JPH1062093A - Eddy-current inspection probe - Google Patents

Eddy-current inspection probe

Info

Publication number
JPH1062093A
JPH1062093A JP8220129A JP22012996A JPH1062093A JP H1062093 A JPH1062093 A JP H1062093A JP 8220129 A JP8220129 A JP 8220129A JP 22012996 A JP22012996 A JP 22012996A JP H1062093 A JPH1062093 A JP H1062093A
Authority
JP
Japan
Prior art keywords
probe
elastic
inspection
eddy current
tube
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
Application number
JP8220129A
Other languages
Japanese (ja)
Other versions
JP3254138B2 (en
Inventor
Ei Tsuzuki
鋭 都築
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP22012996A priority Critical patent/JP3254138B2/en
Publication of JPH1062093A publication Critical patent/JPH1062093A/en
Application granted granted Critical
Publication of JP3254138B2 publication Critical patent/JP3254138B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PROBLEM TO BE SOLVED: To apply rotation to a part to be inspected without generating unevenness in rotation and perform a proper inspection by forming an elastic connecting part with a plurality of aligning members which are longitudinally arranged and rotatably fitted on the outer surface of an elastic hollow pipe and successively connecting the adjacent aligning members together by a plurality of universal joints. SOLUTION: The main body casing 61 of a probe body part 60 is provided with a motor 63. A slip ring 67 is attached to the output shaft of the motor 63 so that a wire 54 is connected thereto. The lead wire 54 is collected to a lead wire 65. An elastic connecting part 70 connected to the output shaft of the motor 63 and transmitting its torque to a probe head part 50 is formed with a plurality of aligning members 71 which are longitudinally arranged and rotatably fitted on the outer surface of an elastic hollow pipe. Further, the respectively adjacent aligning members 71 are successively connected together by a plurality of gimbal mechanism joints 73. Thus, rotation is transmitted to a part to be inspected without generating unevenness in rotation and a proper inspection can be performed.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、渦流探傷検査を行
う検査装置に関し、特に細い曲り管の渦流探傷検査に使
用される検査プローブに関する。
The present invention relates to an inspection apparatus for performing an eddy current inspection, and more particularly to an inspection probe used for an eddy current inspection of a thin curved pipe.

【0002】[0002]

【従来の技術】管形熱交換器では、細い管が伝熱管とし
て使用されているが、その伝熱管の損傷、欠陥等を非破
壊的に検査するため各種の探傷装置が使用されている。
そのうち曲り部のある伝熱管には図4に示すような渦流
検査プローブが使用される。この検査プローブ10は、
先端の検査部11,基端側の回転駆動部13,中間の弾
性連結部15から主として形成されており、曲り部のあ
る伝熱管1の中に挿入されるに適した構造となってい
る。即ち検査部11の先端部及び後端部に調芯部材17
が設けられ、その中間には圧縮コイルばね19により側
方に偏倚された渦流探触子21が設けられている。この
検査部11は、後述するように軸回りに回転されて探傷
が行われる。回転駆動部13は両端の調芯部材25に支
持された本体ケーシング27にモータ29を内蔵し、そ
の出力軸が弾性連結部15のフレキシブルシャフト31
に連結している。このフレキシブルシャフト31はコイ
ル状に巻回した金属線を多層に重ねたもので、長手方向
に等ピッチで配設された多数の支持部材33により伝熱
管1の内面に支持され、モータ29の回転を検査部11
に伝えて探触子21を回転させる。探触子21への給電
及び検出信号は、フレキシブルシャフト31に巻かれた
リード線35により伝達される。このような検査プロー
ブ10は、伝熱管1の外に置かれる送り装置により延長
管3を介して伝熱管1の中に挿入され即ち軸方向に送ら
れるから、回転駆動部13のモータ29により検査部1
1を同時に回転すれば、探触子21は螺旋軌跡を描いて
伝熱管1の内面を走査し、探傷検査が行われる。
2. Description of the Related Art In a tubular heat exchanger, a thin tube is used as a heat transfer tube, and various flaw detectors are used to non-destructively inspect the heat transfer tube for damage, defects and the like.
An eddy current inspection probe as shown in FIG. 4 is used for a heat transfer tube having a bent portion. This inspection probe 10
It is mainly formed of the inspection unit 11 at the distal end, the rotation drive unit 13 on the base end side, and the intermediate elastic connection unit 15, and has a structure suitable for being inserted into the heat transfer tube 1 having a bent portion. That is, the centering member 17 is provided at the front end and the rear end of the inspection unit 11.
, An eddy current probe 21 biased laterally by the compression coil spring 19 is provided in the middle. The inspection unit 11 is rotated about an axis to perform flaw detection as described later. The rotation drive unit 13 has a motor 29 built in a main body casing 27 supported by alignment members 25 at both ends, and its output shaft is a flexible shaft 31 of the elastic connection unit 15.
It is connected to. The flexible shaft 31 is formed by stacking multiple layers of metal wires wound in a coil shape, and is supported on the inner surface of the heat transfer tube 1 by a large number of support members 33 arranged at equal pitches in the longitudinal direction. Inspection unit 11
To rotate the probe 21. The power supply and the detection signal to the probe 21 are transmitted by a lead wire 35 wound around the flexible shaft 31. Such an inspection probe 10 is inserted into the heat transfer tube 1 via the extension tube 3 by the feeding device placed outside the heat transfer tube 1, that is, is sent in the axial direction. Part 1
When the probe 1 is simultaneously rotated, the probe 21 scans the inner surface of the heat transfer tube 1 in a spiral trajectory, and the flaw detection inspection is performed.

