JPH0116383B2 - - Google Patents
Info
- Publication number
- JPH0116383B2 JPH0116383B2 JP58023522A JP2352283A JPH0116383B2 JP H0116383 B2 JPH0116383 B2 JP H0116383B2 JP 58023522 A JP58023522 A JP 58023522A JP 2352283 A JP2352283 A JP 2352283A JP H0116383 B2 JPH0116383 B2 JP H0116383B2
- Authority
- JP
- Japan
- Prior art keywords
- flaw detection
- square steel
- angle
- steel piece
- refraction angle
- 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
- 238000001514 detection method Methods 0.000 claims description 51
- 229910000831 Steel Inorganic materials 0.000 claims description 39
- 239000010959 steel Substances 0.000 claims description 39
- 238000000034 method Methods 0.000 description 13
- 230000007547 defect Effects 0.000 description 9
- 239000002344 surface layer Substances 0.000 description 8
- 230000001788 irregular Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000007665 sagging Methods 0.000 description 4
- 239000000523 sample Substances 0.000 description 4
- 238000002592 echocardiography Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/04—Analysing solids
- G01N29/06—Visualisation of the interior, e.g. acoustic microscopy
- G01N29/0609—Display arrangements, e.g. colour displays
- G01N29/0618—Display arrangements, e.g. colour displays synchronised with scanning, e.g. in real-time
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/02—Indexing codes associated with the analysed material
- G01N2291/028—Material parameters
- G01N2291/02854—Length, thickness
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/04—Wave modes and trajectories
- G01N2291/044—Internal reflections (echoes), e.g. on walls or defects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/04—Wave modes and trajectories
- G01N2291/056—Angular incidence, angular propagation
Landscapes
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)
Description
【発明の詳細な説明】
本発明は角鋼片の超音波斜角探傷法に関し、所
望の探傷領域を精度よく設定できると共に、欠陥
位置推定精度を向上し得るようにしたものであ
る。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an ultrasonic angle flaw detection method for square steel pieces, and is capable of setting a desired flaw detection area with high accuracy and improving the accuracy of defect position estimation.
斜角探傷により角鋼片の内部或いは表面層を探
傷し、検出した欠陥の位置を推定する必要がある
場合には、探触子と角鋼片との位置関係、超音波
ビームの伝播方向(屈折角)、角鋼片の入射面か
らの反射エコーと欠陥エコーとの検出時間差より
求めた路程から演算によつて求められる。しかし
ながら実際の角鋼片には表面凹凸やたおれ等の形
状不整があるため、欠陥位置推定精度が劣化す
る。例えば第1図に示すように超音波ビームSを
入射する角鋼片1の表面に凹凸があれば、超音波
ビームSの入射位置により設定上の入射角と実際
上の入射角βは夫々異なり、また第2図a,bに
示すように同一位置から入射する場合でも、角鋼
片1によつてその位置での面形状が異なるため
に、設定上の入射角と実際上の入射角βは異な
る。その結果屈折角θも変化し、計算上の角鋼片
1中での超音波ビームSの伝播方向と違つてく
る。また第3図に示すように角鋼片1にたおれの
ある場合(標準の角鋼片1aに対して実際の角鋼
片1b)は、例えば角鋼片1の超音波入射面に隣
接する側面下半部分の探傷領域aを走査範囲bで
セクター走査にて探傷しているつもりが、同図に
示す如く角鋼片1bの側面中央部或いは角鋼片1
bの底面及び側面を探傷している場合があり、欠
陥位置推定以前の問題も生じうる。同様のことは
超音波入射面の形状不整による屈折角θの変化に
よつても起こる。従つて、角鋼片1の斜角探傷す
る場合所望の探傷域に超音波ビームSを導くこと
が困難となり、さらにはその検出欠陥位置を精度
よく推定することができなかつた。 When it is necessary to detect the interior or surface layer of a square steel piece using angle angle flaw detection and estimate the position of the detected defect, the positional relationship between the probe and the square steel piece, the propagation direction of the ultrasonic beam (refraction angle) ) is determined by calculation from the path length determined from the detection time difference between the reflected echo from the incident surface of the square steel piece and the defect echo. However, since actual square steel pieces have irregularities such as surface irregularities and sagging, the accuracy