STRUCTURAL INTEGRITY SERVICES
INCREASING ENDURANCE AND RELIABILITY IS OUR BUSINESS

Ultrasonic Measurement of Residual Stresses

Ultrasonic Method of Residual Stress Measurement

One of the promising directions in development of non-destructive techniques for residual stress measurement is application of ultrasound. Ultrasonic stress measurement techniques are based on the acoustic-elasticity effect, according to which the velocity of elastic wave propagation in solids is dependent on the mechanical stress. The relationships between the changes of the velocities of longitudinal ultrasonic waves and shear waves of orthogonal polarization under the action of tensile and compressive external loads in steel and aluminum alloys are presented in Figure 1. As can be seen from Fig. 1, the intensity and character of such changes could be different, depending on material properties.

Different configurations of ultrasonic equipment can be used for residual stress measurements. In each case, waves are launched by a transmitting transducer, propagate through a region of the material and are detected by a receiving transducer as shown in Figure 2 [6]. The technique when the same transducer is used for excitation and receiving of ultrasonic waves is often called pulse-echo method (Figure 2a). This method is effective for analysis of residual stresses in the interior of material. In this case the through-thickness average of residual stresses is measured. In the configuration shown in Figure 2c, the residual stress in a surface/subsurface layer is determined.

 

                                             ∆C/C ·10-3
 

 

 

σ, MPa

 

1                                    2                                       3

Figure 1. Change of ultrasonic longitudinal wave velocity (C L) and shear waves velocities

of orthogonal polarization (C SX3; C SX2) depending on the mechanical stress σ in steel A (1), steel B (2) and aluminum alloy (3) [10]:

● - C SX3; ○ - C SX2; x - C L

 

 

 

Figure 2. Schematic view of ultrasonic measurement configurations:

(a) through-thickness pulse-echo, (b) through-thickness pitch-catch and (c) surface pitch-catch

 

The depth of this layer is related to the ultrasonic wavelength, often exceeding a few millimeters, and hence is much greater than that obtained by X-ray method. Other advantages of the ultrasonic technique are the facts that the instrumentation is convenient to use, quickly to set up, portable, inexpensive and free of radiation hazards.

 

In the proposed in [7, 9, 10] technique, the velocities of longitudinal ultrasonic wave and shear waves of orthogonal polarization are measured at a considered point to determine the uni- and biaxial residual stresses. The bulk waves in this approach are used to determine the stresses averaged over the thickness of the investigated elements. Surface waves are used to determine the uni- and biaxial stresses at the surface of the material. The mechanical properties of the material are represented by the proportionality coefficients, which can be calculated or determined experimentally under an external loading of a sample of considered material.

 

In general, the change in the ultrasonic wave velocity in structural materials under mechanical stress amounts only to tenths of a percentage point. Therefore the equipment for practical application of ultrasonic technique for residual stress measurement should be of high resolution, reliable and fully computerized.

 

Ultrasonic Equipment and Software for Residual Stress Measurement

 

Examples of Residual Stress Measurements Using the Ultrasonic Method

 

Specimen for Fatigue Testing

 

Compound Pipes and Pipes with Surfacing

 

Measurement of Residual Stresses in Welded Samples

 

Measurement of Residual Stresses in Welded Structures

 

References

 

 


Ultrasonic Equipment and Software for Residual Stress Measurement UltraMARS

 

The Ultrasonic Computerized Complex (UCC) for residual stress analysis was developed recently based on an improved ultrasonic methodology [7-10]. The UCC includes a measurement unit with supporting software and a laptop with an advanced database and an Expert System (ES) for analysis of the influence of residual stresses on the fatigue life of welded components. The developed device with gages/transducers for ultrasonic residual stress measurement is presented in Figure 3. The UCC allows determining uni- and biaxial applied and residual stresses for a wide range of materials and structures. In addition, the developed ES can be used for calculation of the effect of measured residual stresses on the fatigue life of welded elements, depending on the mechanical properties of the materials, type of welded element, parameters of cyclic loading and other factors.
 
