CN105547544B - Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment - Google Patents

Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment Download PDF

Info

Publication number
CN105547544B
CN105547544B CN201610006387.0A CN201610006387A CN105547544B CN 105547544 B CN105547544 B CN 105547544B CN 201610006387 A CN201610006387 A CN 201610006387A CN 105547544 B CN105547544 B CN 105547544B
Authority
CN
China
Prior art keywords
flat board
measured
region
residual stress
weldment
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.)
Active
Application number
CN201610006387.0A
Other languages
Chinese (zh)
Other versions
CN105547544A (en
Inventor
苟国庆
朱其猛
陈佳
陈辉
朱忠尹
马传平
刘艳
覃超
安江丽
祝鹏飞
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.)
Southwest Jiaotong University
Original Assignee
Southwest Jiaotong University
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 Southwest Jiaotong University filed Critical Southwest Jiaotong University
Priority to CN201610006387.0A priority Critical patent/CN105547544B/en
Publication of CN105547544A publication Critical patent/CN105547544A/en
Application granted granted Critical
Publication of CN105547544B publication Critical patent/CN105547544B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/25Measuring force or stress, in general using wave or particle radiation, e.g. X-rays, microwaves, neutrons
    • G01L1/255Measuring force or stress, in general using wave or particle radiation, e.g. X-rays, microwaves, neutrons using acoustic waves, or acoustic emission

Landscapes

  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • General Physics & Mathematics (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

A kind of ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment, step are as follows:A1, foil gauge is pasted in the region to be measured of flat board weldment, the ultrasonic propagation direction that foil gauge tests the ultrasonic wave residual stress test with that will carry out that should change direction is consistent;A2, application external force make macroscopical out-of-plane deformation of flat board weldment disappear and maintain formation state;A3, the strain value ε that internal strain piece in region to be measured measures is read, calculate region to be measured and eliminate power σ caused by reversible deformationw, σw=E ε, E are modulus of elasticity of the flat board weldment material in strain testing direction;Foil gauge on A4, removing region to be measured, carries out ultrasonic wave residual stress test to region to be measured, obtains residual stress measurement value σc;A5, the power σ according to caused by region to be measured eliminates reversible deformationwWith residual stress measurement value σc, determine actual the residual-stress value σ, σ=σ in flat board weldment region to be measuredc‑σw.This method can significantly improve ultrasonic wave to the residual stress test precision of macroscopical out-of-plane deformation flat board weldment be present.