of estimating the defect position deteriorates. For example, as shown in FIG. 1, if the surface of a square steel piece 1 on which the ultrasonic beam S is incident is uneven, the set incident angle and the actual incident angle β will differ depending on the incident position of the ultrasonic beam S. Furthermore, even when the incident light is from the same position as shown in Figure 2 a and b, the set angle of incidence and the actual angle of incidence β differ because the surface shape at that position differs depending on the square steel piece 1. . As a result, the refraction angle θ also changes and becomes different from the calculated propagation direction of the ultrasonic beam S in the square steel piece 1. Furthermore, as shown in Fig. 3, if the square steel piece 1 has sagging (the actual square steel piece 1b is different from the standard square steel piece 1a), for example, the lower half of the side surface of the square steel piece 1 adjacent to the ultrasonic incident surface may be bent. I intended to perform flaw detection in the flaw detection area a by sector scanning in the scanning range b, but as shown in the figure, the center part of the side surface of the square steel piece 1b or the square steel piece 1
In some cases, the bottom and side surfaces of part b are being inspected, and problems may occur before the defect position can be estimated. The same thing occurs when the refraction angle θ changes due to the irregular shape of the ultrasonic wave incident surface. Therefore, when performing oblique flaw detection on the square steel piece 1, it is difficult to guide the ultrasonic beam S to the desired flaw detection area, and furthermore, it is not possible to accurately estimate the position of the detected flaw.
また、探傷目的即ち表面層探傷であるか内部探
傷であるかによつて、探傷ゲートをかける範囲が
変わるのであるが、従来の内部探傷法では探傷領
域aのみの探傷データを得るためのゲートのかけ
方として、第4図に示すように角鋼片1の入射表
面からの反射エコーS1の立ち上がりから該反射エ
コーS1のもれ込みの影響の少なくなるところにゲ
ート起点cを設定し、角鋼片1の幅Bを基準に底
面からの反射エコーB1の影響の少ないところま
でをゲート範囲として予め設定する固定ゲート方
式と、第5図に示すように探触子2により底面か
らの反射エコーB1を常時検知し(B1エコーのト
ラツキング)、その反射エコーB1から一定寸法l
だけ手前となるようにゲート終点dを制御する変
動ゲート方式とが用いられている。後述の方式を
用いることにより、角鋼片1の形状不整のいかん
に係わらず底面側の表面層の不感帯域(表面から
の深さ)を一定に保つことができる。ところが、
角鋼片1の内部探傷において表面不感帯を少なく
するため或いは表面層探傷するために、角鋼片1
を斜角探傷する場合には、底面からの反射エコー
B1又はこれに相当する側面からの反射エコーが
ほとんどないため、垂直探傷時の底面からの反射
エコーB1のトラツキングのような変動ゲート方
式は使えない。この斜角探傷において、固定ゲー
ト方式にすることは、前述の角鋼片1の形状不整
による超音波伝播方向の不確定性のため、垂直探
傷の場合以上に問題が多い。例えば第6図に示す
ようにたおれのある角鋼片1bに対し、たおれの
ない標準の角鋼片1aと同様に内部探傷用のゲー
トをかけていると、角鋼片1bを内部と共に表面
も探傷してしまい、表面欠陥Fをその欠陥エコー
F1により内部欠陥として誤検出する惧れがある。 Furthermore, the range in which a flaw detection gate is applied changes depending on the purpose of flaw detection, that is, surface layer flaw detection or internal flaw detection.In the conventional internal flaw detection method, the gate is applied to obtain flaw detection data only in the flaw detection area a. As shown in Fig. 4, the gate starting point c is set at a point where the reflected echo S1 from the incident surface of the square steel piece 1 rises and the influence of the leakage of the reflected echo S1 is reduced. The fixed gate method uses the width B of piece 1 as a reference and sets the gate range in advance to a point where the influence of the reflected echo B 1 from the bottom surface is small, and the fixed gate method uses the probe 2 to detect the reflected echo from the bottom surface as shown in Figure 5. B 1 is constantly detected (B 1 echo tracking), and a certain dimension l is detected from the reflected echo B 1 .