【0003】以上のものは、弾性連結部にフレキシブル
シャフトを使用しているので、回転伝達力が小さいとい
う難があるから、図5に示すような高伝達トルクの屈曲
連結構造も提案されている。これは案内短筒37に回転
自在に支持された軸をジンバル機構継手39で順次連結
しているものである。ジンバル機構継手39は、所定の
屈曲を許容するが捩り剛性が相対的に大きく、このため
回転角をロスなく伝達し、高トルクを伝達できるのであ
る。
[0003] In the above, since a flexible shaft is used for the elastic connecting portion, there is a difficulty that the rotational transmission force is small. Therefore, a bending connection structure having a high transmission torque as shown in FIG. 5 has also been proposed. . In this case, the shaft rotatably supported by the guide short cylinder 37 is sequentially connected by a gimbal mechanism joint 39. The gimbal mechanism joint 39 allows predetermined bending, but has relatively large torsional rigidity, so that it can transmit the rotation angle without loss and transmit high torque.

【0004】[0004]

【発明が解決しようとする課題】前述のように、弾性連
結部にフレキシブルシャフトを使用する検査プローブで
は、フレキシブルシャフトの弾性を利用して伝熱管の曲
り部に追従して挿入できるのであるが、その捩じり剛性
が相対的に小さい。このため挿入される管の曲り部の半
径が小さくなって連結部の抵抗が大きくなると、スティ
ックスリップを起こして検査部に回転むらが生じ、適正
な検査が困難になる。又、連結部にジンバル機構継手を
使用する検査プローブにおいては、屈曲して高トルクを
ロス無く伝達できるのであるが、長手軸に対する屈曲に
対し抵抗が小さい。このため図5に示すような挿入案内
管3と伝熱管1の接続部のように、挿入通路の内面に段
差があると、案内短筒が引っ掛かるという問題を生ず
る。前述の内面の段差は、検査プローブの先端の検査部
を伝熱管に効率良く整列、案内するために挿入案内管の
出口内面を拡大することにより生じたもので、これがな
いと検査プローブを被検査管に円滑に挿入するのが難し
い。従って、本発明は、曲げ半径が小さい伝熱管の内部
でも回転むらを生ぜずに検査部に回転を伝えて適正な検
査ができ、更に伝熱管の入口近傍に内面の不連続部が生
じても引っ掛かったりせずに円滑に挿入できる渦流探傷
検査プローブを提供することを課題とする。
As described above, in the inspection probe using the flexible shaft for the elastic connecting portion, the flexible probe can be inserted following the bent portion of the heat transfer tube by utilizing the elasticity of the flexible shaft. Its torsional rigidity is relatively small. For this reason, when the radius of the bent portion of the inserted tube is reduced and the resistance of the connecting portion is increased, stick slip is caused to cause uneven rotation of the inspection portion, making it difficult to perform an appropriate inspection. Further, in the inspection probe using the gimbal mechanism joint for the connecting portion, it can bend and transmit high torque without loss, but has a small resistance to bending with respect to the longitudinal axis. For this reason, if there is a step on the inner surface of the insertion passage, as in the connection portion between the insertion guide tube 3 and the heat transfer tube 1 as shown in FIG. 5, there arises a problem that the guide short tube is caught. The above-mentioned step on the inner surface is caused by enlarging the inner surface of the exit of the insertion guide tube in order to efficiently align and guide the inspection section at the tip of the inspection probe to the heat transfer tube. Difficult to insert smoothly into the tube. Therefore, according to the present invention, even in the case of a heat transfer tube having a small bending radius, the rotation can be transmitted to the inspection unit without causing rotation unevenness and proper inspection can be performed, and even if a discontinuous portion on the inner surface occurs near the entrance of the heat transfer tube. An object of the present invention is to provide an eddy current inspection probe that can be smoothly inserted without being caught.

