Effect of Cold Working on the Driving Force of the Crack Growth and Crack Growth Rate of Welded Joints under One Overload

To understand the effect of cold working of welding heat-affected zone on the driving force of the crack growth and crack growth rate of stress corrosion cracking (SCC) near the welding fusion line, the finite element simulation method was used to analyze the effect of cold working on the tensile stress of the crack tip at different locations near the fusion line. On this basis, the strain rate of the crack tip in the Ford-Andresen model is replaced by the creep rate of the crack tip, and the creep rate of the crack tip is used as driving force for the crack growth of SCC. )e effect of the cold working level at the heat-affected zone on the driving force of the crack growth and crack growth rate of SCC are analyzed, and driving force of the crack growth and crack growth rate of SCC after one overload was compared.


Introduction
ere are significant differences in mechanical properties of materials on the two sides of the fusion line of welded joints in nuclear power plants. e material composition and organization of the weld area after welding are extremely complex. At the same time, in the process of welding cooling, due to rapid decrease in the temperature of the weld zone, which causes cold shrinkage, it will have a tensile effect on materials in the heat-affected area, and the materials in the heat-affected area will have plastic deformation in different levels under the tensile effect, leading to different levels of cold working in the heat-affected zone [1,2]. Changes of mechanical properties in the heat-affected zone will affect distribution of stress and strain fields at the crack tip in different areas of welded joints, which can affect the driving force of the crack growth and crack growth rate. e SCC crack of welded joints in nuclear power plants is mainly in the weld and heat-affected zone near the fusion line [3]. In the service of material, the phenomenon that load suddenly increases in a short time and exceeds yield stress of the material and then, falls back to normal load is called one overload. One overload will occur due to a sudden increase of load when nuclear power pipelines and pressure vessels in service, for example, sudden increase of load caused by earthquake. Although duration of the one overload process is short, one overload also occurs occasionally in nuclear power plants. One overload will cause mechanical parameters of the microzone at the crack tip of SCC to change, and hardening of the crack tip will occur. One overload will cause mechanical parameters of the microregion at the SCC crack tip to change, and hardening of the crack tip will occur. SCC experiments have found that when loading amplitude changes suddenly or experiment is interrupted and restarted, the SCC crack growth is different [4,5]. erefore, it is of practical engineering significance to study cold working on the SCC driving force of the crack growth and crack growth rate of welded joints in nuclear power plants under one overload. model [6] was proposed to predict the crack growth rate of SCC, which is also widely accepted and applied in the prediction model of SCC crack growth in a nuclear power high temperature water environment. e SCC crack growth rate da/dt can be expressed by where M is the atomic weight, ρ is the density, z is the number of equivalents exchanged, F is Faraday's constant, m is the current attenuation curve exponent, i 0 is the oxidization current density, t 0 is the duration of constant, ε f is the fracture strain of the oxide film at the crack tip, and _ ε ct is the strain rate.
If m≪1 and t f ≫ t 0 , (1) can be simplified to From (2), it can be seen that the strain rate of the crack tip as a single mechanical influencing factor, the strain rate of the crack tip can be regarded as driving force of crack growth, the strain rate of crack tip is large, the driving force of crack growth is large, and the crack growth rate is also large.
SCC crack growth behavior can be regarded as a slow process of oxide film rupture and regeneration under the interaction of mechanics, materials, and corrosive environment at the crack tip. is process is consistent with the creep process. At the same time, the stress at the crack tip is constant for a long period of time, which meets the creep condition of metal. Studies have shown that creep has an important effect on the grain boundary slip at the crack tip. It can be considered that, during crack growth of SCC, rupture of the oxide film is due to grain boundary slippage caused by creep exceeding the rupture strength of the oxide film. erefore, the creep rate of the crack tip instead of the strain rate of the crack tip is used as the driving force for crack growth: Nuclear power structural materials work at high temperature and high pressure, the microregion of the crack tip is a high stress area, and the creep rate usually changes exponentially with stress. erefore, the creep rate of the crack tip is described by the Norton model which is exponential to the stress, as shown in the following equation: where _ ε cr is the creep rate at the crack tip, σ is the stress, R is the creep stress exponent of material, A is the Norton constant of material, R � 3.98, and A � 1.153 × 10 −15 MPa −1 ·h −1 .
According to the Ford-Andresen model, the quantitative prediction model of the SCC crack growth rate can be expressed as κ a can be calculated by the values of standard electrochemical and material parameters [7], and κ a � 8.643 × 10 −4 .

