
This is an ultrasonic inspection device using (b), to which a cathode ray tube 14 is connected. 15 is an operation for inputting a signal corresponding to the total thickness value obtained by the cathode ray tubes 12 and 14 and a signal corresponding to the thickness value of the base material layer, and calculating the difference between the two, that is, the thickness value of the barrier layer. The signal value thus obtained is output to the display 16 to display the thickness value of the barrier layer 4. Emitted from ultrasonic inspection devices 11 and 13
The ultrasonic waves (a) and (b) in the 10 MHz range and 100 to 500 MHz range are made perpendicular to the surface of the composite cladding tube 1, and are incident in the thickness direction of the tube from the same location. This may be done simultaneously or one after the other. The ultrasonic inspection apparatuses 11 and 13 are equipped with filters that can handle only the respective frequencies. The reflected waves of the ultrasonic waves (a) appear on the cathode ray tube 12 as a transmitted echo T, an external echo S caused by reflection from the outer surface of the composite cladding tube 1, and an inner echo B caused by reflection from the inner surface of the barrier layer 4. Further, t 0 corresponds to the total wall thickness of the composite cladding tube 1 . The reflected wave of the ultrasonic wave (b) appears on the cathode ray tube 14 as a transmitted echo T and an external echo S as in the case of the cathode ray tube 12.
A reflected echo F from the boundary surface 3 appears without passing through the boundary surface 3. And t1 corresponds to the thickness of the base material layer 2. The signal at t 0 and the signal at t 1 are sent to the arithmetic unit 15.
The thickness value of the barrier layer 4 is obtained by calculating (t 0 −t 1 ), which is displayed on the display 16. As detailed above, according to the wall thickness measurement method of the present invention, a composite cladding tube with a base layer made of zirconium alloy and a barrier layer of pure zirconium metallically bonded to the inner surface of the base layer made of zirconium alloy, which was previously considered impossible. It is now possible to measure not only the total wall thickness of the reactor, but also the wall thickness of the base material layer and barrier layer, which will greatly contribute to the design of materials used in the core of the reactor, and will help prevent stress corrosion cracking and liquid metal The quality assurance level of composite cladding tubes that can withstand embrittlement can be greatly improved.
第1図は被測定材である複合型被覆管の製造工
程を示すブロツク図、第2図は従来の水浸超音波
検査法による管の肉厚測定状況を示す図、第3図
は熱処理によつて再結晶しジルコニウム合金層と
ジルコニウム層の結晶粒度差が明確に現出されて
いる顕微鏡写真、第4図は使用する超音波周波数
と反射エコーの関係を表わす図、第5図は本発明
の肉厚測定方法の実施に使用される超音波検査装
置の概略を示す図である。
1……複合型被覆管、2……基材層、3……境
界面、4……障壁層、5……水槽、6……探触
子、7……超音波検査装置、8……ブラウン管、
11……10MHz域超音波検査装置、12……ブラ
ウン管、13……100〜500MHz域超音波検査装
置、14……ブラウン管、15……演算器、16
……表示器。
Figure 1 is a block diagram showing the manufacturing process of the composite cladding tube, which is the material to be measured. Figure 2 is a diagram showing how the wall thickness of the tube is measured using conventional water immersion ultrasonic testing. A micrograph clearly showing the difference in crystal grain size between the recrystallized zirconium alloy layer and the zirconium layer, Figure 4 is a diagram showing the relationship between the ultrasonic frequency used and the reflected echo, and Figure 5 is a diagram showing the present invention. FIG. 2 is a diagram schematically showing an ultrasonic inspection device used to implement the wall thickness measurement method of FIG. DESCRIPTION OF SYMBOLS 1... Composite cladding tube, 2... Base material layer, 3... Boundary surface, 4... Barrier layer, 5... Water tank, 6... Probe, 7... Ultrasonic inspection device, 8... cathode ray tube,
11... 10MHz range ultrasonic inspection device, 12... Braun tube, 13... 100-500MHz range ultrasonic inspection device, 14... Braun tube, 15... Arithmetic unit, 16
……display.