Description

Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment
Technical field
The present invention relates to a kind of macroscopical facial contour for solving flat board weldment to cause ultrasonic wave-coupled state and propagation path The ultrasonic wave residual stress test method of change, belong to the field of non destructive testing of welding residual stress.
Background technology
Agitating friction weldering is by the use of frictional heat and plastic deformation heat as welding heat source, by a cylinder or other shapes The mixing needle of (such as threaded cylinder) stretches into the seam crossing of workpiece, is rotated by the high speed of soldering tip, makes itself and welding workpiece material Material friction, so that the material temperature rise softening of connecting portion.Agitating friction welding belongs to non-melt welding, have postwelding without Reinforcement, weld defect is less, and appearance of weld is good, and weld strength can reach strength of parent, and it is excellent that welding dissimilar materials etc. can be achieved Point, had a wide range of applications in Aero-Space, rail vehicle, shipbuilding industry etc..Flat part welds the most frequently used mode Welded for single shaft shoulder agitating friction.During single shaft shoulder agitating friction weldering, due to the residual stress shape of flat board weldment top and bottom State differs greatly, and can often cause macroscopical out-of-plane deformation of flat board weldment.Agitating friction welds the lossless of residual stress distribution state Evaluation, deformation is welded to agitating friction and residual stress state control adjustment is significant.
Supercritical ultrasonics technology measurement remnant stress belongs to indirect measurement, and spread speed of the ultrasonic wave in test sample is treated is with treating test sample In residual stress there is acoustic elasticity relation, i.e., ultrasonic wave in the spread speed in treating test sample and treat that the remnants in test sample should Linear relationship is presented in power substantially.According to ultrasonic wave and the relation between test sample residual stress is treated, the remnants that can treat test sample should Power is tested.The most widely used ultrasonic wave is critical refraction longitudinal wave, when longitudinal wave probe is slanted through test at a certain angle During plane, the compressional wave parallel to test plane can be reflected, the compressional wave is referred to as critical refraction longitudinal wave.Critical refraction longitudinal wave is more at present For the residual stress test to flat work pieces, for having more obvious macroscopic deformation face, the i.e. plane with certain curvature Residual stress test, it is primarily present problems with:1st, the voussoir of mounting ultrasonic is unable to good fit with test plane;2nd, it is critical Refracted longitudinal wave can not be propagated along parallel surfaces, and actual propagation path has more notable difference with nominal propagation path.
The content of the invention
It is an object of the invention to provide a kind of ultrasonic wave residual stress test side for macroscopical out-of-plane deformation flat board weldment Method.It is poor in the test plane couple state of weldment that this method can solve mounting ultrasonic voussoir, ultrasonic wave actual propagation path With nominal path difference problem, ultrasonic wave can be significantly improved to the residual stress test of macroscopical out-of-plane deformation flat board weldment be present Precision.
The present invention realizes that its goal of the invention is adopted the technical scheme that:It is a kind of for macroscopical out-of-plane deformation flat board weldment Ultrasonic wave residual stress test method, its step are as follows:
A1, foil gauge is pasted in the region to be measured of flat board weldment, what foil gauge was tested should change direction with that will carry out Ultrasonic wave residual stress test ultrasonic propagation direction it is consistent;
A2, application external force make macroscopical out-of-plane deformation of flat board weldment disappear and maintain formation state;
A3, the strain value ε that internal strain piece in region to be measured measures is read, calculate region to be measured and eliminate power caused by reversible deformation σw, σw=E ε, wherein E are modulus of elasticity of the flat board weldment material in strain testing direction;
Foil gauge on A4, removing region to be measured, ultrasonic wave residual stress test is carried out to region to be measured, obtains flat board weldering The residual stress measurement value σ in region to be measured when part is in formation statec
A5, the power σ according to caused by the A3 regions to be measured for walking to obtain eliminate reversible deformationwIt is residual with the A4 regions to be measured for walking to obtain Residue stress measured value σc, determine actual the residual-stress value σ, σ=σ in flat board weldment region to be measuredcw
Compared with prior art, the beneficial effects of the invention are as follows:
Agitating friction welding differs greatly due to welding the stress state of top and bottom, more obvious macroscopical face easily occurs Outer deformation, form the test surfaces with certain curvature.The couple state of mounting ultrasonic voussoir and test surfaces is produced more bright Aobvious influence, and the test plane that test is formed easily cause the actual propagation distance of ultrasonic wave and nominal distance to exist more Notable difference.The present invention is first to needing the weld signature region (region to be measured) for carrying out ultrasonic wave residual stress to paste strain Piece, macroscopical out-of-plane deformation of flat board weldment is then eliminated by applying external applied load, after eliminating deformation, according to foil gauge measure should Variate determines power caused by elimination reversible deformation, then removes foil gauge and cleans test plane, then with ultrasonic wave to region to be measured Residual stress test is carried out, further according to residual stress test value, the anti-actual stress state for releasing flat board weldment.Above method solution Mounting ultrasonic voussoir of having determined is poor in test plane couple state, ultrasonic wave actual propagation path and nominal path difference problem, Ultrasonic wave is significantly improved to the residual stress test precision of macroscopical out-of-plane deformation flat board weldment be present.
Further, the region to be measured of flat board weldment of the present invention is the welding for needing to carry out ultrasonic wave residual stress test Characteristic area.
Further, the width in the region to be measured of flat board weldment of the present invention is 5-15mm, length 30-70mm.
In this manner it is ensured that flat board weldment each region to be measured with ultrasonic wave residual stress test ultrasonic propagation Region is consistent, that is, eliminates power σ caused by reversible deformationwCorresponding region to be measured and residual stress measurement value σcCorresponding area to be measured Domain is basically identical, so as to ensure the accuracy of the actual residual-stress value in region to be measured finally obtained.
Further, the foil gauge of the present invention pasted in each region to be measured of flat board weldment is no less than 4, step It is the mean strain that all foil gauges measure in region to be measured to read the strain value ε that internal strain piece in region to be measured measures in rapid A3 Value.
The strain value measured by multiple foil gauges calculates mean strain value, it is ensured that calculates region to be measured and eliminates contravariant Power σ caused by shapewAccuracy.
Further, step A2 of the present invention applies external force and macroscopical out-of-plane deformation of flat board weldment is disappeared and remain flat The concrete operations of whole state are:Flat board weldment is put into smooth sample bench, external force is applied by rigid fixture, reduces flat board weldment Due to macroscopical out-of-plane deformation caused by welding, the flatness of flat board weldment is detected by three-coordinates measuring machine, is surveyed according to three coordinates Instrument testing result is measured, rigid fixture is transferred, is wholly absent macroscopical out-of-plane deformation, flat board weldment is in substantially flat shape State.
So, macroscopical out-of-plane deformation in flat board weldment region to be measured can be completely eliminated, be allowed to be in formation state, ensure Obtained region to be measured eliminates power σ caused by reversible deformationwAccuracy, also simultaneously make A4 step carry out ultrasonic wave residual stress test When ultrasonic wave voussoir and weldment test plane between couple state it is good, ensure test accuracy.
Further, the modulus of elasticity of flat board weldment material used in step A3 of the present invention in strain testing direction E measuring method is:According to treating that master plate weldment material processes modulus of elasticity test specimens, and modulus of elasticity test specimens length direction It is consistent with the strain testing direction, the modulus of elasticity of test specimens is measured by stretching demarcation mode.
So, modulus of elasticity of the flat board weldment material in strain testing direction can be accurately tested out, is further ensured that final The accuracy of the obtained actual residual stress of test zone.
The present invention is described in further detail with reference to the accompanying drawings and detailed description.
Brief description of the drawings
Fig. 1 is the flat board weldment section for existing in the embodiment of the present invention after agitating friction weldering is welded macroscopical out-of-plane deformation Schematic diagram.
Fig. 2 is the flat board weldment schematic top plan view that the embodiment of the present invention has divided region to be measured.
Fig. 3 is the test point point that the embodiment of the present invention carries out ultrasonic wave residual stress test to the region to be measured of flat board weldment Cloth schematic diagram.
Fig. 4 is the flat board weldment vertical view signal that step of embodiment of the present invention A1 pastes foil gauge in each region to be measured Figure.
Fig. 5 is that step of embodiment of the present invention A2 applies macroscopical out-of-plane deformation schematic diagram that load eliminates flat board weldment.
Fig. 6 is test point distribution schematic diagram of the embodiment of the present invention by blind hole measuring flat board weldment region to be measured.
Fig. 7 is the residual-stress value comparison diagram that the embodiment of the present invention is measured by distinct methods.
Embodiment
Embodiment
The present invention a kind of embodiment be:A kind of ultrasonic wave of flat board weldment for macroscopical out-of-plane deformation is remaining Stress test method, its step are as follows:
A1, foil gauge is pasted in the region to be measured of flat board weldment, what foil gauge was tested should change direction with that will carry out Ultrasonic wave residual stress test ultrasonic propagation direction it is consistent;
A2, application external force make macroscopical out-of-plane deformation of flat board weldment disappear and maintain formation state;