Geometric Model.
Taking welded joints in nuclear power plants as the research object, in finite element analysis of the driving force of the crack growth and crack growth rate of stress corrosion cracking (SCC), compact tensile specimen (1T-CT) is used, and the geometric dimension of the specimen is shown in Figure 1. e initial precrack length a � 2 mm. During the SCC process, a dense oxide film is formed at the crack tip of 316L SS. e thickness of the oxide film varies according to the corrosion environment. e thickness of the oxide film is generally 0.1 μm∼2 μm [8]. In the study, the geometric model of the oxide film at the crack tip of SCC is simplified as shown in Figure 1, and the thickness of the oxide film is 0.5 μm.
According to the location of the SCC crack in welded joints in nuclear power plants, SCC cracks are easily generated in the heat-affected zone and the fusion line, and cold working at heat effects can occur due to the welding process. e distribution of cracks in different positions of welded joint is shown in Figure 1. When a crack initiates at the interface, the crack coincided with fusion line, and two sides of the crack are nickel-based 600 and 316L SS. When a crack initiates in the heat-affected zone, the distance d between the crack and fusion line is 5 μm and 15 μm, respectively.

Mechanical Model.
e structure material for nuclear power pipelines is 316L SS, and material for welds is nickelbased 600. Both are power hardening materials. erefore, the Ramberg-Osgood (R-O) relationship is selected as the constitutive equation.
e heat-affected zone of the welded joint has a different level of cold working due to cold shrinkage of the weld. To simulate the different level of cold working in the heat-affected zone, tensile experiments were used to 316L SS by 10% and 20%, respectively, to obtain mechanical parameters of material with a different level of cold working. Young's modulus of the oxide film is about 70% of metal material's [9]. erefore, Young's modulus of the oxide film at the crack tip is 140 GPa, and the Poisson ratio of the oxide film is 0.3. In experiment, stress intensity factor K I � 30 MPa·m 1/2 [10]. It is assumed that nickel-based 600 and 316L SS have the same creep parameters. e mechanical parameters of materials are shown in Table 1.

Finite Element Model.
Using the numerical simulation method, the finite element model is as shown in Figure 2. e plane strain model is adopted in finite element analysis because the crack in the nuclear power pipeline conforms to the plane strain model. e crack tip adopts a circular arc shape. e submodel technology is used to refine the crack tip to obtain more accurate simulation data. Both the global model and submodel use an 8-node quadratic plane strain element (CPE8). e discrepancy of material properties in the finite element model is marked in Figure 1