Claims (1)
層とが金属結合されてなる複合材を再結晶温度以
上の温度で熱処理することにより、前記純ジルコ
ニウム層とジルコニウム合金層の相互間に結晶粒
度の差を生ぜしめ、該熱処理後の複合材に対して
周波数10MHz域の超音波(a)と周波数100〜500MHz
の超音波(b)とを、ジルコニウム合金層側から同時
に又は相前後して入射し、前記超音波(a)による反
射エコーにもとづいて複合材の全肉厚値を求め、
前記超音波(b)による反射エコーにもとづいてジル
コニウム合金層の肉厚値を求め、複合材の全肉厚
値とジルコニウム合金層の肉厚値との差により純
ジルコニウム層の肉厚値を検知することを特徴と
するジルコニウム複合材の肉厚測定方法。1 By heat-treating a composite material in which a substantially pure zirconium layer and a zirconium alloy layer are metallically bonded at a temperature higher than the recrystallization temperature, a difference in crystal grain size is created between the pure zirconium layer and the zirconium alloy layer. After tightening, the composite material after the heat treatment is subjected to ultrasonic waves (a) in the frequency range of 10MHz and frequencies of 100 to 500MHz.
The ultrasonic waves (b) are incident simultaneously or one after another from the zirconium alloy layer side, and the total thickness value of the composite material is determined based on the echoes reflected by the ultrasonic waves (a),
The wall thickness value of the zirconium alloy layer is determined based on the echo reflected by the ultrasonic wave (b), and the wall thickness value of the pure zirconium layer is detected from the difference between the total wall thickness value of the composite material and the wall thickness value of the zirconium alloy layer. A method for measuring the wall thickness of a zirconium composite material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4109881A JPS57154009A (en) | 1981-03-19 | 1981-03-19 | Measurement of thickness of composite object composed of zirconium layer and zirconium alloy layer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4109881A JPS57154009A (en) | 1981-03-19 | 1981-03-19 | Measurement of thickness of composite object composed of zirconium layer and zirconium alloy layer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS57154009A JPS57154009A (en) | 1982-09-22 |
| JPS6313125B2 true JPS6313125B2 (en) | 1988-03-24 |
Family
ID=12598998
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4109881A Granted JPS57154009A (en) | 1981-03-19 | 1981-03-19 | Measurement of thickness of composite object composed of zirconium layer and zirconium alloy layer |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS57154009A (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2617914B2 (en) * | 1986-03-04 | 1997-06-11 | 神鋼特殊鋼管株式会社 | Method for measuring liner thickness of double pipe and biaxial follower for ultrasonic probe |
| US4669310A (en) * | 1986-03-26 | 1987-06-02 | The Babcock & Wilcox Company | High frequency ultrasonic technique for measuring oxide scale on the inner surface of boiler tubes |
| JPH0678905B2 (en) * | 1987-06-05 | 1994-10-05 | 住友金属工業株式会社 | Clad material thickness measuring device |
| FR2629586B1 (en) * | 1988-03-30 | 1992-01-03 | Cezus Co Europ Zirconium | METHOD FOR ULTRASONIC CONTROL OF THE PLACEMENT THICKNESS OF A METAL TUBE, CORRESPONDING DEVICE AND APPLICATION TO TUBES OF ZR PLATE ALLOY |
| US5661241A (en) * | 1995-09-11 | 1997-08-26 | The Babcock & Wilcox Company | Ultrasonic technique for measuring the thickness of cladding on the inside surface of vessels from the outside diameter surface |
| DE10115328A1 (en) * | 2001-03-28 | 2002-10-10 | Framatome Anp Gmbh | Method for ultrasonic measurement of partial layer thicknesses of thin-walled pipes |
| JP4545351B2 (en) * | 2001-06-18 | 2010-09-15 | ブリヂストンスポーツ株式会社 | Golf ball cover thickness measuring method and apparatus |
-
1981
- 1981-03-19 JP JP4109881A patent/JPS57154009A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS57154009A (en) | 1982-09-22 |
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