CN111812193B - Array eddy current probe for actively relieving electromagnetic coupling between adjacent coils - Google Patents
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Abstract
本发明提出一种主动解除相邻线圈之间电磁耦合的阵列涡流探头,主要解决现有的阵列涡流探头采用屏蔽罩被动屏蔽电磁耦合的两个不足:一、阻隔了罩内检测线圈焦耳热与外部对流换热的通道,易造成线圈温升,带来温漂误差;二、增大探头体积,探头空间分辨力降低。其技术方案为:在探头检测线圈外设置两个与检测线圈同轴的辅助线圈,辅助线圈产生的磁场削弱检测线圈产生的外部磁场,从而减小相邻检测线圈的磁场干扰。辅助线圈上装有金属滑片,移动滑片可改变辅助线圈接入加载电路的长度和匝数,进而调节外部磁场的削弱程度,满足不同应用场景对相邻线圈电磁解耦程度的不同要求。与现有阵列涡流探头相比,本发明提出的探头体积更小、温漂误差更小。
The present invention proposes an array eddy current probe that actively releases the electromagnetic coupling between adjacent coils, which mainly solves the two shortcomings of the existing array eddy current probe that uses a shielding cover to passively shield the electromagnetic coupling: 1. It blocks the Joule heat of the detection coil in the cover and The external convective heat transfer channel will easily cause the temperature rise of the coil and cause temperature drift errors; 2. Increase the volume of the probe, and the spatial resolution of the probe will decrease. The technical solution is: outside the detection coil of the probe, two auxiliary coils coaxial with the detection coil are arranged, and the magnetic field generated by the auxiliary coil weakens the external magnetic field generated by the detection coil, thereby reducing the magnetic field interference of adjacent detection coils. The auxiliary coil is equipped with a metal slide, and moving the slide can change the length and number of turns of the auxiliary coil connected to the loading circuit, thereby adjusting the weakening degree of the external magnetic field to meet the different requirements of different application scenarios for the degree of electromagnetic decoupling of adjacent coils. Compared with the existing array eddy current probe, the probe proposed by the invention has smaller volume and smaller temperature drift error.
Description
技术领域technical field
本发明属于无损检测技术领域,进一步属于电涡流检测技术领域,具体涉及一种用于无损检测的阵列涡流探头,尤其涉及一种降低相邻检测线圈之间电磁耦合的、无屏蔽罩的阵列涡流探头。The invention belongs to the technical field of non-destructive testing, and further belongs to the technical field of eddy current testing, in particular to an array eddy current probe for non-destructive testing, in particular to an array eddy current probe without a shield that reduces electromagnetic coupling between adjacent detection coils probe.
背景技术Background technique
涡流检测是一种在工业领域应用广泛的无损检测技术,工作原理基于电磁感应原理:当通有交变电流的检测线圈靠近金属导体时,将在金属导体中产生交变磁场,称为一次磁场,同时该交变磁场在金属导体表面感应出电涡流;金属导体中的电涡流也会产生磁场,称为二次磁场;金属导体表面如果存在裂纹等缺陷,将会引起电涡流的变化,这一变化再经二次磁场在检测线圈中得以感应,最终表征为线圈阻抗的变化,由此就可以判断金属导体表面缺陷的存在及严重程度。电涡流检测具有非接触、速度快、对表面缺陷灵敏度高等优势。单检测线圈式涡流探头覆盖面积小,对较大面积试件进行逐点扫查检测不仅费时费力,有时还可能出现漏检。阵列涡流探头由多个独立的检测线圈排列组成,与单检测线圈式探头相比具有如下优势:探头覆盖面积大,检测效率高;可根据被检测试件的尺寸和形面进行外形设计,不需要设计制作复杂的机械扫查装置。但是,相邻检测线圈之间存在电磁耦合,所引起的检测线圈阻抗变化会叠加在由缺陷引起的阻抗变化之中,从而造成检测结果的偏差。为解决这一问题,当前多采用在检测线圈外设置由电磁屏蔽罩的方法。但是,封闭的屏蔽罩结构会阻碍罩内通电线圈的热量交换,易造成线圈过热,影响线圈的精度和使用寿命;其次,屏蔽罩的引入会增大探头的体积,导致探头的空间分辨能力低。因此,发明一种无需增加屏蔽罩结构、亦能去除检测线圈之间电磁耦合效应的阵列涡流探头是十分必要的。Eddy current testing is a non-destructive testing technology widely used in the industrial field. Its working principle is based on the principle of electromagnetic induction: when the detection coil with alternating current is close to the metal conductor, an alternating magnetic field will be generated in the metal conductor, which is called the primary magnetic field. , at the same time, the alternating magnetic field induces an eddy current on the surface of the metal conductor; the eddy current in the metal conductor will also generate a magnetic field, which is called a secondary magnetic field; if there are defects such as cracks on the surface