Pub Date : 2024-08-11DOI: 10.1007/s11661-024-07547-w
Laxya Gupta, Nachiket Keskar, Bikas C. Maji, R. N. Singh, Madangopal Krishnan
Triple-layer stainless-steel clad plate having 317L stainless steel (SS317L) as cladding layer and ASTM SA516 GR60 (GR60) as backing layer was successfully fabricated through vacuum hot roll bonding (VHRB) at 1373 K (1100 °C) temperature and strain rate regime of 1–5 s−1, which were identified through process efficiency maps of the base materials (SS317L and GR60). The process efficiency maps were constructed by conducting isothermal compression tests within the temperature range of 1173 K (900 °C)–1473 K (1200 °C) and 0.1–50 s−1strain rate regime. Effect of post-rolling heat treatments on the mechanical properties of clad plate was studied after solutionization at 1173 K (900 °C) for 1 h followed by cooling at different rates, i.e., water quenching, air cooling, and furnace cooling. As compared to other post-rolling heat treatments, the ultimate tensile strength, uniform plastic elongation, and maximum shear strength showed a significant change from 524 MPa, 0.46 and 519 MPa to 652 MPa, 0.36 and 410 MPa, when the normalized clad plate was solutionized at 1173 K (900 °C) and water quenched. A drastic change in shear fracture mode from gradual failure in normalized condition to catastrophic failure was also noticed after water quenching. These changes are essentially manifestation of the microstructural change in GR60 layer which led to the change in mechanical properties.
{"title":"Effect of Heat Treatments on the Microstructure and Mechanical Properties of SS317L/ASTM SA516 GR60 Steel Clad Plate Fabricated Through Hot Roll Bonding","authors":"Laxya Gupta, Nachiket Keskar, Bikas C. Maji, R. N. Singh, Madangopal Krishnan","doi":"10.1007/s11661-024-07547-w","DOIUrl":"https://doi.org/10.1007/s11661-024-07547-w","url":null,"abstract":"<p>Triple-layer stainless-steel clad plate having 317L stainless steel (SS317L) as cladding layer and ASTM SA516 GR60 (GR60) as backing layer was successfully fabricated through vacuum hot roll bonding (VHRB) at 1373 K (1100 °C) temperature and strain rate regime of 1–5 s<sup>−1</sup>, which were identified through process efficiency maps of the base materials (SS317L and GR60). The process efficiency maps were constructed by conducting isothermal compression tests within the temperature range of 1173 K (900 °C)–1473 K (1200 °C) and 0.1–50 s<sup>−1</sup>strain rate regime. Effect of post-rolling heat treatments on the mechanical properties of clad plate was studied after solutionization at 1173 K (900 °C) for 1 h followed by cooling at different rates, <i>i.e.</i>, water quenching, air cooling, and furnace cooling. As compared to other post-rolling heat treatments, the ultimate tensile strength, uniform plastic elongation, and maximum shear strength showed a significant change from 524 MPa, 0.46 and 519 MPa to 652 MPa, 0.36 and 410 MPa, when the normalized clad plate was solutionized at 1173 K (900 °C) and water quenched. A drastic change in shear fracture mode from gradual failure in normalized condition to catastrophic failure was also noticed after water quenching. These changes are essentially manifestation of the microstructural change in GR60 layer which led to the change in mechanical properties.</p>","PeriodicalId":18504,"journal":{"name":"Metallurgical and Materials Transactions A","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141948502","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Circumferential near-neutral pH corrosion fatigue (C-NNpH-CF) is the result of the simultaneous impact of axial residual and applied stresses along with the near-neutral pH corrosive environment established on the external surface of the buried pipeline because of leakage through the protective coating. (This mechanism has previously been referred to as near-neutral pH stress corrosion cracking.) Since integrity management measures should be implemented before Stage III (rapid crack propagation to rupture), this study aims to evaluate the effect of bending residual stress (a suitable source of axial residual stress) and cyclic loading (simulated pipeline pressure fluctuations) on crack growth at Stage II. Based on the digital image correlation (DIC) method, the final stress distribution in length and thickness direction was used to analyze crack growth in various test parameters, including applied cyclic loading, initial notch depth/position, and bending angle/direction. As a result of stress gradients in the depth direction of bent pipelines, a new method was developed to obtain the stress intensity factor. A comparison of crack growth rates between circumferentially oriented and longitudinally oriented NNpH-CF was performed to reveal the growth mechanism. Crack growth was maximum at 1 mm depth initial notch, 20 deg bend (inward), and 50 pct cycling load.
{"title":"Pipeline Circumferential Cracking in Near-Neutral pH Environment Under the Influence of Residual Stress: Crack Growth","authors":"Hamed Shirazi, Shidong Wang, Reg Eadie, Weixing Chen","doi":"10.1007/s11661-024-07542-1","DOIUrl":"https://doi.org/10.1007/s11661-024-07542-1","url":null,"abstract":"<p>Circumferential near-neutral pH corrosion fatigue (C-NNpH-CF) is the result of the simultaneous impact of axial residual and applied stresses along with the near-neutral pH corrosive environment established on the external surface of the buried pipeline because of leakage through the protective coating. (This mechanism has previously been referred to as near-neutral pH stress corrosion cracking.) Since integrity management measures should be implemented before Stage III (rapid crack propagation to rupture), this study aims to evaluate the effect of bending residual stress (a suitable source of axial residual stress) and cyclic loading (simulated pipeline pressure fluctuations) on crack growth at Stage II. Based on the digital image correlation (DIC) method, the final stress distribution in length and thickness direction was used to analyze crack growth in various test parameters, including applied cyclic loading, initial notch depth/position, and bending angle/direction. As a result of stress gradients in the depth direction of bent pipelines, a new method was developed to obtain the stress intensity factor. A comparison of crack growth rates between circumferentially oriented and longitudinally oriented NNpH-CF was performed to reveal the growth mechanism. Crack growth was maximum at 1 mm depth initial notch, 20 deg bend (inward), and 50 pct cycling load.</p>","PeriodicalId":18504,"journal":{"name":"Metallurgical and Materials Transactions A","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2024-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141948647","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2024-08-07DOI: 10.1007/s11661-024-07525-2
Samar Mandal, Arjun Mahato, Zafir Alam, Shibayan Roy
In the present study, 3D non-woven needle-punched preform (NPP) Cf–SiCm composite with 7.5 pct volume fraction of carbon fiber is prepared via liquid silicon infiltration technique and characterized for microstructure, phase formation and mechanical behaviors. Additionally, the composite is subjected to plasma arc jet tests for evaluation of ablation resistance under ultra-high temperature oxidation environment. The dense composite (density ~ 2.5 to 2.6 g/cm3) contains β-SiC phase due to the reaction between infiltrated molten silicon and carbon matrix surrounding the carbon fibers. The resultant Cf–SiCm composite shows high hardness and high abrasion resistance due to a higher proportion of hard SiC matrix as well as exhibits various toughening mechanisms from the carbon fiber reinforcement causing a delay in fracture. It also contains excellent resistance to thermal shock and thermo-oxidative erosion resistance during plasma arc jet ablation test without any visible crack or damage on the exposed surface.