CN211402244U - Test block - Google Patents
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- CN211402244U CN211402244U CN201921504879.8U CN201921504879U CN211402244U CN 211402244 U CN211402244 U CN 211402244U CN 201921504879 U CN201921504879 U CN 201921504879U CN 211402244 U CN211402244 U CN 211402244U
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Abstract
本实用新型提供一种检测试块,用于对涡流检测仪器进行标定,涡流检测仪器检测试块的材料与待检测工件的材料一致,而且涡流检测仪器检测试块上设置有与待检测对象尺寸一致的孔,孔的开口位于检测试块的表面处,且孔的延伸方向与该表面垂直,限定孔的壁面上设置有缺陷,缺陷与待检测工件上的待检测缺陷的形式一致。本实用新型的检验试块,具有对应于待检测工件的装配孔的孔结构,孔结构处设置有用于模拟实际缺陷的结构,用该检测试块完成标定的检验设备能够在实际检测时具有较好的检测精度。
The utility model provides a detection test block, which is used for calibrating an eddy current detection instrument. The material of the detection test block of the eddy current detection instrument is consistent with the material of the workpiece to be detected, and the detection test block of the eddy current detection instrument is provided with a size corresponding to the size of the object to be detected. Consistent hole, the opening of the hole is located on the surface of the test block, and the extension direction of the hole is perpendicular to the surface, and the wall surface of the defined hole is provided with defects, and the defects are in the same form as the defects to be detected on the workpiece to be detected. The inspection test block of the utility model has a hole structure corresponding to the assembly hole of the workpiece to be inspected, and the hole structure is provided with a structure for simulating actual defects. good detection accuracy.
Description
技术领域technical field
本实用新型涉及飞行器维修与制造领域,具体涉及一种检测试块。The utility model relates to the field of aircraft maintenance and manufacture, in particular to a detection test block.
背景技术Background technique
在对飞行器上的导电性工件进行检测时,通常会采用涡流检测方法。涡流检测方法是以电磁感应为基础的无损检测技术,适用于导电材料检测,在民航无损检测中应用非常广泛。其中需要用到检测试块来对涡流检测仪器进行标定,因此检测试块是客机无损检测重要组成部分,是保障飞机安全运行的基础。Eddy current testing is usually used when testing conductive workpieces on aircraft. The eddy current testing method is a non-destructive testing technology based on electromagnetic induction, which is suitable for the testing of conductive materials and is widely used in civil aviation non-destructive testing. Among them, a test block is needed to calibrate the eddy current testing instrument. Therefore, the test block is an important part of the non-destructive testing of passenger aircraft and the basis for ensuring the safe operation of the aircraft.
现有的待检测工件多为采用螺栓或者铆钉连接的多层金属结构,在持续飞行过程中螺栓孔或铆钉孔有产生裂纹等缺陷的可能。而如果采用现有的检测试块对涡流检测仪器进行标定,标定好的涡流检测仪器可能无法检测出待检测工件内的缺陷,也就是说现有的检测试块无法满足涡流检测仪器的标定要求。The existing workpieces to be inspected are mostly multi-layer metal structures connected by bolts or rivets, and the bolt holes or rivet holes may have defects such as cracks during continuous flight. However, if the eddy current testing instrument is calibrated with the existing test block, the calibrated eddy current testing instrument may not be able to detect the defects in the workpiece to be tested, that is to say, the existing test block cannot meet the calibration requirements of the eddy current testing instrument. .
因而,需要提供一种检测试块,以至少部分地解决上述问题。Therefore, there is a need to provide a test block to at least partially solve the above problems.
实用新型内容Utility model content
本实用新型的主要目的是提供一种检测试块,其能够较为准确地模拟通过连接件来连接的待检测工件,用该检测试块来标定检测仪器,能够使得标定后的检测仪器能够准确地完成对待检测工件的检测。The main purpose of the utility model is to provide a detection test block, which can more accurately simulate the workpiece to be tested connected by the connecting piece, and use the detection test block to calibrate the detection instrument, so that the calibrated detection instrument can accurately Complete the inspection of the workpiece to be inspected.