of the metal conductor, it will cause changes in the eddy current, which A change is then induced in the detection coil by the secondary magnetic field, and finally characterized as a change in coil impedance, from which the existence and severity of defects on the surface of the metal conductor can be judged. Eddy current testing has the advantages of non-contact, fast speed, and high sensitivity to surface defects. The single detection coil eddy current probe has a small coverage area, and it is time-consuming and labor-intensive to perform point-by-point scanning and detection of larger-area specimens, and sometimes missed detection may occur. The array eddy current probe is composed of multiple independent detection coils. Compared with the single detection coil probe, the array eddy current probe has the following advantages: the probe covers a large area and the detection efficiency is high; It is necessary to design and manufacture complex mechanical scanning devices. However, there is electromagnetic coupling between adjacent detection coils, and the resulting change in the impedance of the detection coil will be superimposed on the impedance change caused by the defect, resulting in deviations in the detection results. In order to solve this problem, the method of setting an electromagnetic shield outside the detection coil is currently used. However, the closed shield structure will hinder the heat exchange of the energized coil in the shield, which will easily cause the coil to overheat and affect the accuracy and service life of the coil; secondly, the introduction of the shield will increase the volume of the probe, resulting in low spatial resolution of the probe . Therefore, it is very necessary to invent an array eddy current probe that can eliminate the electromagnetic coupling effect between detection coils without adding a shield structure.
发明内容Contents of the invention
本发明的目的在于克服现有技术的不足,提供一种可以主动解除相邻线圈之间电磁耦合的阵列涡流探头,该探头具有以下优势:无须在检测线圈外增加屏蔽罩,便于检测线圈的焦耳热及时耗散以免造成过热;探头体积减小,空间分辨力得到提高。The purpose of the present invention is to overcome the deficiencies of the prior art and provide an array eddy current probe that can actively release the electromagnetic coupling between adjacent coils. The heat is dissipated in time to avoid overheating; the volume of the probe is reduced, and the spatial resolution is improved.
本发明解决其技术问题所采用的技术方案是:去掉屏蔽罩,在检测线圈外布置与两个与检测线圈同轴、分别位于检测线圈两个端部的螺线管线圈作为辅助线圈;辅助线圈产生的磁场削弱检测线圈产生的在径向分布的外部磁场,从而减小相邻检测线圈之间的磁场干扰;在辅助线圈上设置变阻器式金属滑片,将金属滑片和辅助线圈的一个终端接入辅助线圈的加载电路,这样通过移动金属滑片可改变辅助线圈接入加载电路的长度和匝数,调整辅助线圈磁场对检测线圈磁场的削弱程度,以满足不同应用场景对检测线圈之间电磁解耦程度的不同要求。The technical scheme adopted by the present invention to solve the technical problem is: remove the shielding cover, and arrange two solenoid coils coaxial with the detection coil and respectively located at the two ends of the detection coil as auxiliary coils outside the detection coil; The generated magnetic field weakens the radially distributed external magnetic field generated by the detection coil, thereby reducing the magnetic field interference between adjacent detection coils; a rheostat-type metal slide is set on the auxiliary coil, and a terminal of the metal slide and the auxiliary coil is connected Access to the loading circuit of the auxiliary coil, so that the length and number of turns of the auxiliary coil connected to the loading circuit can be changed by moving the metal slide, and the degree of weakening of the magnetic field of the auxiliary coil to the magnetic field of the detection coil can be adjusted to meet the needs of different application scenarios. Different requirements for the degree of electromagnetic decoupling.