 

 

Figure 3. Using of UltraMARS System for Residual Stress Measurement in Laboratory

 

The developed equipment allows one to determine the magnitudes and signs of uni- and biaxial residual and applied stresses for a wide range of materials as well as stress, strain and force in various size fasteners. The sensors, using quartz plates measuring from 3*3 mm to 10*10 mm as ultrasonic transducers, are attached to the object of investigation by special clamping straps (see Figure 3) and/or electromagnets.

 

The main technical characteristics of the measurement unit:

 

- stress can be measured in materials with thickness 2 - 150 mm;

- weight of unit with sensors: 6 kg

- error of stress determination (from external load): 5 -10 MPa;

- error of residual stress determination: 0.1 sy (yield strength) MPa;

- stress, strain and force measurement in fasteners (pins) 25-1000 mm long;

- independent  power supply (accumulator battery 12 V);

- overall dimensions of measurement device: 300x200x150 mm;

 

The supporting software allows controlling the measurement process, storing the measured and other data and calculating and plotting the distribution of residual stresses. The software also allows an easy connection with standard PC’s.

 

An example of presentation of the residual stress measurement data, using the developed software, is shown in Figure 4. The software allows comparing different data on residual stress measurement and transferring selected data for further fatigue analysis. In Figure 4, the left side of the screen displays information on the measured ultrasonic wave velocities as well as other technical information on the sample. The right side of the screen displays the distribution of calculated residual stresses.

 

In the example of residual stress measurement presented in Figure 4, a plate made from low carbon steel, with yield strength of 296 MPa, was heated locally, with the focal point of heating located approximately 50 mm from the left side of the plate. The distribution of both components of residual stresses in the specimen, as a result of this local heating are shown in the right side of Figure 4. As can be seen, in the heating zone, both residual stress components are tensile and reach the yield strength of the considered material. In the compression zone, located between the edge of the plate and the centre of the heating zone, the longitudinal component of residual stresses reaches minus 140 MPa.

 

 

                                                                                           

                                                                               

 
 

 

             Figure 4. Distribution of residual stresses in a low carbon steel plate

                after local heating [10].

 

 
 
 

Examples of Residual Stress Measurements Using the Ultrasonic Method

 

 

One of the main advantages of the developed technique and equipment is the possibility to measure the residual and applied stresses in samples and real structure elements. Such measurements were performed for a wide range of materials, parts and structures. A few examples of the practical application of the developed technique and equipment for residual stress measurement based on using of the ultrasonic technique are presented below.

 

 

Specimen for Fatigue Testing

 

The residual stresses were measured in a 500x160x3 mm specimen made of an aluminum alloy (σy = 256 MPa, σu = 471 MPa) with a fatigue crack. The residual stresses were induced by local heating at a distance of 30 mm from the centre of the specimen.As can be seen from Figure 5, in the heating zone, both components of the residual stress are tensile. In the compression zones, the longitudinal component of residual stresses reaches minus 130 MPa.

 

 

 

                                                                                                                

                                                                                                      

                                                                                         

 
 

Figure 5. Distribution of residual stresses induced by local heating in a specimen made of an aluminum alloy with a fatigue crack: L – distance from the center of specimen [10]

 

 

Compound Pipes and Pipes with Surfacing

 

 

 

Another example of measuring the residual stresses by ultrasonic method is associated with compound pipes. Compound pipes are used in various applications and they are made by fitting under pressure one pipe with an outer diameter into a pipe with approximately the same inner diameter. For residual stress measurement, rings were cut-off from a number of compound pipes of different diameters. The width of the rings was 16 mm. Residual stresses were measured across the prepared cross-sections in three different locations at 120 degrees to each other with a subsequent averaging of the measurement results. Depending on the differences between the inner diameter D1 of the outer pipe and the outer diameter D2 of the inner pipe, the measurements were made in 3 to 5 points along the radius. The distribution of residual stresses as measured across the wall thickness of the compound pipe is presented in Figure 6.
 