A variable gate method is used in which the gate end point d is controlled so that the gate end point d is positioned as close as possible. By using the method described below, the dead zone (depth from the surface) of the surface layer on the bottom side can be kept constant regardless of the irregular shape of the square steel piece 1. However,
In order to reduce the surface dead zone in internal flaw detection of the square steel piece 1 or to perform surface layer flaw detection, the square steel piece 1 is
When performing oblique inspection, the reflected echo from the bottom surface
Since there are almost no B 1 or equivalent echoes reflected from the side, a variable gate method such as tracking the B 1 reflected echo from the bottom surface during vertical flaw detection cannot be used. In this angle flaw detection, using the fixed gate method has more problems than in the case of vertical flaw detection because of the uncertainty in the ultrasonic propagation direction due to the aforementioned irregular shape of the square steel piece 1. For example, as shown in Fig. 6, if a square steel slab 1b with sagging is covered with a gate for internal flaw detection in the same way as a standard square steel slab 1a without sagging, the surface of the square steel slab 1b will be inspected as well as the inside. Then, the surface defect F is expressed as its defect echo.
There is a risk of false detection as an internal defect due to F1 .
本発明は上記問題点を解消したものである。 The present invention solves the above problems.
まず、本発明の概要を説明すると、角鋼片の内
部または表面層を超音波斜角探傷法によつて探傷
するとき、まず超音波入射面に隣接する側面下部
のコーナ付近を斜角探傷する。そしてコーナ部か
らの反射エコーが最大となるときの超音波ビーム
走査位置を検知し、その走査位置を基準にして所
望の探傷領域が探傷できるように超音波ビーム走
査範囲および探傷ゲート範囲を補正し、その後実
際の探傷を行なうのである。 First, an overview of the present invention will be described. When inspecting the interior or surface layer of a square steel piece by the ultrasonic angle flaw detection method, first, the vicinity of the lower corner of the side surface adjacent to the ultrasonic incidence surface is subjected to the angle angle flaw detection. Then, the ultrasonic beam scanning position where the reflected echo from the corner becomes the maximum is detected, and the ultrasonic beam scanning range and flaw detection gate range are corrected based on that scanning position so that the desired flaw detection area can be detected. Then, the actual flaw detection is carried out.
以下、電子セクター+リニア走査で角鋼片の超
音波入射面に隣接する側面下半部分の表面層を探
傷するときの方法を具体的に説明する。 Hereinafter, a method for detecting flaws in the surface layer of the lower half of the side surface adjacent to the ultrasonic incident surface of a square steel piece using electronic sector + linear scanning will be specifically described.
第7図に示すように超音波ビームSの入射点O
を角鋼片1の入射面中央とすると、コーナ部から
の反射エコーが最大となるのは、超音波ビームS
が下部コーナの曲率中心Aを通るときであり、そ
のときの標準状態(角鋼片1aの場合)における
屈折角θcは計算上次式で求まる。 As shown in Fig. 7, the incident point O of the ultrasonic beam S
Assuming that the center of the incident surface of the square steel piece 1 is the center of the incident surface of the square steel piece 1, the reflected echo from the corner part becomes the maximum when the ultrasonic beam S
passes through the center of curvature A of the lower corner, and the refraction angle θc in the standard state (in the case of the square steel piece 1a) at that time is calculated by the following formula.