【0005】[0005]

【課題を解決するための手段】如上の課題を解決するた
め、本発明によれば、渦流探傷検査プローブは、回転駆
動部と検査部と前記回転駆動部からの回転駆動力を前記
検査部に伝達する弾性連結部とからなり、その回転駆動
部は本体ケーシング内に設けられたモータとスリップリ
ングとを有し、前記検査部は、前端部及び後端部に配置
された第1調芯部材と、この第1調芯部材間に回転自在
に支持された渦流探触子と、この渦流探触子を半径方向
外方に偏倚するばねとを有し、更に前記弾性連結部は、
弾性中空管と、この弾性中空管の外面に回転自在に且つ
長手方向に並んで嵌装された複数の第2調芯部材と、隣
接する前記第2調芯部材を順次連結する複数の自在継手
とを有する。そして、前記弾性中空管としては、復元力
のある弾性ホース又は螺旋ばね管を用いると、内部に給
電及び出力信号用導線を挿通するのに好適であるが、弾
性中空管の代わりに超弾性体棒を使用しても、本発明の
大部分の特徴的作用効果が得られる。
According to the present invention, there is provided an eddy current inspection probe comprising: a rotary driving unit, an inspection unit, and a rotational driving force from the rotary driving unit; A rotational drive unit having a motor and a slip ring provided in a main body casing, and the inspection unit includes a first alignment member disposed at a front end and a rear end. An eddy current probe rotatably supported between the first alignment members, and a spring biasing the eddy current probe radially outward.
An elastic hollow tube, a plurality of second alignment members rotatably fitted on the outer surface of the elastic hollow tube in the longitudinal direction, and a plurality of second alignment members that sequentially connect the adjacent second alignment members. And a universal joint. When an elastic hose or a helical spring tube having a restoring force is used as the elastic hollow tube, it is preferable to insert a power supply and output signal conducting wire therein. Most of the characteristic effects of the present invention can be obtained by using the elastic rod.

【0006】[0006]