Analysis of Tensile Stress at the Crack Tip
One overload occurs in service, and the microregion at the crack tip will harden. e hardening of the microregion at the crack tip will affect the distribution of stress field at the crack tip. e tensile stress direction is consistent with the external load direction, and it is perpendicular to the crack opening direction, which can truly reflect stress at the crack tip. erefore, distribution of tensile stress at the crack tip is mainly analyzed. When SCC crack is on the fusion line, tensile stress at the crack tip with and without hardening is as shown in Figure 3. It can be seen from the figure that tensile stress at the crack tip with hardening is greater. Because the material in the microregion at the crack tip is hardened and plasticity becomes worse, it is not easy to deform and release stress. e mechanical properties of the two sides of the crack are different, and the distribution of tensile stress is also asymmetric. Cold working is generated due to cold shrinkage of the heat-affected zone. e effect of cold working of 316L SS in the heat-affected zone on tensile stress at the crack tip on the fusion line is shown in Figure 4. It can be seen from the figure that the higher the cold working level of 316L SS in the    heat-affected zone, the greater the tensile stress at the crack tip, and tensile stress is more and more biased to the 316L SS side as the cold working level of 316L SS increases. Tensile stress is more and more concentrated on the side with higher level of cold working because the metal with higher level of cold working is less plastic and less prone to deformation. When the crack is in the heat-affected zone, the effect of cold working of material in the heat-affected zone on tensile stress is as shown in Figure 5. It can be seen that when d � 5 μm and d � 15 μm, and there is no cold working in the heat-affected zone, the yield strength and hardening exponent of 600 alloy are higher than that of 316L SS, and so tensile stress shifts toward the 600 alloy. As the level of cold working in the heat-affected zone increases, the tensile stress at the crack tip shifts toward 316L SS. Because the level of cold working of 316L SS is higher than that of nickel-based alloys, it can be seen that tensile stress will shift to the side where the material is at high level of cold working. When the level of cold working is higher, tensile stress is also relatively greater. Comparing the distribution tensile stress at the crack tip with d � 5 μm and d � 15 μm, it can be seen that when the crack tip is closer to the weld, the tensile stress at the crack tip is greatly affected by mechanical parameters of 600 alloy. As d increases, the crack tip gradually moves away from weld, and tensile stress at the crack tip is greatly affected by the mechanical properties of 316L SS in the heat-affected zone. tip. When external load is constant and the crack tip is hardened, the plasticity of the crack tip decreases and the stress of the crack tip increases. On the other hand, due to the restraint of the crack tip, hardening of the crack tip will generate residual compressive stress at the crack tip. erefore, only considering hardening of the crack tip without considering the residual stress, when the crack tip is hardened, the tensile stress is greater. When the hardening at the crack tip and residual stress are considered at the same time, the effective stress at the crack tip should be the combination of tensile stress and residual stress. e effective stress is used in the calculation of the driving force and crack growth rate. When the crack occurs on the fusion line, the 0°-90°area of the crack tip belongs to the weld area, and the material is nickel-based 600 and the 90°-180°area belongs to the heat-affected area, and material is 316L SS. To study the distribution of the creep rate at different distances from crack tips, three paths from the crack tip, r � 0 μm, r � 0.2 μm, and r � 0.4 μm, were chosen and analyzed.

Effect of Cold
When the crack tip is not hardened and the heat-affected zone is not cold-worked, the creep rate at the crack tip is as shown in Figure 6. It can be seen from the figure that the closer to the crack tip, the greater the creep rate of crack tip and the greater the driving force for crack growth. e value and distribution of the creep rate at the crack tip are affected by mechanical properties of the weld and heat-affected zone. e yield strength and hardening exponent of the nickelbased 600 in the weld zone are higher than those of 316L SS in the heat-affected zone, and the maximum value of the creep rate at the crack tip is biased toward the weld material.
When the crack tip is hardened and the heat-affected zone is not cold-worked, the distribution of the creep rate at the crack tip is as shown in Figure 7. It can be seen from the figure that the closer to the crack tip, the higher the creep rate. e maximum value of the creep rate at the crack tip did not appear at 90°in front of the crack tip, but was biased towards the weld zone. e distribution of the creep rate at the crack tip with and without hardening is shown in Figure 8. It can be seen that the creep rate at the crack tip with hardening is smaller. is is because although the hardening at the crack tip increases tensile stress, it also generates residual compressive stress. e residual compressive stress needs to be overcome when reloading, which will temporarily reduce the stress at the crack tip. e effect of cold working on the creep rate at the crack tip is shown in Figure 9. It can be seen from the figure that the value of the maximum creep rate appears in weld when there is no cold working in the heat-affected zone. As the level of cold working in the heat-affected zone increases, the maximum value of the creep rate will shift. When the mechanical properties of material in the heat-affected zone are higher than those of the material in the weld zone, the maximum value of the creep rate appears in the heat-affected zone, and the maximum value of creep rate increases. As the level of cold working in the heat-affected zone further increases, the maximum value of the creep rate also increases rapidly, and the maximum value of the creep rate is still in the heat-affected zone. erefore, the creep rate tends to be on the side of the material with higher level of cold working.

Effect of Cold Working on the Driving Force of Crack Growth in the Heat-Affected Zone.
e creep rate at the crack tip of cold working 316L SS in the heat-affected zone is Advances in Materials Science and Engineering shown in Figure 10 when the crack is in the heat-affected zone. It can be seen that the higher the level of cold working, the greater the creep rate and the greater the driving force for crack growth. e maximum value of the creep rate is gradually away from the weld zone, and the maximum value of the creep rate increases rapidly. at is, the higher the level of cold working, the greater the driving force for crack growth.
e distribution of the creep rate at the crack tip is shown in Figure 11 when the distance between the fusion line and crack tip is different. It can be seen from the figure that the crack is closer to the weld fusion line, the creep rate is greatly affected by the weld material, and the maximum value of the creep rate is also biased toward the weld zone. When the crack is far away from the weld, the creep rate is mainly affected by mechanical parameters of 316L SS in the heat-affected zone, and the effect of mechanical properties in weld gradually decreases.