θc=arc tanB−2R/2(B−R)
B:角鋼片の幅
R:コーナの曲率半径
角鋼片1に形状不整がある場合(角鋼片1bの
場合)には、コーナ部からの反射エコーが最大と
なる屈折角θpは変動する。例えば幅Bが155mm、
曲率半径Rが18mmの角鋼片1で、許容できるたお
れ角αが±3゜とすると、標準状態で、θp=θc=
23.5゜に対して屈折角θpは20.9゜〜25.9゜の範囲の値
をとる。よつてこの場合は屈折角θが18゜〜28゜程
度の走査範囲fでまずセクター+リニア走査する
ことにより、コーナエコーがピークになる屈折角
θpを検知できる。 θc = arc tanB-2R/2 (B-R) B: Width of the square steel slab R: Radius of curvature of the corner If the square steel slab 1 has an irregular shape (in the case of the square steel slab 1b), the reflected echo from the corner part The refraction angle θp at which θp becomes maximum varies. For example, width B is 155mm,
If the square steel piece 1 has a radius of curvature R of 18 mm and the allowable folding angle α is ±3°, then in the standard state, θp = θc =
For 23.5°, the refraction angle θp takes a value in the range of 20.9° to 25.9°. Therefore, in this case, the refraction angle θp at which the corner echo peaks can be detected by first performing sector+linear scanning in the scanning range f in which the refraction angle θ is about 18° to 28°.
このコーナピーク検出のためのセクター+リニ
ア走査は連続的に微小角変化させていけば正確に
コーナエコーが最大となる屈折角θpを求めるこ
とができるが、アレイ型探触子の分割幅の制約、
超音波ビーム偏向のための制御等の問題を加味
し、経済的には0.5゜ピツチ程度で探傷し、その内
で最大エコー高さとなるときの屈折角θを近似的
に反射エコーが最大となる屈折角θpとみなす。
或いは精度を上げるため各屈折角θとエコー高さ
の関係を放物線近似し、その放物線のピークとな
るときの屈折角θを最大となる屈折角θpとして
もよい。 Sector + linear scanning for detecting corner peaks can accurately determine the refraction angle θp at which the corner echo is maximized by continuously changing the small angle, but there are restrictions on the division width of the array type probe. ,
Taking into account issues such as control for ultrasonic beam deflection, it is economically viable to perform flaw detection at a pitch of about 0.5°, and within that range, the refraction angle θ at which the maximum echo height is reached is approximately determined to maximize the reflected echo. It is regarded as the refraction angle θp.
Alternatively, in order to improve accuracy, the relationship between each refraction angle θ and the echo height may be approximated to a parabola, and the refraction angle θ at the peak of the parabola may be set as the maximum refraction angle θp.
このようにしてコーナエコーが最大となる位置
を検知すれば、次はこの屈折角θpを基準に探傷
領域aである超音波入射面に隣接する側面の下半
部分の表面層を探傷するため屈折角θiを補正す
る。すなわち形状不整のない標準の角鋼片1aか
ら計算で求めた屈折角θcと実測の屈折角θpとの
差Δθ=θp−θc分を、探傷領域aを探傷するため
予め決めてあつた屈折角θiに加える。例えば計算
上θc=23.5゜から4゜ピツチで8回のセクター+リニ
ア走査(θ1=23.5゜、θ2=27.5゜、θ3=31.5゜、…
θ8=
51.5゜)する予定のとき、θp=25゜なる値を得たと
すれば、走査予定の屈折角θ1〜θ8の各値にΔθ=
15゜を加え、走査する屈折角θi′を、θ1′=25゜、θ
2′=
29.0゜、θ3′=33゜、…θ8′=53゜とする。つまり電
子走
査の場合、屈折角θi′に合わせアレイ型探触子の
各エレメントの遅延時間を制御する必要があり、
まず屈折角θが18゜〜28゜となる走査範囲fを0.5゜
ピツチでセクター+リニア走査し、計算機によつ
て屈折角θとエコー高さの関係を放物線近似する
ことによつてコーナ位置を示す屈折角θpを算出
したあと、予め決めた屈折角θiに差Δθを加え、
その補正した屈折角θi′で探傷できるように各エ
レメントの遅延時間を制御すればよい。 Once the position where the corner echo is maximum is detected in this way, the next step is to use the refraction angle θp as a reference to detect flaws in the surface layer of the lower half of the side surface adjacent to the ultrasonic incident surface, which is the flaw detection area a. Correct the angle θi. In other words, the difference Δθ = θp - θc between the refraction angle θc calculated from a standard square steel piece 1a with no irregular shape and the actually measured refraction angle θp is determined as the refraction angle θi predetermined for testing the flaw detection area a. Add to. For example, calculated from θc = 23.5°, 8 sectors + linear scan at 4° pitch (θ 1 = 23.5°, θ 2 = 27.5°, θ 3 = 31.5°,...