本发明的技术效果体现在:(a)无需在探头检测线圈外设置屏蔽罩结构,有利于探头工作时产生的焦耳热得到及时扩散,提高探头的热稳定性,减小温度漂移对检测信号的影响;同时,减小了探头体积,提高了探头的空间分辨力。(b)在不同应用场景下,无需重新设计和制作探头,通过移动辅助线圈上的金属滑片,即可实现相邻检测线圈之间电磁耦合效应不同程度的解耦。The technical effect of the present invention is reflected in: (a) no shielding cover structure needs to be arranged outside the probe detection coil, which is conducive to the timely diffusion of Joule heat generated when the probe is working, improves the thermal stability of the probe, and reduces the impact of temperature drift on the detection signal At the same time, the volume of the probe is reduced and the spatial resolution of the probe is improved. (b) In different application scenarios, without redesigning and manufacturing the probe, the electromagnetic coupling effect between adjacent detection coils can be decoupled to different degrees by moving the metal slide on the auxiliary coil.
附图说明Description of drawings
图1为本发明的阵列探头总体结构图;Fig. 1 is the overall structural diagram of the array probe of the present invention;
图2为本发明的子探头结构图;Fig. 2 is a sub-probe structural diagram of the present invention;
图3为本发明的子探头线圈电流加载实施方案。Fig. 3 is an embodiment of the sub-probe coil current loading of the present invention.
具体实施方式Detailed ways
本发明设计的阵列探头总体结构图如图1所示。该探头由多个相互之间以一定距离隔开的独立的子探头(10)组成,每个子探头具有相同的结构:检测线圈(1)外部设置第一辅助线圈(2)和第二辅助线圈(3),它们与检测线圈(1)同轴,且分别位于检测线圈(1)的上下两端。检测线圈(1)为空心圆柱线圈,第一辅助线圈(2)和第二辅助线圈(3)为螺线管式线圈,且检测线圈(1)、第一辅助线圈(2)和第二辅助线圈(3)三者的绕线分离。第一辅助线圈(2)与第一金属滑片(4)接触并导通,第二辅助线圈(3)与第二金属滑片(5)接触并导通。检测线圈(1)的两个终端连接加载电路(6),第一辅助线圈(2)和第二辅助线圈(3)分别接入第一辅助加载电路(7)和加载电路(8)。加载电路(6)、第一辅助加载电路(7)和第二辅助加载电路(8)输出的电流具有相同的频率。第一金属滑片(4)和第二金属滑片(5)安装在导轨(9)上,在导轨(9)上移动第一金属滑片(4)和第二金属滑片(5)可分别改变第一辅助线圈(2)和第二辅助线圈(3)各自接入第一辅助加载电路(7)和第二辅助加载电路(8)的长度和匝数。当加载电路(6)接通时,检测线圈(1)产生激励磁场,该磁场一方面在被测构件中感应出电涡流用于检测,另一方面其径向分量也会影响与之相邻的检测线圈,产生电磁耦合效应。当第一辅助加载电路(7)和第二辅助加载电路(8)接通时,第一辅助线圈(2)和第二辅助线圈(3)产生的磁场与检测线圈(1)产生的激励磁场方向相反,且在轴向快速衰减。这一磁场可大大抵消检测线圈(1)产生的激励磁场的径向分量,而对在被测构件内激发出涡流的轴向磁场影响很小,从而削弱了相邻检测线圈之间的电磁耦合,又不会对探头的检测能力造成影响。The overall structure diagram of the array probe designed by the present invention is shown in FIG. 1 . The probe is composed of a plurality of independent sub-probes (10) separated by a certain distance from each other, and each sub-probe has the same structure: a first auxiliary coil (2) and a second auxiliary coil are arranged outside the detection coil (1) (3), they are coaxial with the detection coil (1), and are respectively located at the upper and lower ends of the detection coil (1). The detection coil (1) is a hollow cylindrical coil, the first auxiliary coil (2) and the second auxiliary coil (3) are solenoid coils, and the detection coil (1), the first auxiliary coil (2) and the second auxiliary coil The windings of the three coils (3) are separated. The first auxiliary coil (2) contacts and conducts with the first metal slide (4), and the second auxiliary coil (3) contacts and conducts with the second metal slide (5). Two terminals of the detection coil (1) are connected to a loading circuit (6), and a first auxiliary coil (2) and a second auxiliary coil (3) are respectively connected to a first auxiliary loading circuit (7) and a loading circuit (8). Currents output by the loading circuit (6), the first auxiliary loading circuit (7) and