为此,本实用新型提供一种检测试块,用于对涡流检测仪器进行标定,所述涡流检测仪器用于检测具有安装孔的待检测工件,所述检测试块的材料与所述待检测工件的材料一致,而且所述检测试块上设置有与所述安装孔的尺寸一致的孔,所述孔的开口位于所述检测试块的表面处,且所述孔的延伸方向与所述表面垂直,限定所述孔的壁面上设置有缺陷,所述缺陷与所述待检测工件上的待检测缺陷的形式一致。To this end, the present invention provides a detection test block for calibrating an eddy current detection instrument, the eddy current detection instrument is used to detect a workpiece to be tested with a mounting hole, and the material of the detection test block is the same as that of the to-be-detected workpiece. The material of the workpiece is the same, and the detection test block is provided with a hole with the same size as the installation hole, the opening of the hole is located on the surface of the detection test block, and the extension direction of the hole is the same as that of the installation hole. The surface is vertical, and the walls defining the hole are provided with defects, and the defects are in the same form as the defects to be inspected on the workpiece to be inspected.
根据本方案,检测试块能够模拟待检测工件上的安装孔以及可能存在于安装孔处的缺陷,用这样的检测试块进行标定的涡流检测仪器对工件的检测结果能够更加准确。According to this solution, the test block can simulate the mounting holes on the workpiece to be tested and the defects that may exist in the mounting holes, and the eddy current testing instrument calibrated with such a test block can detect the workpiece more accurately.
在一种实施方式中,所述形式包括尺寸,所述缺陷的尺寸与所述待检测工件的所述安装孔处的最大允许缺陷的尺寸相同。In one embodiment, the form includes a size, and the size of the defect is the same as the size of a maximum allowable defect at the mounting hole of the workpiece to be inspected.
根据本方案,用检测试块标定完成后的涡流检测仪器能够准确地检测到待检测工件的缺陷是否超过允许范围。According to this solution, the eddy current testing instrument after calibration with the test block can accurately detect whether the defect of the workpiece to be tested exceeds the allowable range.
在一种实施方式中,所述孔贯穿所述检测试块。In one embodiment, the hole penetrates the test block.
在一种实施方式中,所述检测试块形成为圆柱体结构,所述孔沿所述圆柱体的轴向方向贯穿所述检测试块。In one embodiment, the test block is formed into a cylindrical structure, and the hole penetrates the test block along the axial direction of the cylinder.
根据上述两种方案,孔能够模拟螺栓孔,而螺栓连接方式是飞行器上常用的连接方式。According to the above two solutions, the holes can simulate bolt holes, and the bolt connection method is a commonly used connection method on aircraft.
在一种实施方式中,所述缺陷关于所述孔的轴向方向对称设置;并且/或者In one embodiment, the defect is arranged symmetrically with respect to the axial direction of the hole; and/or
所述缺陷关于穿过所述孔的中心的径向方向对称设置。The defects are arranged symmetrically with respect to a radial direction passing through the center of the hole.
在一种实施方式中,所述缺陷为两个,两个所述缺陷关于所述孔的轴向方向对称,且在与两个所述缺陷的对称平面垂直的截面内,所述缺陷的形状为三角形。In one embodiment, the number of defects is two, the two defects are symmetrical with respect to the axial direction of the hole, and the shape of the defect is in a cross-section perpendicular to the plane of symmetry of the two defects is a triangle.
在一种实施方式中,所述三角形为直角三角形,且限定所述孔的壁面与所述截面的交线和所述直角三角形的直角边共线。In one embodiment, the triangle is a right-angled triangle, and the intersection of the wall defining the hole and the cross-section is collinear with the right-angled side of the right-angled triangle.
根据上述几种方案,缺陷的设置形式与工件上经常出现的缺陷形式相一致,能够提升检测仪器的标定精度。According to the above solutions, the setting form of defects is consistent with the form of defects that often appear on the workpiece, which can improve the calibration accuracy of the detection instrument.
在一种实施方式中,所述孔的直径为20.5mm或22.5mm。In one embodiment, the diameter of the hole is 20.5mm or 22.5mm.
在一种实施方式中,所述孔为螺栓孔形式的孔。In one embodiment, the holes are holes in the form of bolt holes.
在一种实施方式中,所述缺陷为斜切槽形式的缺陷。In one embodiment, the defect is a defect in the form of a bevel groove.
在一种实施方式中,所述检测试块由铝合金制成。In one embodiment, the test block is made of aluminum alloy.
本实用新型的检验试块,具有对应于待检测工件的装配孔的孔结构,孔结构处设置有用于模拟实际缺陷的缺陷,用该检测试块完成标定的检验设备能够在实际检测时具有较好的检测精度。The inspection test block of the utility model has a hole structure corresponding to the assembly hole of the workpiece to be inspected, and the hole structure is provided with defects for simulating actual defects. good detection accuracy.
附图说明Description of drawings
为了更好地理解本实用新型的上述及其他目的、特征、优点和功能,可以参考附图中所示的优选实施方式。附图中相同的附图标记指代相同的部件。本领域技术人员应该理解,附图旨在示意性地阐明本实用新型的优选实施方式,对本实用新型的范围没有任何限制作用,图中各个部件并非按比例绘制。For a better understanding of the above and other objects, features, advantages and functions of the present invention, reference may be made to the preferred embodiments shown in the accompanying drawings. The same reference numbers in the figures refer to the same parts. It should be understood by those skilled in the art that the accompanying drawings are intended to schematically illustrate the preferred embodiments of the present invention, and have no limiting effect on the scope of the present invention, and the various components in the drawings are not drawn to scale.
图1是根据本实用新型的一个优选实施方式的检测试块的俯视图;Fig. 1 is a top view of a detection test block according to a preferred embodiment of the present invention;
图2是图1中的检测试块沿A-A线截取的截面图;Fig. 2 is the sectional view taken along the A-A line of the detection test block in Fig. 1;
图3是图1中的检测试块沿B-B线截取的截面图。FIG. 3 is a cross-sectional view of the test block in FIG. 1 taken along line B-B.
具体实施方式Detailed ways
现在参考附图,详细描述本实用新型的具体实施方式。这里所描述的仅仅是根据本实用新型的优选实施方式,本领域技术人员可以在所述优选实施方式的基础上想到能够实现本实用新型的其他方式,所述其他方式同样落入本实用新型的范围。Referring now to the accompanying drawings, specific embodiments of the present invention will be described in detail. What is described here is only the preferred embodiment of the present invention, and those skilled in the art can think of other ways to realize the present invention on the basis of the preferred embodiment, and the other ways also fall within the scope of the present invention. scope.
本实用新型提供了一种用于涡流检测的检测试块,用于对涡流检测仪器进行标定,涡流检测仪器用于检测具有安装孔的工件。图1 至图3示出了检测试块的一种优选实施方式。检测试块1可以由各种类型的导电材料制成,但检测试块1的材料需要与待检测工件的材料一致。The utility model provides a detection test block for eddy current detection, which is used for calibrating an eddy current detection instrument, and the eddy current detection instrument is used for detecting workpieces with installation holes. Figures 1 to 3 show a preferred embodiment of the test block. The test block 1 can be made of various types of conductive materials, but the material of the test block 1 needs to be consistent with the material of the workpiece to be tested.
经过与待检测工件的几何特性相比对,检测试块1上被加工出与安装孔的尺寸一致的孔2,限定孔2的壁面3上设置有缺陷4,缺陷4与工件上实际出现或实际可能出现的缺陷一致。该缺陷4可以由诸如电火花或线切割等方式被加工出。After comparing with the geometric characteristics of the workpiece to be tested, a
检测试块1的孔2能够模拟工件的安装孔,因而通过使用检测试块1而完成标定的涡流检测仪器适用于具有安装孔的工件检测,在对这类工件进行实际检测时能够具有较高的准确度。The
优选地,缺陷4的尺寸可以与工件的安装孔处可接受缺陷的最大尺寸相同。这样,在标定完成后,若涡流检测仪器实际检测出较大幅值,则证明工件的安装孔处的缺陷已超出可接受范围。Preferably, the size of the
其中,工件上的安装孔例如可以为螺栓孔,那么检测试块1上的孔2便可被加工为类似于螺栓孔的圆柱形通孔,该圆柱形通孔的直径例如可以为20.5mm或22.5mm。圆柱形的孔2与圆柱体的检测试块1共轴线,即,孔2沿圆柱体的轴向方向D1(见图2)贯穿检测试块1。Wherein, the mounting hole on the workpiece can be, for example, a bolt hole, then the
缺陷4用于模拟工件的安装孔处实际可能产生的缺陷。在本实施方式中,缺陷4为两个且为斜切槽形式,两个缺陷4关于孔2的轴向方向D1对称设置,并且两个缺陷4还关于穿过孔2的中心的径向方向D2也对称地设置。也就是说,两个缺陷4关于检验试块的中心对称地设置。
可以理解,在本实施方式中,两个缺陷4之间的对称平面实际上为图1中的B-B线所截取的平面(即图3所示平面),沿A-A线截取的截面(即图2所示平面)垂直于两个缺陷4的对称平面。在如图2所示的沿A-A线截取的平面内,两个缺陷4的形状为直角三角形。It can be understood that, in this embodiment, the symmetry plane between the two
优选地,两个缺陷4可以彼此不同,以模拟工件的安装孔上可能出现的不同缺陷。Preferably, the two
本实施方式的检测试块1可广泛应用于飞行器的蒙皮和连接接头开孔2处的涡流检测。该检测过程具体可以包括如下步骤:The test block 1 of this embodiment can be widely used in the eddy current test of the skin of the aircraft and the
1、操作人员或操作设备进入飞行器、并靠近待检测工件;1. The operator or operating equipment enters the aircraft and approaches the workpiece to be inspected;
2、对涡流检测仪器进行初始化设定和调整;2. Initialize and adjust the eddy current testing instrument;
3、使用检测试块1对涡流检测仪器进行标定;3. Use the test block 1 to calibrate the eddy current testing instrument;
4、使用标定后的涡流检测仪器来测试工件;4. Use the calibrated eddy current testing instrument to test the workpiece;
5、得出检测结果,其中若涡流检测仪器的幅值大于当涡流检测仪器应用于检测试块1时的幅值,则认定工件存在超标缺陷;5. Obtain the test results, in which if the amplitude of the eddy current testing instrument is greater than the amplitude when the eddy current testing instrument is applied to test the test block 1, it is determined that the workpiece has excessive defects;
6、进行后续处理。6. Perform follow-up processing.
本实用新型的检验试块,具有对应于待检测工件的安装孔的孔2 结构,孔结构处设置有用于模拟实际缺陷的缺陷,因而该检测试块较为接近待检测工件的结构,用该检测试块完成标定的检验设备能够在实际检测时具有较好的检测精度。The inspection test block of the present invention has a
本实用新型的多种实施方式的以上描述出于描述的目的提供给相关领域的一个普通技术人员。不意图将本实用新型排他或局限于单个公开的实施方式。如上所述,以上教导的领域中的普通技术人员将明白本实用新型的多种替代和变型。因此,虽然具体描述了一些替代实施方式,本领域普通技术人员将明白或相对容易地开发其他实施方式。本实用新型旨在包括这里描述的本实用新型的所有替代、改型和变型,以及落入以上描述的本实用新型的精神和范围内的其他实施方式。The foregoing description of various embodiments of the present invention is provided for the purpose of description to one of ordinary skill in the relevant art. It is not intended that the invention be exclusive or limited to a single disclosed embodiment. As described above, various alternatives and modifications to the present invention will be apparent to those of ordinary skill in the art of the above teachings. Thus, while some alternative embodiments have been described in detail, other embodiments will be apparent to or relatively readily developed by those of ordinary skill in the art. This invention is intended to include all alternatives, modifications, and variations of the invention described herein, as well as other embodiments that fall within the spirit and scope of the invention described above.
部件附图标记列表:List of parts reference numbers:
检测试块 1Test block 1
孔 2
限定孔的壁面 3The wall that defines the hole 3
缺陷 4
限定孔的壁面与A-A线截取的截面之间的交线 31Intersection between the wall defining the hole and the section taken by the
轴向方向 D1Axial direction D1
径向方向 D2。Radial direction D2.
Claims (11)
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