θ 8 =
51.5°), and if we obtain a value of θp = 25 °, then Δθ =
15°, the scanning refraction angle θi′ is θ 1 ′=25°, θ
2 ′=
29.0°, θ 3 ′=33°, ... θ 8 ′=53°. In other words, in the case of electronic scanning, it is necessary to control the delay time of each element of the array type probe according to the refraction angle θi'.
First, the scanning range f where the refraction angle θ is 18° to 28° is sector + linear scanned at a pitch of 0.5°, and the corner position is determined by approximating the relationship between the refraction angle θ and the echo height to a parabola using a computer. After calculating the refraction angle θp, add the difference Δθ to the predetermined refraction angle θi,
The delay time of each element may be controlled so that flaw detection can be performed using the corrected refraction angle θi'.
次に探傷ゲート範囲の補正の方法であるが、コ
ーナエコー最大となる屈折角θpを算出したあと
は、θ1′=θpからセクター+リニア走査する。こ
のθ1′=θpは前述のようにコーナエコーが最大と
なるときであり、垂直探傷時における底面から反
射エコーB1のトラツキング(第5図参照)と同
手法によつてコーナエコーの手前でゲート終点d
となるようにする。コーナ部以外の側面の探傷領
域aのゲート範囲の求め方を以下に示す。 Next, as a method for correcting the flaw detection gate range, after calculating the refraction angle θp at which the corner echo is maximum, sector+linear scanning is performed from θ 1 ′=θp. This θ 1 ′ = θp is the time when the corner echo is at its maximum as described above, and by tracking the echo B 1 reflected from the bottom surface during vertical flaw detection (see Figure 5), the same method can be used to track the echo B 1 in front of the corner echo. Gate end point d
Make it so that The method for determining the gate range of the flaw detection area a on the side surface other than the corner portion is shown below.
第8図に示すように、屈折角θpが算出されれ
ば角鋼片1bのたおれ角αは近似的に次式で表わ
される。 As shown in FIG. 8, once the refraction angle θp is calculated, the folding angle α of the square steel piece 1b can be approximately expressed by the following equation.
tanα=tanθp−tanθc
屈折角θi′=θi+Δθのとき、入射点Oから側表
面までの路程Xi′=は
X′i=B/2sinθi′+ω/sinθi′
ω≒B/2tanθi(tanθp−tanθc)
Xi′≒B/2sinθi′(tanθp−tanθc/tanθi+1
)
ω=点Dから角鋼片1aまでの寸法(第8図参
照)
ここで予め計算で求められる屈折角θiのときの
入射点Oから側表面までの路程Xi=は、
Xi=B/2sinθi
故に路程変化ΔXiは、ΔXi=Xi′−Xiで表わさ
れる。従つてこの路程変化ΔXiを計算機で算出
し、各屈折角θiでのゲート終点dを決定する。ゲ
ート起点cについてはゲート終点dより探傷領域
aを差し引きすることにより求められる。 tanα=tanθp−tanθc When the refraction angle θi′=θi+Δθ, the distance Xi′= from the point of incidence O to the side surface is X′i=B/2sinθi′+ω/sinθi′ ω≒B/2tanθi(tanθp−tanθc) Xi ′≒B/2sinθi′(tanθp−tanθc/tanθi+1
) ω = Dimension from point D to square steel piece 1a (see Figure 8) Here, the distance Xi = from the incident point O to the side surface when the refraction angle θi, which is calculated in advance, is Xi = B/2sinθi Therefore, The path change ΔXi is expressed as ΔXi=Xi′−Xi. Therefore, this path change ΔXi is calculated by a computer, and the gate end point d at each refraction angle θi is determined. The gate starting point c is found by subtracting the flaw detection area a from the gate ending point d.