the second auxiliary loading circuit (8) have the same frequency. The first metal slide (4) and the second metal slide (5) are installed on the guide rail (9), and the first metal slide (4) and the second metal slide (5) can be moved on the guide rail (9). The length and the number of turns of the first auxiliary coil (2) and the second auxiliary coil (3) connected to the first auxiliary loading circuit (7) and the second auxiliary loading circuit (8) are respectively changed. When the loading circuit (6) is turned on, the detection coil (1) generates an excitation magnetic field, which on the one hand induces an eddy current in the component under test for detection, and on the other hand its radial component will also affect the adjacent The detection coil produces electromagnetic coupling effect. When the first auxiliary loading circuit (7) and the second auxiliary loading circuit (8) are switched on, the magnetic field produced by the first auxiliary coil (2) and the second auxiliary coil (3) and the excitation magnetic field produced by the detection coil (1) The direction is opposite and decays rapidly in the axial direction. This magnetic field can largely cancel the radial component of the excitation magnetic field generated by the detection coil (1), but has little effect on the axial magnetic field that excites eddy currents in the measured component, thus weakening the electromagnetic coupling between adjacent detection coils , and will not affect the detection ability of the probe.
图2所示为利用本发明方法实现的一种阵列涡流探头的子探头结构图。子探头(10)包括检测线圈(1)、第一辅助线圈(2)、第二辅助线圈(3)、金属滑片(4)、金属滑片(5)、导轨(9)、检测线圈骨架(11)、辅助线圈骨架(12)、外壳(13)、弹性垫圈(14)、支撑板(15)、航空插座(16)和4芯线缆(17)。检测线圈(1)缠绕在检测线圈骨架(11)上,第一辅助线圈(2)和第二辅助线圈(3)缠绕在辅助线圈骨架(12)上。导轨(9)安装在外壳(13)上,且标记有刻度。第一金属滑片(4)和第二金属滑片(5)安装在导轨(9)上,它们的触头分别与第一辅助线圈(2)和第二辅助线圈(3)接通。检测线圈(1)的两个终端通过航空插座(16)与4芯线缆(17)的第1、2芯相连;第一辅助线圈(2)的上终端与4芯线缆(17)的第3芯相连;第二辅助线圈(3)的下终端与4芯线缆(17)的第4芯相连。4芯线缆(17)的第1、2芯接入加载电路(6),第一金属滑片(4)和4芯线缆(17)的第3芯接入加载电路(7),第二金属滑片(5)和4芯线缆(17)的第4芯接入加载电路(8)。根据导轨(9)上的刻度移动第一金属滑片(4)和金属滑片(5),可分别控制第二辅助线圈(3)和第二辅助线圈(3)各自接入第一辅助加载电路(7)和第二辅助加载电路(8)的长度。子探头(10)通过弹性垫圈(14)和航空插座(16),以悬挂的形式安装在阵列探头的支撑板(15)上。Fig. 2 is a sub-probe structure diagram of an array eddy current probe realized by the method of the present invention. The sub-probe (10) includes a detection coil (1), a first auxiliary coil (2), a second auxiliary coil (3), a metal slide (4), a metal slide (5), a guide rail (9), and a detection coil skeleton (11), auxiliary coil skeleton (12), shell (13), elastic washer (14), support plate (15), aviation socket (16) and 4-core cable (17). The detection coil (1) is wound on the detection coil skeleton (11), and the first auxiliary coil (2) and the second auxiliary coil (3) are wound on the auxiliary coil skeleton (12). Guide rail (9) is installed on the shell (13), and mark has scale. The first metal slide (4) and the second metal slide (5) are installed on the guide rail (9), and their contacts are connected with the first auxiliary coil (2) and the second auxiliary coil (3) respectively. The two terminals of the detection coil (1) are connected to the 1st and 2nd cores of the 4-core cable (17) through the aviation socket (16); the upper terminal of the first