 
 
                                                                                                                               

 
 
 

Figure 6. Residual stress distribution in a compound ring with the following dimensions [10]:

inner ring: D1 = 160mm and D2 = 180mm; outer ring: D1 = 180mm and D2 = 220mm (D1- inner diameter, D2- outer diameter, width of the ring – 16 mm)

 

The results of the residual stress measurement by using ultrasonic method in rings cut-off from the pipes with inner surfacing are presented in Figure 7.

 

 

 

                                                                                                                             

 

                                                                                                      a)                   b)

Figure 7. Residual stress distribution in rings with inner surfacing [10]:

a) ring withD1 = 150mm andD2= 180mm;

  b) ring with D1 = 180mm and D2= 220mm.

(D1- inner diameter, D2- outer diameter, width of the rings - 16 mm)

 

 

 

 

The residual stresses were measured in a specimen measuring 1000x500x36 mm, representing a butt-welded element of a wind tunnel. The distribution of biaxial residual stresses was investigated in X (along the weld) and Y directions after welding and in the process of cyclic loading of the specimen [7]. Figure 8 represents the distribution of longitudinal (along the weld) and transverse components of residual stresses along the weld toe. Both components of the residual stress reached their maximum levels in the central part of the specimen: longitudinal -195 MPa, transverse - 110 MPa.

 

 

 

 

Figure 8. Distribution of longitudinal (along the weld) and transverse

components of residual stresses along the butt weld toe [7]

 

The ultrasonic method was applied also for residual stress measurement in a specimen measuring 900x140x70 mm and made of low-alloyed steel, representing the butt weld of a structure [8]. The distribution of residual stress components in X3 (along the weld) and X2 (perpendicular to the weld) directions as well as through the thickness of the specimen near the weld (X1 direction) are presented on Figure 9.

 

 

Measurement of Residual Stresses in Welded  Structures


 

The developed ultrasonic equipment could be used for RS measurement for both laboratory/factory and field conditions.

 

The residual stresses were measured by the ultrasonic method in large-scale welded panels in as-welded condition and during the fatigue loading of the panels [11]. The objectives of the study were to identify the residual stress distribution and relaxation in specimens with welded longitudinal attachment and welded panel that represent large scale models of ship structural detail, and compare the results of experimental and numerical analyses. During the fatigue testing the residual stresses were measured after 1, 2, 10 and 2010 cycles of loading. Figure 10 shows the process of residual stress measurement after certain number of cycles of loading. Figure 11 illustrates the distributions of the residual stress in large-scale welded panel near the weld that is critical from the fatigue point of view in as-welded condition and after 2010 cycles of loading.
 
 

                                                                

 
                                                                                                                                                                                        B

        

                                                                 

                                 

                                                                         C                                                                                                             D

                            

 Figure 9. Welded specimen (A) and distribution of the residual stresses along the butt weld I-I (B), perpendicular to the weld II-II (C) and through the thickness near the weld III-III (D) [8]: ● – σ22 ; ○ - σ33; ∆- σ11

 

 

Figure 10. Measurement of residual stresses using UltraMARS system

in large-scale welded panel in as-welded condition and during the fatigue loading of the panel

 

 

 

 

 

Figure 11. The distributions of residual stress in large-scale welded panel near the weld

that is critical from the fatigue point of view in as-welded condition

and after 2010 cycles of loading [11]

 

The process and some of the results of ultrasonic measurement of residual stresses in welded elements of a bridge are shown in Figures 12 and 13. The residual stresses were measured by ultrasonic method in the main wall of the bridge span near the end of one of welded vertical attachments. In the vicinity of the weld the measured levels of harmful tensile residual stresses reached 240 MPa. Such high tensile residual stresses are the result of thermo-plastic deformations during the welding process and are one of the main factors leading to the origination and propagation of the fatigue cracks in welded elements.
 