Effect of Cold Working on the Crack
Growth Rate e effect of cold working of 316L SS in the heat-affected zone on the crack growth rate is shown in Figure 12 when the crack is on the fusion line of the weld. It can be seen from the figure that with the higher level of cold working of 316L SS in the heat-affected zone, the maximum value of the crack growth rate is gradually transferred from the weld to the heat-affected zone. e maximum value of the crack growth rate is biased toward the side of metal with higher levels of cold working. e higher level of cold working in  the heat-affected zone, the greater the crack growth rate, and the crack growth rate increases rapidly with the increase of the level of cold working. e cold working of material increases the crack growth rate of SCC, which is an unfavorable factor. Figure 13 shows the comparison of the crack growth rate at the crack tip with hardening and without hardening when the crack is on the fusion line. It can be seen from the figure that the crack growth rate is smaller when the crack tip is hardened, and the hardening at the crack tip has a greater effect on the crack growth rate. e crack tip with hardening reduces the crack growth rate within a certain range, which may be a favorable factor.
When crack appears in the heat-affected zone at a distance d � 5 μm from the fusion line, the effect of cold working in the heat-affected zone on the crack growth rate is as shown in Figure 14. It can be seen that as the level of cold working of 316L SS in heat-affected zone increases, the maximum value of the crack growth rate gradually moves away from the weld zone. e higher the level of cold working of 316L SS, the greater the crack growth rate. It can be seen that cold working of material increases the crack growth rate. Figure 15 compares the crack growth rate in the heataffected zone when the distance between the crack and fusion line is different. It can be seen from the figure that the greater the distance between the crack tip and fusion line, the greater the crack growth rate. is is because mechanical properties of the metal in the heat-affected zone are higher than those of the weld metal. At this time, the crack growth rate is greatly affected by the mechanical properties of the metal in the heat-affected zone.
Crack growth rate da/dt (mm/s) Figure 13: Comparison of the crack growth rate between the crack tip with and without hardening.

Conclusions
(1) Using the creep rate of the crack tip to replace the strain rate of the crack tip in the Ford-Andresen model, the driving force of the crack growth and crack growth rate calculation models are optimized, which is more convenient for practical application. (2) e mechanical properties of the metal on both sides of the fusion line are different, and the tensile stress is different. e tensile stress will be biased toward the side of metal with a higher level of cold working. As the level of cold working in the heat-affected zone increases, tensile stress is obviously biased towards the heat-affected zone, and the tensile stress increases as the level of cold working increases.
(3) Both the driving force of the crack growth and crack growth rate increase with the level of cold working of material in the heat-affected zone, and the maximum value of the crack growth driving force and crack growth rate are biased toward the side of the metal with a high level of cold working. e farther the crack tip is from the fusion line, the smaller the effect of the crack growth driving force and crack growth rate on mechanical properties of weld metal, and the greater the effect on mechanical properties of metal in the heat-affected zone. (4) One overload will cause the crack tip of SCC to harden. e hardening of the crack tip not only increases the tensile stress to a certain extent but also generates residual compressive stress. erefore, the driving force of the crack growth and crack growth rate is reduced to a certain extent.

Data Availability
1. Previously reported Young's modulus and Poisson's ratio of the oxide film were used to support this study and are available at https://doi.org/10.1016/S00406090(01)01464-X. ese prior studies (and datasets) are cited at relevant places within the text as references [9]. 2. Mechanical parameters of nickel-based alloy 600 were used to support this study and are available at https://doi.org/10.1016/j.ijpvp.2019.04.005. ese prior studies (and datasets) are cited at relevant places within the text as references [11]. 3. e data of mechanical parameters of 316L SS with a different level of cold working are obtained by the research group through the tensile test. 4. e numerical simulation data at the crack tip of 316L stainless steel used to support the findings of this study are included in the article.

Conflicts of Interest
e authors declare that they have no conflicts of interest.  Advances in Materials Science and Engineering