auxiliary coil (2) is connected to the 4-core cable (17) The third core is connected; the lower terminal of the second auxiliary coil (3) is connected with the fourth core of the 4-core cable (17). The first and second cores of the 4-core cable (17) are connected to the loading circuit (6), and the first metal slide (4) and the third core of the 4-core cable (17) are connected to the loading circuit (7). The 4th core of the two metal slides (5) and the 4-core cable (17) is connected to the loading circuit (8). Move the first metal slide (4) and the metal slide (5) according to the scale on the guide rail (9), respectively control the second auxiliary coil (3) and the second auxiliary coil (3) to access the first auxiliary load The length of the circuit (7) and the second auxiliary loading circuit (8). The sub-probe (10) is installed on the support plate (15) of the array probe in the form of suspension through the elastic washer (14) and the aviation socket (16).
辅助线圈的布置方式不局限于上述的一组线圈对称布置方式,包括但不限于单个线圈、多组线圈对称布置等布置方式,只要能够抵消检测线圈产生的激励磁场的径向分量即可。The arrangement of the auxiliary coils is not limited to the above-mentioned symmetrical arrangement of a group of coils, including but not limited to a single coil, symmetrical arrangement of multiple sets of coils, etc., as long as the radial component of the exciting magnetic field generated by the detection coil can be canceled out.
图3所示为本发明的子探头线圈电流加载实施方案。若检测线圈(1)、第一辅助线圈(2)和第二辅助线圈(3)三个线圈的旋向相同,则第一辅助线圈(2)和第二辅助线圈(3)中加载同相位的电流,而检测线圈(1)中加载与前两者反相位的电流;若第一辅助线圈(2)和第二辅助线圈(3)的旋向相同,而与检测线圈(1)的旋向相反,则三个线圈加载同相位的电流;若检测线圈(1)和第一辅助线圈(2)的旋向相同,而与第二辅助线圈(3)的旋向相反,则检测线圈(1)和第二辅助线圈(3)加载同相位的电流,而第一辅助线圈(2)加载与前两者反相位的电流;若检测线圈(1)和第二辅助线圈(3)的旋向相同,而与第一辅助线圈(2)的旋向相反,则检测线圈(1)和第一辅助线圈(2)加载同相位的电流,而第二辅助线圈(3)加载与前两者反相位的电流。Fig. 3 shows the current loading implementation of the sub-probe coil of the present invention. If the detection coil (1), the first auxiliary coil (2) and the second auxiliary coil (3) have the same rotation direction, then the first auxiliary coil (2) and the second auxiliary coil (3) are loaded with the same phase The current of the detection coil (1) is loaded with the current of the opposite phase with the first two; if the first auxiliary coil (2) and the second auxiliary coil (3) have the same rotation direction, and the detection coil (1) If the direction of rotation is opposite, the three coils are loaded with the same phase current; if the direction of rotation of the detection coil (1) and the first auxiliary coil (2) is the same, and the direction of rotation of the second auxiliary coil (3) is opposite, the detection coil (1) and the second auxiliary coil (3) are loaded with the current of the same phase, and the first auxiliary coil (2) is loaded with the current of the opposite phase with the former two; if the detection coil (1) and the second auxiliary coil (3) The direction of rotation is the same as that of the first auxiliary coil (2), and the detection coil (1) and the first auxiliary coil (2) are loaded with the same phase current, while the second auxiliary coil (3) is loaded with the same phase current as the first auxiliary coil (2). The two currents are in opposite phases.
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