A3, the strain value ε that internal strain piece in region to be measured measures is read, calculate region to be measured and eliminate power caused by reversible deformation σw, σw=E ε, wherein E are modulus of elasticity of the flat board weldment material in strain testing direction;
Foil gauge on A4, removing region to be measured, ultrasonic wave residual stress test is carried out to region to be measured, obtains flat board weldering The residual stress measurement value σ in region to be measured when part is in formation statec
A5, the power σ according to caused by the A3 regions to be measured for walking to obtain eliminate reversible deformationwIt is residual with the A4 regions to be measured for walking to obtain Residue stress measured value σc, determine actual the residual-stress value σ, σ=σ in flat board weldment region to be measuredcw
The region to be measured of flat board weldment described in this example is the weld signature area for needing to carry out ultrasonic wave residual stress test Domain, the width in region to be measured is 5-15mm, length 30-70mm.
The foil gauge pasted described in this example in each region to be measured of flat board weldment is no less than 4, is read in step A3 The strain value ε for taking internal strain piece in region to be measured to measure is the mean strain value that all foil gauges measure in region to be measured.
Step A2 described in this example, which applies external force, to be made macroscopical out-of-plane deformation of flat board weldment disappear and maintains formation state Concrete operations are:Flat board weldment is put into smooth sample bench, external force is applied by rigid fixture, reduces flat board weldment due to welding Caused macroscopical out-of-plane deformation, the flatness of flat board weldment is detected by three-coordinates measuring machine, is detected according to three-coordinates measuring machine As a result, rigid fixture is transferred, is wholly absent macroscopical out-of-plane deformation, flat board weldment is in substantially flat state.
Flat board weldment material used is in the measurement side of the elastic modulus E in strain testing direction in step A3 described in this example Method is:According to treat master plate weldment material process modulus of elasticity test specimens, and modulus of elasticity test specimens length direction with it is described should It is consistent to become measurement direction, the modulus of elasticity of test specimens is measured by stretching demarcation mode.
In order to prove the measurement accuracy of the inventive method, chosen material is 2219 flat aluminium alloy plate weldments, is stirred Friction welding, there is macroscopical out-of-plane deformation outside more obvious face in parallel bead direction after the completion of welding, as shown in Figure 1.
The part for needing measurement remnant stress of flat board weldment is divided into 36 regions to be measured, as shown in Fig. 2 a is flat The region for needing measurement remnant stress of plate weldment, b are the region to be measured of division.The central point for taking each region to be measured is ultrasound The test point of ripple residual stress test, totally 36, directly carry out ultrasonic wave residual stress test, distribution such as Fig. 3 institutes of test point Show, the result measured is as shown in distributing line K1 in Fig. 7.
According to step A1,4 foil gauges are each pasted in region to be measured in flat board weldment, as shown in figure 4, c is area to be measured The foil gauge pasted in domain.External force is applied by rigid fixture according to step A2, makes flat board weldment due to macroscopical caused by welding Out-of-plane deformation disappears, and flat board weldment is in formation state;Fig. 5 shows to apply macroscopical out-of-plane deformation that external force eliminates flat board weldment Schematic diagram, F1, F2 are the power applied in flat board weldment two edges.According to step A3, calculate each region to be measured and eliminate reversible deformation Caused power.Flat board weldment region surface to be measured is cleaned up according to step A4, to the flat board weldment in formation state Each region to be measured carries out ultrasonic wave residual stress test, the test point of ultrasonic wave residual stress test and above-mentioned is not handled by It is identical to carry out the test point of ultrasonic wave residual stress test, is the central point in each region to be measured.Determined according to step A5 flat The actual residual-stress value in each region to be measured in plate weldment region to be measured, as shown in distributing line K2 in Fig. 7.
External load is discharged, flat board weldment is recovered original initial deformation state, is used for the unified accreditation of industry Damage method of testing Blind Hole Method and residual stress test is carried out to it, as shown in fig. 6, d represents to pass through blind hole measuring flat board weldment The test point of region residual stress to be measured.The result measured is as shown in K3 distributed points in Fig. 7.
As can be seen from Figure 7 the stress test result (K1) of the inventive method is not used generally than using the inventive method Test result (K2) it is big, be compared test, the stress test result of Blind Hole Method using the Blind Hole Method of the unified accreditation of industry (K3) with, more closely, demonstrating the practicality of this method, solving fixed ultrasound using method institute test result (K2) of the present invention Ripple voussoir is poor in test plane couple state, ultrasonic wave actual propagation path and nominal path difference problem, significantly improves super To the residual stress test precision of macroscopical out-of-plane deformation flat board weldment be present in sound wave.