 

 

 

 

 

Figure 12. Installing the ultrasonic gage for residual stress measurement

 
 
 

 

 
 
Figure 13. Distribution of longitudinal (oriented along the weld) residual stresses

near the fillet weld in bridge span: x – distance from the weld toe

 

Based on the ultrasonic method the stresses were measured in the bridge both in conditions of no traffic on the bridge as well as in condition when a few heavy loaded trucks were put in certain locations to determine the total stress.

 

 

Summary

 

1.     Residual stresses play an important role in operating performance of materials, parts and structural elements. Their effect on the engineering properties of materials such as fatigue and fracture, corrosion resistance and dimensional stability can be considerable. The residual stresses, therefore, should be taken into account during design, fatigue assessment and manufacturing of parts and welded elements.

 

2.     Certain progress has been achieved during the past few years in improvement of traditional techniques and development of new methods for residual stress measurement. The developed advanced ultrasonic method, based on it portable instrument and the supporting software can be used for non-destructive measurement of applied and residual stresses in laboratory samples and real parts and structural elements in many applications for a wide range of materials. The developed ultrasonic technique was successfully applied in construction industry, shipbuilding, railway and highway bridges, nuclear reactors, aerospace industry, oil and gas engineering and in other areas during manufacturing, in service inspection and repair of welded element s and structures.

 

References

 

[1]. Handbook on Residual Stress. Volume 1. Edited by Jian Lu. Society for Experimental Mechanics. 2005. 417 p.
 
[2]. V. Trufyakov, P. Mikheev and Y. Kudryavtsev. Fatigue Strength of Welded Structures. Residual Stresses and Improvement Treatments. Harwood Academic Publishers GmbH. London. 1995. 100 p.

 

[3]. Y. Kudryavtsev and J. Kleiman. Fatigue Improvement of Welded Elements and Structures by Ultrasonic Impact Treatment (UIT/UP). International Institute of Welding. IIW Document XIII-2276-09. 2009.

 

[4]. Y. Kudryavtsev. Residual Stress. Springer Handbook on Experimental Solid Mechanics. Springer – SEM. 2008. P. 371-387.

 

[5]. Y. Kudryavtsev and J. Kleiman. Residual Stress Management: Measurement, Fatigue Analysis and Beneficial Redistribution. X International Congress and Exposition on Experimental and Applied Mechanics. Costa Mesa, California USA, June 7-10, 2004. pp. 1-8.
 
[6]. Handbook of Measurement of Residual Stresses. Society for Experimental Mechanics. Edited by J. Lu. 1996. 238 p.

 

[7]. Y. Kudryavtsev. Application of the ultrasonic method for residual stress measurement. Development of fracture toughness requirement for weld joints in steel structures for arctic service. VTT-MET. B-89. Espoo. Finland. 1985. p.62-76.

 

[8]. Y. Kudryavtsev, J. Kleiman and O. Gushcha. Residual Stress Measurement in Welded Elements by Ultrasonic Method. IX International Congress on Experimental Mechanics. Orlando. Florida. USA, June 5-8, 2000. p. 954-957.

 

[9]. Y. Kudryavtsev, J. Kleiman and O. Gushcha. Ultrasonic Measurement of Residual Stresses in Welded Railway Bridge. Structural Materials Technology: An NDT Conference. Atlantic City. NJ. February 28-March 3, 2000. p. 213-218.

 

[10]. Y. Kudryavtsev, J. Kleiman, O. Gushcha, V. Smilenko and V. Brodovy. Ultrasonic Technique and Device for Residual Stress Measurement. X International Congress and Exposition on Experimental and Applied Mechanics. Costa Mesa, California USA, June 7-10, 2004. pp. 1-7.
 
 [11]. H. Polezhayeva, J. Kang, J. Lee, Y. Yang and Y. Kudryavtsev. A Study on Residual Stress Distribution and Relaxation in Welded Components. Proceedings of the 20th International Offshore (Ocean) and Polar Engineering Conference ISOPE-2010, June 20-26, 2010, Beijing, China.
 
 
 

 

 Copyright © 2021 Structural Integrity Services - All Rights Reserved