【発明の実施の形態】以下添付の図面を参照して本発明
の実施形態を説明する。先ず図1を参照するに、曲り部
を有する伝熱管1を探傷検査する探傷装置の検査プロー
ブ40は、先端の検査部即ちプローブヘッド部50、基
端側の回転駆動部即ちプローブボデー部60及び中間の
弾性連結部70から構成され、プローブボデー部60
は、可撓チューブ41を介して伝熱管1の外に置かれる
送り装置(図示しない)に連絡している。プローブヘッ
ド部50は、前端部及び後端部に調芯部材51を有し、
更に中央部に渦流探触子53を有するが、それらの詳細
構造は図2に示されている。図2を参照するに、例えば
弾性針状体を環状に植設してなる調芯部材51に軸受5
5を介してケーシング57が支持され、そのケーシング
57内に圧縮コイルばね59に偏倚されて渦流探触子5
3が支持されている。そして更にケーシング57の先端
には弾頭状の案内体58が取り付けられている。このた
め、伝熱管1の入口部において、案内体58がプローブ
ヘッド部50の進入を容易化し、渦流探触子53が半径
方向外側にある伝熱管1の内面に押し付けられつつ回転
が可能になっている。尚、渦流探触子53から延びたリ
ード線54は、後述するように外部の探傷器に連絡して
いる。
Embodiments of the present invention will be described below with reference to the accompanying drawings. First, referring to FIG. 1, an inspection probe 40 of a flaw detector for flaw-detecting a heat transfer tube 1 having a bent portion includes an inspection unit at a distal end, ie, a probe head unit 50, a rotation driving unit, ie, a probe body unit 60 at a proximal end side, and a probe body 60. The probe body 60 is composed of an intermediate elastic connection 70.
Is connected via a flexible tube 41 to a feeding device (not shown) placed outside the heat transfer tube 1. The probe head 50 has a centering member 51 at the front end and the rear end,
Further, a vortex probe 53 is provided at the center, and their detailed structure is shown in FIG. Referring to FIG. 2, for example, a bearing 5 is mounted on a centering member 51 in which an elastic needle-like body is implanted in a ring shape.
5, a casing 57 is supported, and is biased by a compression coil spring 59 in the casing 57 so that the eddy current probe 5
3 are supported. Further, a warhead-shaped guide body 58 is attached to the tip of the casing 57. For this reason, at the entrance of the heat transfer tube 1, the guide body 58 facilitates the entry of the probe head portion 50, and the eddy current probe 53 can rotate while being pressed against the inner surface of the heat transfer tube 1 on the radially outer side. ing. The lead wire 54 extending from the eddy current probe 53 is connected to an external flaw detector as described later.

【0007】再び図1を参照するに、プローブボデー部
60の本体ケーシング61には、モータ63が設けら
れ、そこから延びた給電線及び制御線はリード線65と
なって可撓チューブ41の中を延び、伝熱管1の外側に
置かれる図示しない制御盤に連絡している。モータ63
の出力軸にはスリップリング67が取付けられ、前述の
リード線54の接続を行い、そのリード線54はリード
線65に纏められている。モータ63の出力軸に連絡
し、その回転力をプローブヘッド部50に伝達する弾性
連結部70は、複数の調芯部材71とジンバル機構継手
73を有しているが、その詳細構造は図3に示されてい
る。図3において、両端がジンバル機構継手73に連結
された中空軸75には、軸受77を介して調芯部材71
が嵌装されている。この調芯部材71は、軸受77に嵌
合する内筒部71aと軸方向の切れ目71bで周方向に
分割された外筒フィンガ部71cを有し、全体として弾
性材料から形成されている。このため山形の外面形状を
持つ外筒フィンガ部71cは、中心連結部71dを支持
端とした片持ち梁のように弾性変形し、調芯作用を行
う。そして、中空軸75及びジンバル機構継手73を貫
いて弾性ホース79が延びていて、その中を渦流探触子
53からのリード線54が通っている。そして、図1に
示すように、プローブボデー部60側の端部のジンバル
機構継手73は、モータ63の出力軸に連結されてい
る。尚、弾性ホース79の代わりに螺旋ピッチの小さ
い、例えば線径にほぼ等しい管状のコイルばねを使用し
ても良い。この場合でも、リード線54は、コイルばね
の中に通される。
Referring to FIG. 1 again, a motor 63 is provided on a main body casing 61 of the probe body 60, and a power supply line and a control line extending from the motor 63 become lead wires 65 inside the flexible tube 41. And communicates with a control panel (not shown) placed outside the heat transfer tube 1. Motor 63
A slip ring 67 is attached to the output shaft of the first embodiment to connect the above-mentioned lead wire 54, and the lead wire 54 is combined with a lead wire 65. The elastic connecting portion 70 that communicates with the output shaft of the motor 63 and transmits the rotational force to the probe head portion 50 has a plurality of centering members 71 and a gimbal mechanism joint 73, the detailed structure of which is shown in FIG. Is shown in In FIG. 3, a hollow shaft 75 having both ends connected to a gimbal mechanism joint 73 is provided with a centering member 71 via a bearing 77.
Is fitted. The centering member 71 has an inner cylindrical portion 71a fitted to the bearing 77, and an outer cylindrical finger portion 71c divided in the circumferential direction by a cut 71b in the axial direction, and is entirely made of an elastic material. For this reason, the outer cylindrical finger portion 71c having a mountain-shaped outer surface shape elastically deforms like a cantilever having the center connecting portion 71d as a support end, and performs a centering action. An elastic hose 79 extends through the hollow shaft 75 and the gimbal mechanism joint 73, and the lead wire 54 from the eddy current probe 53 passes through the elastic hose 79. As shown in FIG. 1, the gimbal mechanism joint 73 at the end on the probe body 60 side is connected to the output shaft of the motor 63. Instead of the elastic hose 79, a tubular coil spring having a small helical pitch, for example, approximately equal to the wire diameter may be used. Even in this case, the lead wire 54 is passed through the coil spring.