Claims (7)

1. a kind of ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment, its step is as follows:
A1, foil gauge is pasted in the region to be measured of flat board weldment, what foil gauge was tested should change direction and will carry out super The ultrasonic propagation direction of sound wave residual stress test is consistent;
A2, application external force make macroscopical out-of-plane deformation of flat board weldment disappear and maintain formation state;
A3, the strain value ε that internal strain piece in region to be measured measures is read, calculate region to be measured and eliminate power σ caused by reversible deformationw, σw= E ε, wherein E are modulus of elasticity of the flat board weldment material in strain testing direction;
Foil gauge on A4, removing region to be measured, carries out ultrasonic wave residual stress test to region to be measured, obtains at flat board weldment The residual stress measurement value σ in region to be measured when formation statec
A5, the power σ according to caused by the A3 regions to be measured for walking to obtain eliminate reversible deformationwRemnants with the A4 regions to be measured for walking to obtain should Power measured value σc, determine actual the residual-stress value σ, σ=σ in flat board weldment region to be measuredcw
A kind of 2. ultrasonic wave residual stress test side for macroscopical out-of-plane deformation flat board weldment according to claim 1 Method, it is characterised in that:The region to be measured of the flat board weldment is the weld signature area for needing to carry out ultrasonic wave residual stress test Domain.
A kind of 3. ultrasonic wave residual stress test side for macroscopical out-of-plane deformation flat board weldment according to claim 2 Method, it is characterised in that:The width in the region to be measured of the flat board weldment is 5-15mm, length 30-70mm.
A kind of 4. ultrasonic wave residual stress test side for macroscopical out-of-plane deformation flat board weldment according to claim 3 Method, it is characterised in that:The foil gauge pasted in the region to be measured of flat board weldment is no less than 4, reads and treats in step A3 It is the mean strain value that all foil gauges measure in region to be measured to survey the strain value ε that internal strain piece in region measures.
5. surveyed according to a kind of any described ultrasonic wave residual stress for macroscopical out-of-plane deformation flat board weldment of claim 1-4 Method for testing, it is characterised in that:The step A2, which applies external force, to be made macroscopical out-of-plane deformation of flat board weldment disappear and maintains smooth shape The concrete operations of state are:Flat board weldment is put into smooth sample bench, by rigid fixture apply external force, reduce flat board weldment due to Macroscopical out-of-plane deformation caused by welding, the flatness of flat board weldment is detected by three-coordinates measuring machine, according to three-coordinates measuring machine Testing result, rigid fixture is transferred, be wholly absent macroscopical out-of-plane deformation, flat board weldment is in substantially flat state.
6. surveyed according to a kind of any described ultrasonic wave residual stress for macroscopical out-of-plane deformation flat board weldment of claim 1-4 Method for testing, it is characterised in that:The survey of the elastic modulus E of flat board weldment material used in strain testing direction in the step A3 Amount method is:According to treating that master plate weldment material processes modulus of elasticity test specimens, and modulus of elasticity test specimens length direction and institute State that strain testing direction is consistent, the modulus of elasticity of test specimens is measured by stretching demarcation mode.
A kind of 7. ultrasonic wave residual stress test side for macroscopical out-of-plane deformation flat board weldment according to claim 5 Method, it is characterised in that:The measurement side of the elastic modulus E of flat board weldment material used in strain testing direction in the step A3 Method is:According to treat master plate weldment material process modulus of elasticity test specimens, and modulus of elasticity test specimens length direction with it is described should It is consistent to become measurement direction, the modulus of elasticity of test specimens is measured by stretching demarcation mode.
CN201610006387.0A 2016-01-04 2016-01-04 Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment Active CN105547544B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610006387.0A CN105547544B (en) 2016-01-04 2016-01-04 Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610006387.0A CN105547544B (en) 2016-01-04 2016-01-04 Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment

Publications (2)

Publication Number Publication Date
CN105547544A CN105547544A (en) 2016-05-04
CN105547544B true CN105547544B (en) 2018-01-16

Family

ID=55826892

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610006387.0A Active CN105547544B (en) 2016-01-04 2016-01-04 Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment

Country Status (1)

Country Link
CN (1) CN105547544B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109032070B (en) * 2018-07-19 2020-11-03 西南交通大学 Non-contact R-test measuring instrument calibration method adopting eddy current displacement sensor
CN112097972B (en) * 2020-08-12 2022-04-05 佛山方竹科技有限公司 Method for rapidly measuring internal stress of building ceramic plate and application
CN113552061B (en) * 2021-07-21 2024-02-20 安徽理工大学 Ultrasonic welding-cementing composite interface friction coefficient measurement and calculation method