なお、前記実施例では角鋼片1の表面層を探傷
域とする場合について説明したが、内部探傷の場
合でもまた底面側を探傷領域とする場合でも同様
にコーナ位置を基準にして走査範囲およびゲート
範囲を補正することができる。走査方式について
も電子セクター+リニア走査に限定されるもので
なく、一般的なセクター走査、リニア走査におい
ても適用可能である。 In the above embodiment, the case where the surface layer of the square steel slab 1 is used as the flaw detection area was explained, but even in the case of internal flaw detection or when the bottom surface side is used as the flaw detection area, the scanning range and gate are similarly determined based on the corner position. The range can be corrected. The scanning method is not limited to electronic sector + linear scanning, and general sector scanning and linear scanning are also applicable.
以上のように本発明によれば、コーナ近傍を斜
角探傷することによりコーナ位置を検知し、その
コーナ位置を基準にして超音波ビームの走査範囲
及び探傷ゲート範囲を補正し、斜角探傷するの
で、所望の探傷領域を精度よく確実に探傷でき、
しかも欠陥位置の推定が必要な場合は、その位置
検出精度も著しく向上できる。 As described above, according to the present invention, the corner position is detected by performing oblique flaw detection near the corner, and the scanning range of the ultrasonic beam and the flaw detection gate range are corrected based on the corner position, and the flaw detection is performed at an oblique angle. Therefore, the desired flaw detection area can be detected accurately and reliably.
Moreover, when the defect position needs to be estimated, the position detection accuracy can be significantly improved.
第1図乃至第3図は従来の問題点説明用の図、
第4図及び第5図は夫々従来の探傷方法を示す
図、第6図は同探傷方法の問題点説明用の図、第
7図は本発明のコーナ位置の検知方法及び走査範
囲の補正方法を示す図、第8図は同探傷ゲート範
囲の補正方法を示す図である。
1……角鋼片、S……超音波。
Figures 1 to 3 are diagrams for explaining conventional problems;
Figures 4 and 5 are diagrams showing the conventional flaw detection method, Figure 6 is a diagram for explaining problems with the same flaw detection method, and Figure 7 is the corner position detection method and scanning range correction method of the present invention. FIG. 8 is a diagram showing a method of correcting the flaw detection gate range. 1...Square steel piece, S...Ultrasonic wave.
Claims (1)
する側面下部のコーナ近傍を斜角探傷することに
よつてコーナ位置を検知し、そのコーナ位置を基
準にして超音波ビームの走査範囲及び探傷ゲート
範囲を補正し、斜角探傷することを特徴とする角
鋼片の超音波斜角探傷法。1 Using ultrasonic waves, the corner position is detected by performing oblique angle flaw detection near the corner of the lower side of the square steel piece adjacent to the ultrasonic incidence surface, and the scanning range of the ultrasonic beam is determined based on the corner position. An ultrasonic angle angle flaw detection method for square steel pieces, which is characterized by correcting the flaw detection gate range and performing oblique angle flaw detection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58023522A JPS59148860A (en) | 1983-02-14 | 1983-02-14 | Ultrasonic oblique flaw detecting method of square steel piece |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58023522A JPS59148860A (en) | 1983-02-14 | 1983-02-14 | Ultrasonic oblique flaw detecting method of square steel piece |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59148860A JPS59148860A (en) | 1984-08-25 |
| JPH0116383B2 true JPH0116383B2 (en) | 1989-03-24 |
Family
ID=12112775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58023522A Granted JPS59148860A (en) | 1983-02-14 | 1983-02-14 | Ultrasonic oblique flaw detecting method of square steel piece |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59148860A (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4523579B2 (en) * | 2006-12-15 | 2010-08-11 | 株式会社神戸製鋼所 | Manufacturing method of wire for cold forging |
| CN105223270A (en) * | 2014-06-26 | 2016-01-06 | 上海金艺检测技术有限公司 | Eliminate the detection method of square steel Inner Defect Testing system fillet scanning blind area |
-
1983
- 1983-02-14 JP JP58023522A patent/JPS59148860A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59148860A (en) | 1984-08-25 |
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