【0008】以上の構成の検査プローブ40を使用して
探傷検査を行うには、伝熱管1の端部からプローブヘッ
ド部50を先頭にして検査プローブ40を押込む。この
際案内体58が芯合わせ作用を行う。可撓チューブ41
等を掴持し、或いは送り装置により伝熱管1の中に検査
プローブ40を送り込んでいくと、プローブヘッド部5
0は調芯部材51により伝熱管1の中で同軸に保持され
る。伝熱管1に図1に示すような曲り部があれば、その
曲りに倣って弾性連結部70が変形していく。検査すべ
き伝熱管1の形状寸法は、製作図等の設計資料により既
知であるから弾性連結部70の長さは予めこれを見込ん
でおけば良い。プローブヘッド部50の伝熱管1内位置
は、可撓チューブ41等の送り量で分かるから、検査領
域に達すれば、送り装置による送りとモータ63の回転
駆動を組み合わせる。このようにして、モータ63の回
転変位は弾性連結部70によりプローブヘッド部50の
ケーシング57に伝えられ、その軸回りの回転となる。
即ち、渦流探触子53は、螺旋軌跡を描いて伝熱管1の
内面を走査している。このような走査に際し渦流探触子
53にリード線54を介して励磁電流を送り、他方渦流
信号を検出して探傷器に送る。このようにして探傷検査
が行われる。弾性連結部70の変形追従に際しては、調
芯部材71の外筒フィンガ部71cが両端部でバランス
よく変形するので、中空軸75及び内部の弾性ホース7
9を伝熱管1の中心に保持する。調芯部材71に軸受7
7を介して支持された中空軸75は、自在継手であるジ
ンバル機構継手73により相互に連結されているので、
モータ67の回転は損失無くプローブヘッド部50のケ
ーシング57に伝達される。尚、前述の実施形態の弾性
ホース79やコイルばね管に代えて超弾性棒を使用して
も良いが、その場合はリード線54は、外面に沿わせて
適宜保持することになる。
To perform a flaw detection inspection using the inspection probe 40 having the above-described configuration, the inspection probe 40 is pushed in from the end of the heat transfer tube 1 with the probe head 50 at the head. At this time, the guide body 58 performs a centering operation. Flexible tube 41
When the inspection probe 40 is fed into the heat transfer tube 1 by the feed device, the probe head 5
0 is coaxially held in the heat transfer tube 1 by the core adjusting member 51. If the heat transfer tube 1 has a bent portion as shown in FIG. 1, the elastic connecting portion 70 is deformed following the bent portion. Since the shape and dimensions of the heat transfer tube 1 to be inspected are known from design data such as production drawings, the length of the elastic connecting portion 70 may be estimated in advance. Since the position in the heat transfer tube 1 of the probe head 50 can be determined by the feed amount of the flexible tube 41 or the like, when the position reaches the inspection area, the feed by the feed device and the rotation drive of the motor 63 are combined. In this manner, the rotational displacement of the motor 63 is transmitted to the casing 57 of the probe head 50 by the elastic connecting portion 70, and is rotated around its axis.
That is, the eddy current probe 53 scans the inner surface of the heat transfer tube 1 in a spiral trajectory. At the time of such scanning, an exciting current is sent to the eddy current probe 53 via the lead wire 54, while an eddy current signal is detected and sent to the flaw detector. The flaw detection inspection is performed in this manner. When the deformation of the elastic connecting portion 70 is followed, the outer cylindrical finger portion 71c of the alignment member 71 is deformed in a balanced manner at both ends, so that the hollow shaft 75 and the internal elastic hose 7 are formed.
9 is held at the center of the heat transfer tube 1. Bearing 7 on alignment member 71
Since the hollow shaft 75 supported via 7 is connected to each other by a gimbal mechanism joint 73 which is a universal joint,
The rotation of the motor 67 is transmitted to the casing 57 of the probe head 50 without any loss. A superelastic rod may be used in place of the elastic hose 79 and the coil spring tube of the above-described embodiment, but in that case, the lead wire 54 is appropriately held along the outer surface.

【0009】[0009]

【発明の効果】以上説明したように、本発明によれば先
端の検査部と基端側の回転駆動部とを繋ぐ弾性連結部に
自在継手としてジンバル機構継手を使用し、その中心に
弾性中空管を通したので、回転駆動部の回転がロス無く
検査部に伝達され、渦流探触子が所定の軌跡で伝熱管の
内面を走査し、適切な探傷検査が行うことができる。更
に弾性中空管の変形復元力により自在継手に屈曲復元機
能が付与されたので、移動通路内面に不連続部があって
も引っ掛かることはなく、伝熱管内で検査ぷローブを円
滑に移動することができる。
As described above, according to the present invention, a gimbal mechanism joint is used as a universal joint at the elastic connecting part connecting the inspection part at the distal end and the rotary driving part at the base end, and the elastic joint is provided at the center thereof. Since the air has passed through the empty tube, the rotation of the rotary drive unit is transmitted to the inspection unit without loss, and the eddy current probe scans the inner surface of the heat transfer tube with a predetermined trajectory, so that appropriate flaw detection inspection can be performed. In addition, since the flexible joint is provided with a bending restoration function by the deformation restoring force of the elastic hollow tube, even if there is a discontinuous portion on the inner surface of the moving passage, it is not caught and the inspection lobe moves smoothly in the heat transfer tube. be able to.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の実施形態の全体構造図である。FIG. 1 is an overall structural diagram of an embodiment of the present invention.

【図2】図1の部分拡大断面図である。FIG. 2 is a partially enlarged sectional view of FIG.

【図3】図1の別の部分の拡大断面図である。FIG. 3 is an enlarged sectional view of another part of FIG. 1;

【図4】従来のものの一例を示す全体側面図である。FIG. 4 is an overall side view showing an example of a conventional one.

【図5】別の従来装置の概念説明図である。FIG. 5 is a conceptual explanatory view of another conventional apparatus.

【符号の説明】[Explanation of symbols]

40 検査プローブ 41 可撓チューブ 50 プローブヘッド部 51 調芯部材 53 渦流探触子 54 リード線 55 軸受 57 ケーシング 58 案内体 59 圧縮コイルばね 60 プローブボデー部 61 本体ケーシング 63 モータ 65 リード線 70 弾性連結部 71 調芯部材 73 ジンバル機構継手 75 中空軸 77 軸受 79 弾性ホース Reference Signs List 40 inspection probe 41 flexible tube 50 probe head 51 alignment member 53 eddy current probe 54 lead 55 bearing 57 casing 58 guide 59 compression coil spring 60 probe body 61 main body casing 63 motor 65 lead wire 70 elastic connection portion 71 Aligning member 73 Gimbal mechanism joint 75 Hollow shaft 77 Bearing 79 Elastic hose

Claims (3)

【特許請求の範囲】[Claims] 【請求項1】 回転駆動部と検査部と前記回転駆動部か
らの回転駆動力を前記検査部に伝達する弾性連結部とか
らなり、 前記回転駆動部は本体ケーシング内に設けられたモータ
とスリップリングとを有し、 前記検査部は、前端部及び後端部に配置された第1調芯
部材と、同第1調芯部材間に回転自在に支持された渦流
探触子と、同渦流探触子を半径方向外方に偏倚するばね
とを有し、 前記弾性連結部は、弾性中空管と、同弾性中空管の外面
に回転自在に且つ長手方向に並んで嵌装された複数の第
2調芯部材と、隣接する前記第2調芯部材を順次連結す
る複数の自在継手とを有することを特徴とする渦流探傷
検査プローブ。
1. A rotary drive unit, an inspection unit, and an elastic connection unit for transmitting a rotational drive force from the rotary drive unit to the inspection unit, wherein the rotary drive unit slips with a motor provided in a main body casing. A first alignment member disposed at a front end portion and a rear end portion; an eddy current probe rotatably supported between the first alignment member; A spring for biasing the probe radially outward, wherein the elastic connecting portion is rotatably fitted to the outer surface of the elastic hollow tube so as to be rotatable and arranged in the longitudinal direction. An eddy current inspection probe comprising: a plurality of second alignment members; and a plurality of universal joints for sequentially connecting adjacent second alignment members.
【請求項2】 前記弾性中空管が弾性ホース又は螺旋ば
ね管であることを特徴とする請求項1の渦流探傷検査プ
ローブ。
2. The eddy current inspection probe according to claim 1, wherein the elastic hollow tube is an elastic hose or a helical spring tube.
【請求項3】 前記弾性中空管に代えて超弾性体棒を使
用することを特徴とする請求項1の渦流探傷検査プロー
ブ。
3. The eddy current inspection probe according to claim 1, wherein a superelastic rod is used instead of the elastic hollow tube.
JP22012996A 1996-08-21 1996-08-21 Eddy current inspection probe Expired - Fee Related JP3254138B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP22012996A JP3254138B2 (en) 1996-08-21 1996-08-21 Eddy current inspection probe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP22012996A JP3254138B2 (en) 1996-08-21 1996-08-21 Eddy current inspection probe

Publications (2)

Publication Number Publication Date
JPH1062093A true JPH1062093A (en) 1998-03-06
JP3254138B2 JP3254138B2 (en) 2002-02-04

Family

ID=16746368

Family Applications (1)

Application Number Title Priority Date Filing Date
JP22012996A Expired - Fee Related JP3254138B2 (en) 1996-08-21 1996-08-21 Eddy current inspection probe

Country Status (1)

Country Link
JP (1) JP3254138B2 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012083110A (en) * 2010-10-06 2012-04-26 Mitsubishi Heavy Ind Ltd Calibration method, calibration jig and tube inspection method
CN104914157A (en) * 2015-05-08 2015-09-16 上海海事大学 Nondestructive detection apparatus for detects in miniature space of metal structure
CN108132298A (en) * 2018-02-02 2018-06-08 山东大学 A kind of vertical retractable type eddy current probe and its application based on the detection of piston aditus laryngis
CN109444258A (en) * 2018-12-21 2019-03-08 核动力运行研究所 A kind of small diameter tube vortex rotating detector

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012083110A (en) * 2010-10-06 2012-04-26 Mitsubishi Heavy Ind Ltd Calibration method, calibration jig and tube inspection method
CN104914157A (en) * 2015-05-08 2015-09-16 上海海事大学 Nondestructive detection apparatus for detects in miniature space of metal structure
CN108132298A (en) * 2018-02-02 2018-06-08 山东大学 A kind of vertical retractable type eddy current probe and its application based on the detection of piston aditus laryngis
CN109444258A (en) * 2018-12-21 2019-03-08 核动力运行研究所 A kind of small diameter tube vortex rotating detector

Also Published As

Publication number Publication date
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