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5984131A (en) * 1982-11-06 1984-05-15 Hitachi Zosen Corp Stress measuring method of structure
CN102879137A (en) * 2012-10-10 2013-01-16 北京理工大学 Flexible fixing device for residual stress detection
CN103017953A (en) * 2011-09-22 2013-04-03 北京理工大学 Device for detecting residual stress close to surfaces of metal materials
CN103808438A (en) * 2014-01-16 2014-05-21 浙江工业大学 Method for measuring sheet welding residual stress
CN104316237A (en) * 2014-11-12 2015-01-28 武汉钢铁(集团)公司 Steel plate surface residual stress detection device and method based on online ultrasonic wave
CN105004789A (en) * 2015-07-13 2015-10-28 四川广正科技有限公司 Error correction method of welding residual stress ultrasonic measurement

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0518833A (en) * 1990-09-19 1993-01-26 Toshiba Corp Residual stress measuring method and lens used for the same

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5984131A (en) * 1982-11-06 1984-05-15 Hitachi Zosen Corp Stress measuring method of structure
CN103017953A (en) * 2011-09-22 2013-04-03 北京理工大学 Device for detecting residual stress close to surfaces of metal materials
CN102879137A (en) * 2012-10-10 2013-01-16 北京理工大学 Flexible fixing device for residual stress detection
CN103808438A (en) * 2014-01-16 2014-05-21 浙江工业大学 Method for measuring sheet welding residual stress
CN104316237A (en) * 2014-11-12 2015-01-28 武汉钢铁(集团)公司 Steel plate surface residual stress detection device and method based on online ultrasonic wave
CN105004789A (en) * 2015-07-13 2015-10-28 四川广正科技有限公司 Error correction method of welding residual stress ultrasonic measurement

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
超声波法曲面工件残余应力测量;马子奇等;《焊接学报》;20111130;第32卷(第11期);全文 *

Also Published As

Publication number Publication date
CN105547544A (en) 2016-05-04

Similar Documents

Publication Publication Date Title
CN102207488B (en) Positioning method of transverse wave TOFD (Time of Flight Diffraction) defect
CN103245729B (en) Detection method and device for internal defects of welding seams
US20200047425A1 (en) Structural Health Monitoring of Curved Composite Structures Using Ultrasonic Guided Waves
CN105547544B (en) Ultrasonic wave residual stress test method for macroscopical out-of-plane deformation flat board weldment
Ling et al. Input electrical impedance as quality monitoring signature for characterizing resistance spot welding
CN104458910A (en) Nondestructive testing method for bonding defects of shell of wind turbine blade and web plate
CN105203635A (en) Surface wave detection method for longitudinal defect on outer surface of small-diameter tube
CN107167273B (en) High-strength bolt connecting node plate compaction degree detection method based on ultrasonic echo
CN104111286B (en) A kind of velocity of wave for the detection of supersonic welding point and thickness calibration steps
CN108918667B (en) Wedge defect detection method
KR20130137109A (en) Industrial robotic device, non-destructive testing of spot welds
Wang et al. Propagation characteristics of ultrasonic weld-guided waves in friction stir welding joint of same material
JP2002048773A (en) Calibration test piece for ultrasonic inspection of rail welded part
JP5865100B2 (en) Defect inspection apparatus and inspection method
CN107941923B (en) Phased array ultrasonic detection capability verification test block group and use method thereof
MORI et al. Influence of steel static strength on fatigue strength of web-gusset welded joints with UIT
CN104914171A (en) Detecting method of far-field near-bottom-surface blind areas of ultrasonic wave normal probes and workpiece processing method for overcoming near-bottom-surface defect of workpiece
CN208902317U (en) A kind of Axle Surface residual stress detection device
CN106383175A (en) Ultrasonic flaw detection test block for blade detection
CN202453330U (en) Pipeline ultrasonic detection reference block
Köhler et al. Characterisation of lateral offsets in clinch points with computed tomography and transient dynamic analysis
Croccolo et al. Adhesive defect density estimation applying the acoustic emission technique
Guagliano et al. An experimental–numerical approach for the analysis of internally cracked railway wheels
CN210321535U (en) Auxiliary detection tool for height detection of designated intersection point
Qiu et al. Experimental Investigation on Adhesive Bonded Joints of Carbon Fiber Composite Laminates Containing Disbond Defect

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant