Pub Date : 2026-01-06DOI: 10.1016/j.msea.2026.149743
Pengpeng Huang, Yizhe Meng, Yake Wu, Feng Jiang, Jun Sun
SiCp-reinforced aluminum matrix composites (AMCs) are promising lightweight structural materials owing to high specific strength, high specific modulus, and excellent wear resistance. However, their application is severely limited by the poor plasticity, which originates mainly from the formation of interfacial brittle Al4C3 and strain incompatibility between the SiC phase and the matrix. Here, we present a novel strategy for tailoring the SiC/Al interface structure in the SiCp/Al-Cu-Mg composites by integrating low-temperature sintering (566 °C) with closed-die hot forging. The designed strategy not only suppresses the formation of Al4C3, but also preserves local porosity adjacent to the SiC particles, enabling the formation of low-strain zones (LSZs) there during subsequent hot forging. As a result, the composites with 5, 10, and 15 wt % SiC all exhibit favorable strength-ductility synergy, where the 5 wt% SiCp/Al-Cu-Mg composite shows a yield strength of 332.0 MPa, an ultimate tensile strength of 458.0 MPa and an elongation of 11.0 %. Without forming the brittle Al4C3 phase, the LSZs further serve to redistribute dislocations, mitigate strain localization and provide more dislocation storage space in the SiC/Al interface zones, thereby alleviating strain incompatibility and reducing stress concentration towards simultaneous property enhancement over the unreinforced alloy. Our work offers an innovative feasible strategy for making high-performance AMCs by tailoring the interfacial structure.
sicp增强铝基复合材料(AMCs)具有高比强度、高比模量和优异的耐磨性,是一种很有前途的轻量化结构材料。然而,塑性差严重限制了它们的应用,这主要源于界面脆性Al4C3的形成以及SiC相与基体之间的应变不相容。在这里,我们提出了一种将低温烧结(566°C)与闭模热锻相结合的方法来定制SiCp/Al- cu - mg复合材料中SiC/Al界面结构的新策略。设计的策略不仅抑制了Al4C3的形成,而且保留了SiC颗粒附近的局部孔隙,从而在随后的热锻过程中形成了低应变区(LSZs)。结果表明,添加5%、10%和15% SiC的复合材料均表现出良好的强度-塑性协同效应,其中5% SiCp/Al-Cu-Mg复合材料的屈服强度为332.0 MPa,极限抗拉强度为458.0 MPa,伸长率为11.0%。在不形成脆性Al4C3相的情况下,LSZs进一步重新分配位错,减轻应变局部化,并在SiC/Al界面区提供更多的位错存储空间,从而减轻应变不相容,减少应力集中,同时提高合金的性能。我们的工作提供了一种创新的可行策略,通过定制界面结构来制造高性能的amc。
{"title":"Achieving strength-ductility synergy in SiCp/Al-Cu-Mg composites via deploying low-strain zones around Al4C3-free interfaces","authors":"Pengpeng Huang, Yizhe Meng, Yake Wu, Feng Jiang, Jun Sun","doi":"10.1016/j.msea.2026.149743","DOIUrl":"10.1016/j.msea.2026.149743","url":null,"abstract":"<div><div>SiC<sub>p</sub>-reinforced aluminum matrix composites (AMCs) are promising lightweight structural materials owing to high specific strength, high specific modulus, and excellent wear resistance. However, their application is severely limited by the poor plasticity, which originates mainly from the formation of interfacial brittle Al<sub>4</sub>C<sub>3</sub> and strain incompatibility between the SiC phase and the matrix. Here, we present a novel strategy for tailoring the SiC/Al interface structure in the SiC<sub>p</sub>/Al-Cu-Mg composites by integrating low-temperature sintering (566 °C) with closed-die hot forging. The designed strategy not only suppresses the formation of Al<sub>4</sub>C<sub>3</sub>, but also preserves local porosity adjacent to the SiC particles, enabling the formation of low-strain zones (LSZs) there during subsequent hot forging. As a result, the composites with 5, 10, and 15 wt % SiC all exhibit favorable strength-ductility synergy, where the 5 wt% SiC<sub>p</sub>/Al-Cu-Mg composite shows a yield strength of 332.0 MPa, an ultimate tensile strength of 458.0 MPa and an elongation of 11.0 %. Without forming the brittle Al<sub>4</sub>C<sub>3</sub> phase, the LSZs further serve to redistribute dislocations, mitigate strain localization and provide more dislocation storage space in the SiC/Al interface zones, thereby alleviating strain incompatibility and reducing stress concentration towards simultaneous property enhancement over the unreinforced alloy. Our work offers an innovative feasible strategy for making high-performance AMCs by tailoring the interfacial structure.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149743"},"PeriodicalIF":7.0,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145922496","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-06DOI: 10.1016/j.msea.2026.149748
Meiyue Tao , Guoliang Li , Boyu Liu , Jia Sun , Jinghan Ma , Jian Liu , Bo Peng , Zhiqiang Cao , Tingju Li , Jinchuan Jie
The solid solution and aging treatments were carried out on Cu-2.85Ni-xTi alloys, and the effects of precipitates on the properties of the alloys with different Ti contents were studied. The microstructure observation was performed on the as-cast and aging samples, the hardness, strength and high temperature properties were investigated to reveal the precipitate strengthening mechanisms. The results show that the microstructure of the as-cast alloys is mainly composed of elliptical disk-like and granular phases except for Cu-2.85Ni. No precipitate is formed in Cu-2.85Ni after aging, while the precipitation phase of Cu-2.85Ni-0.48Ti is mainly rod-like/needle-like and elliptical disk-like. The precipitation phase of Cu-2.85Ni-3.07Ti is similar to that of Cu-2.85Ni-0.48Ti, while rod-like/needle-like phases become larger. Peak aging is achieved after solid solution at 950 °C for 1 h and aging at 500 °C for 2 h. The Cu-2.85Ni-0.48Ti possesses excellent comprehensive performance, with its hardness, conductivity, yield strength, tensile strength, elongation and softening temperature of 153.1 HV, 47.4 % IACS, 227 MPa, 370 MPa, 23.1 %, and 723 °C respectively. The Cu-2.85Ni-0.48Ti alloy has a softening temperature above 720 °C due to the stable Ni3Ti phase and the NiTi phase which maintains semi-coherent relationship with the matrix. However, the formation of lamellar β-Cu4Ti discontinuous precipitates in Cu-2.85Ni-3.07Ti deteriorated the strength and hardness. The Cu-2.85Ni-xTi developed in this work exhibits a significantly higher softening temperature than conventional alloys, making it suitable for demanding high-temperature applications.
{"title":"Microstructure evolution and mechanical properties of high-temperature anti-softening Cu-Ni-Ti alloy","authors":"Meiyue Tao , Guoliang Li , Boyu Liu , Jia Sun , Jinghan Ma , Jian Liu , Bo Peng , Zhiqiang Cao , Tingju Li , Jinchuan Jie","doi":"10.1016/j.msea.2026.149748","DOIUrl":"10.1016/j.msea.2026.149748","url":null,"abstract":"<div><div>The solid solution and aging treatments were carried out on Cu-2.85Ni-xTi alloys, and the effects of precipitates on the properties of the alloys with different Ti contents were studied. The microstructure observation was performed on the as-cast and aging samples, the hardness, strength and high temperature properties were investigated to reveal the precipitate strengthening mechanisms. The results show that the microstructure of the as-cast alloys is mainly composed of elliptical disk-like and granular phases except for Cu-2.85Ni. No precipitate is formed in Cu-2.85Ni after aging, while the precipitation phase of Cu-2.85Ni-0.48Ti is mainly rod-like/needle-like and elliptical disk-like. The precipitation phase of Cu-2.85Ni-3.07Ti is similar to that of Cu-2.85Ni-0.48Ti, while rod-like/needle-like phases become larger. Peak aging is achieved after solid solution at 950 °C for 1 h and aging at 500 °C for 2 h. The Cu-2.85Ni-0.48Ti possesses excellent comprehensive performance, with its hardness, conductivity, yield strength, tensile strength, elongation and softening temperature of 153.1 HV, 47.4 % IACS, 227 MPa, 370 MPa, 23.1 %, and 723 °C respectively. The Cu-2.85Ni-0.48Ti alloy has a softening temperature above 720 °C due to the stable Ni<sub>3</sub>Ti phase and the NiTi phase which maintains semi-coherent relationship with the matrix. However, the formation of lamellar β-Cu<sub>4</sub>Ti discontinuous precipitates in Cu-2.85Ni-3.07Ti deteriorated the strength and hardness. The Cu-2.85Ni-xTi developed in this work exhibits a significantly higher softening temperature than conventional alloys, making it suitable for demanding high-temperature applications.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149748"},"PeriodicalIF":7.0,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145922975","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
In this study, the microstructural evolution and microstructure-property relationships through the thickness of a 100 mm thick, 510 MPa grade heavy steel plate, manufactured by a thermo-mechanical control process, were investigated. The results indicate that the microstructure near the surface of the plate was dominated by granular bainite (GB) and polygonal ferrite (PF), exhibiting a relatively high average dislocation density. In contrast, the microstructure at the quarter-thickness (1/4t) and mid-thickness (1/2t) layers was primarily characterized by GB with low dislocation density. This difference arises from gradients in the cooling rate and strain accumulation through the thickness direction during the rolling process. In addition, results from cyclic load-unload-reload (LUR) tests indicate that the hetero-deformation-induced (HDI) stress increases from the 1/2t layer toward the surface. Specifically, the HDI stress values for the surface sample, 1/4t sample, and 1/2t sample are 387 MPa, 298 MPa and 302 MPa, respectively. This trend is attributed to the dense hetero-pairs formed by the GB and PF phases in the surface microstructure, which promote strong strain partitioning during deformation. The impact energy at −80 °C for surface, 1/4t, and 1/2t are 29 ± 10 J, 131 ± 30 J, and 39 ± 5 J, respectively. The research revealed that a uniform and homogeneous microstructure with an appropriate dislocation density facilitates strain compatibility and enhances damage tolerance, constituting the primary rationale for the enhanced impact toughness at 1/4t layer compared to other layers. Moreover, the surface layer samples exhibit significant anisotropy in impact toughness compared to the 1/4t and 1/2t layers, which can be attributed to differences in their microstructure, texture, and delamination mechanisms. This study elucidates the mechanisms underlying the evolution of microstructure and mechanical performance through the thickness of heavy steel plates, providing valuable insights for designing high-strength, high-toughness heavy steel plates.
{"title":"Through-thickness microstructure and mechanical property variations in a 100 mm ultra-heavy steel plate","authors":"Wei Liu, Yinan Zhang, Xiaoning Xu, Bin Wang, Bingxing Wang, Yong Tian","doi":"10.1016/j.msea.2026.149744","DOIUrl":"10.1016/j.msea.2026.149744","url":null,"abstract":"<div><div>In this study, the microstructural evolution and microstructure-property relationships through the thickness of a 100 mm thick, 510 MPa grade heavy steel plate, manufactured by a thermo-mechanical control process, were investigated. The results indicate that the microstructure near the surface of the plate was dominated by granular bainite (GB) and polygonal ferrite (PF), exhibiting a relatively high average dislocation density. In contrast, the microstructure at the quarter-thickness (1/4t) and mid-thickness (1/2t) layers was primarily characterized by GB with low dislocation density. This difference arises from gradients in the cooling rate and strain accumulation through the thickness direction during the rolling process. In addition, results from cyclic load-unload-reload (LUR) tests indicate that the hetero-deformation-induced (HDI) stress increases from the 1/2t layer toward the surface. Specifically, the HDI stress values for the surface sample, 1/4t sample, and 1/2t sample are 387 MPa, 298 MPa and 302 MPa, respectively. This trend is attributed to the dense hetero-pairs formed by the GB and PF phases in the surface microstructure, which promote strong strain partitioning during deformation. The impact energy at −80 °C for surface, 1/4t, and 1/2t are 29 ± 10 J, 131 ± 30 J, and 39 ± 5 J, respectively. The research revealed that a uniform and homogeneous microstructure with an appropriate dislocation density facilitates strain compatibility and enhances damage tolerance, constituting the primary rationale for the enhanced impact toughness at 1/4t layer compared to other layers. Moreover, the surface layer samples exhibit significant anisotropy in impact toughness compared to the 1/4t and 1/2t layers, which can be attributed to differences in their microstructure, texture, and delamination mechanisms. This study elucidates the mechanisms underlying the evolution of microstructure and mechanical performance through the thickness of heavy steel plates, providing valuable insights for designing high-strength, high-toughness heavy steel plates.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149744"},"PeriodicalIF":7.0,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145922923","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-06DOI: 10.1016/j.msea.2026.149747
Yusha Luo , Qihan Zheng , Bo Sun , Ruixin Sheng , Jinxiong Hou , Zhenzeng Chong , Qianqian Wang , Zhijun Guo , Zhe Jia , Yang Tong , Baolong Shen
FCC-Laves eutectic high-entropy alloys (EHEAs) often exhibit brittleness due to mechanical disparity and incompatible interfaces between the soft FCC and hard Laves lamellae. In this study, we report an aging-driven phase-selective transformation approach to develop coherent interfaces in FCC-Laves EHEAs. After aging for 6 h (AG-6h alloy), the brittle Laves phase transforms into deformable D022 lamellae, converting semi-coherent FCC-Laves interfaces to coherent FCC-D022 boundaries. Simultaneously, coherent L12 precipitates form within the FCC lamellae. This structural evolution leads to doubled compressive plasticity (∼12 %) and elevated strength (∼3000 MPa) compared to the suction-casted alloy. First-principles calculations reveal that the phase-selective transformations of (Ni14Co8Fe1Cr1)(Ta6Cr1Fe1)-D022 and cubical (Co9Ni8Fe5Cr2)(Ta3Cr2Fe3)-L12 precipitates are thermodynamically favorable and enable interfaces coherent with the FCC matrix. The newly formed coherent FCC-D022 and FCC-L12 interfaces promote strain partitioning between adjacent lamellae under high stress. Consequently, the deformation mode changed from planar slips and stacking faults (SFs) in the suction-cast alloy to a coordinated mechanism in AG-6h alloy, involving dislocations with SFs in both FCC and D022 phases, along with deformation twins within the D022 phase. The competition between various deformation micro-mechanism modes is studied by transmission electron microscope and discussed based on generalized stacking fault energy curves. The phase-selective transformation strategy opens new perspectives for designing novel FCC-Laves EHEAs with low-misfit interfaces and high performance.
{"title":"Phase-selective transformation enabled coherent interfaces for coordinated deformation in FCC-Laves eutectic high-entropy alloys","authors":"Yusha Luo , Qihan Zheng , Bo Sun , Ruixin Sheng , Jinxiong Hou , Zhenzeng Chong , Qianqian Wang , Zhijun Guo , Zhe Jia , Yang Tong , Baolong Shen","doi":"10.1016/j.msea.2026.149747","DOIUrl":"10.1016/j.msea.2026.149747","url":null,"abstract":"<div><div>FCC-Laves eutectic high-entropy alloys (EHEAs) often exhibit brittleness due to mechanical disparity and incompatible interfaces between the soft FCC and hard Laves lamellae. In this study, we report an aging-driven phase-selective transformation approach to develop coherent interfaces in FCC-Laves EHEAs. After aging for 6 h (AG-6h alloy), the brittle Laves phase transforms into deformable D0<sub>22</sub> lamellae, converting semi-coherent FCC-Laves interfaces to coherent FCC-D0<sub>22</sub> boundaries. Simultaneously, coherent L1<sub>2</sub> precipitates form within the FCC lamellae. This structural evolution leads to doubled compressive plasticity (∼12 %) and elevated strength (∼3000 MPa) compared to the suction-casted alloy. First-principles calculations reveal that the phase-selective transformations of (Ni<sub>14</sub>Co<sub>8</sub>Fe<sub>1</sub>Cr<sub>1</sub>)(Ta<sub>6</sub>Cr<sub>1</sub>Fe<sub>1</sub>)-D0<sub>22</sub> and cubical (Co<sub>9</sub>Ni<sub>8</sub>Fe<sub>5</sub>Cr<sub>2</sub>)(Ta<sub>3</sub>Cr<sub>2</sub>Fe<sub>3</sub>)-L1<sub>2</sub> precipitates are thermodynamically favorable and enable interfaces coherent with the FCC matrix. The newly formed coherent FCC-D0<sub>22</sub> and FCC-L1<sub>2</sub> interfaces promote strain partitioning between adjacent lamellae under high stress. Consequently, the deformation mode changed from planar slips and stacking faults (SFs) in the suction-cast alloy to a coordinated mechanism in AG-6h alloy, involving dislocations with SFs in both FCC and D0<sub>22</sub> phases, along with deformation twins within the D0<sub>22</sub> phase. The competition between various deformation micro-mechanism modes is studied by transmission electron microscope and discussed based on generalized stacking fault energy curves. The phase-selective transformation strategy opens new perspectives for designing novel FCC-Laves EHEAs with low-misfit interfaces and high performance.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149747"},"PeriodicalIF":7.0,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145922497","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.msea.2026.149742
Peter Benard Oboso , Julia Horioka , Seiya Oyama , Li-Fu Yi , Tetsuhiko Onda , Lili Guo , Shigekazu Morito , Zhong-Chun Chen
Co-free high-entropy alloys (HEAs) are promising, cost-effective candidates for structural applications, but their inherently low strength has hindered widespread industrial adoption. In this study, a series of Cu20Cr10Fe35-0.5xNi35-0.5xTix (x = 0, 2, 6, 8, and 10) HEAs were synthesized through mechanical alloying (MA) and spark plasma sintering (SPS). Microstructural analysis revealed a predominantly FCC-structured matrix with minor secondary phases strongly dependent on Ti content. Alloys with low Ti contents (Ti < 6 at%) contained Cr7C3 phase, while the Ti6 alloy (x = 6) showed TiC and η phases. At higher Ti contents, TiC particles formed alongside η and L12 precipitation phases. Notably, this work demonstrates for the first time that Ti additions can transform detrimental Cr7C3 contamination from milling media into beneficial TiC particles, leading to significant grain refinement. The Ti6 alloy achieved a yield strength (YS) of 683 MPa with 30.0 % elongation, while the Ti8 alloy attained a YS of 1085 MPa and an elongation of 9.5 %. In particular, the Ti8 alloy demonstrates one of the best strength–ductility combinations reported for Cu-rich HEAs, despite the inherent tendency of Cu to segregate and degrade mechanical strength. This exceptional performance is attributed to grain refinement, dispersion strengthening by TiC particles and L12 nanoprecipitates, and a distinctive three-stage work-hardening behavior associated with hierarchical precipitation and deformation twinning. This work presents an effective strategy for overcoming the strength–ductility trade-off in MAed/SPSed Co-free HEAs through Ti alloying.
{"title":"Achieving high strength and good ductility in Co-free CuCrFeNiTi high entropy alloys through controlled titanium addition","authors":"Peter Benard Oboso , Julia Horioka , Seiya Oyama , Li-Fu Yi , Tetsuhiko Onda , Lili Guo , Shigekazu Morito , Zhong-Chun Chen","doi":"10.1016/j.msea.2026.149742","DOIUrl":"10.1016/j.msea.2026.149742","url":null,"abstract":"<div><div>Co-free high-entropy alloys (HEAs) are promising, cost-effective candidates for structural applications, but their inherently low strength has hindered widespread industrial adoption. In this study, a series of Cu<sub>20</sub>Cr<sub>10</sub>Fe<sub>35-0.5x</sub>Ni<sub>35-0.5x</sub>Ti<sub>x</sub> (x = 0, 2, 6, 8, and 10) HEAs were synthesized through mechanical alloying (MA) and spark plasma sintering (SPS). Microstructural analysis revealed a predominantly FCC-structured matrix with minor secondary phases strongly dependent on Ti content. Alloys with low Ti contents (Ti < 6 at%) contained Cr<sub>7</sub>C<sub>3</sub> phase, while the Ti6 alloy (x = 6) showed TiC and η phases. At higher Ti contents, TiC particles formed alongside η and L1<sub>2</sub> precipitation phases. Notably, this work demonstrates for the first time that Ti additions can transform detrimental Cr<sub>7</sub>C<sub>3</sub> contamination from milling media into beneficial TiC particles, leading to significant grain refinement. The Ti6 alloy achieved a yield strength (YS) of 683 MPa with 30.0 % elongation, while the Ti8 alloy attained a YS of 1085 MPa and an elongation of 9.5 %. In particular, the Ti8 alloy demonstrates one of the best strength–ductility combinations reported for Cu-rich HEAs, despite the inherent tendency of Cu to segregate and degrade mechanical strength. This exceptional performance is attributed to grain refinement, dispersion strengthening by TiC particles and L1<sub>2</sub> nanoprecipitates, and a distinctive three-stage work-hardening behavior associated with hierarchical precipitation and deformation twinning. This work presents an effective strategy for overcoming the strength–ductility trade-off in MAed/SPSed Co-free HEAs through Ti alloying.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149742"},"PeriodicalIF":7.0,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145922933","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.msea.2026.149737
Yunpeng Hu , Yi Ru , Yifeng Xing , Boxuan Du , Yang Cao , Tianxu Ji , Yang Song , Hongzhi Su , Ming Gu , Ben Chen , Bin Gan , Shan Li , Wenyue Zhao , Yanling Pei , Shusuo Li , Shengkai Gong , Huibin Xu
Conventional rejuvenation heat treatment (RHT) for crept single-crystal (SX) superalloys generally employs full solution treatment above the γ′-solvus, promoting dynamic annihilation of crystal defects such as dislocations and re-establishment of γ/γ′ dual-phase microstructure. However, not all crystal defects introduced during plastic deformation are deleterious; certain dislocations can enhance the phase-interface stability. This work proposes a sub-solvus solution RHT with the maximum solution temperature slightly below γ′ solvus. For specimens subjected to creep interruption at 760 °C, following sub-solvus solution RHT, the rupture life rejuvenates to several times that of the original standard heat treatment (SHT) state. After the sub-solvus solution RHT, the γ′ precipitates become slightly coarser and show a noticeable deviation in size compared with the original SHT state, while most dislocations and stacking faults within γ′ precipitates are eliminated and the γ/γ′ interfaces contain reorganized interfacial dislocation networks that evolve into a equilibrium configuration. These equilibrium dislocation networks effectively drag mobile dislocations and inhibit shearing of stacking faults into γ′ precipitates, substantially decreasing steady-state creep rate by an order of magnitude. This work gives new insight of rejuvenating the repaired beyond the original and provides an approach of tailoring creep-induced crystal defects during rejuvenation.
{"title":"Sub-solvus solution rejuvenation heat treatment enhances intermediate-temperature creep resistance of superalloys beyond original properties","authors":"Yunpeng Hu , Yi Ru , Yifeng Xing , Boxuan Du , Yang Cao , Tianxu Ji , Yang Song , Hongzhi Su , Ming Gu , Ben Chen , Bin Gan , Shan Li , Wenyue Zhao , Yanling Pei , Shusuo Li , Shengkai Gong , Huibin Xu","doi":"10.1016/j.msea.2026.149737","DOIUrl":"10.1016/j.msea.2026.149737","url":null,"abstract":"<div><div>Conventional rejuvenation heat treatment (RHT) for crept single-crystal (SX) superalloys generally employs full solution treatment above the γ′-solvus, promoting dynamic annihilation of crystal defects such as dislocations and re-establishment of γ/γ′ dual-phase microstructure. However, not all crystal defects introduced during plastic deformation are deleterious; certain dislocations can enhance the phase-interface stability. This work proposes a sub-solvus solution RHT with the maximum solution temperature slightly below γ′ solvus. For specimens subjected to creep interruption at 760 °C, following sub-solvus solution RHT, the rupture life rejuvenates to several times that of the original standard heat treatment (SHT) state. After the sub-solvus solution RHT, the γ′ precipitates become slightly coarser and show a noticeable deviation in size compared with the original SHT state, while most dislocations and stacking faults within γ′ precipitates are eliminated and the γ/γ′ interfaces contain reorganized interfacial dislocation networks that evolve into a equilibrium configuration. These equilibrium dislocation networks effectively drag mobile dislocations and inhibit shearing of stacking faults into γ′ precipitates, substantially decreasing steady-state creep rate by an order of magnitude. This work gives new insight of rejuvenating the repaired beyond the original and provides an approach of tailoring creep-induced crystal defects during rejuvenation.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149737"},"PeriodicalIF":7.0,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145973513","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.msea.2026.149738
Caibo Xie , Yan Jiang , Tao Wu , Litao Chang
Ni-based alloy GH3535 is a key structural material for the molten salt reactors (MSRs), and it is usually processed via traditional cast & wrought routes. In the present study, the feasibility of processing of this alloy via powder metallurgy-hot isostatic pressing (PM-HIPing) has been explored. Pre-alloyed GH3535 powder was produced by gas atomization and consolidated at representative HIPing temperatures. Microstructure and room-temperature tensile properties of the PM-HIPed blocks were characterized using complementary analytical techniques. The results indicated that nearly full dense GH3535 blocks were obtained at all HIPing temperatures. These blocks exhibited uniformly distributed fine carbide particles and equiaxed grains, although size and morphology of the carbide and grain size uniformity varied with HIPing temperature. The sample had ∼60 % of coincidence site lattice (CSL) grain boundaries when it was HIPed at 1140 °C, and the amount of CSL grain boundaries increased to more than 74 % when HIPing was conducted in the range between 1180 °C and 1260 °C. Yield strength and ultimate tensile strength of the PM-HIPed samples decreased while the elongation increased with the increase of HIPing temperature. Furthermore, the samples all featured with dimple ductile dominant fracture mode. The present study not only verified the feasibility of the PM-HIPing process for alloy GH3535 but also provide a foundation for its further optimization.
{"title":"Processing of Ni-based alloy GH3535 with homogeneous and grain boundary engineered microstructure via powder metallurgy-hot isostatic pressing","authors":"Caibo Xie , Yan Jiang , Tao Wu , Litao Chang","doi":"10.1016/j.msea.2026.149738","DOIUrl":"10.1016/j.msea.2026.149738","url":null,"abstract":"<div><div>Ni-based alloy GH3535 is a key structural material for the molten salt reactors (MSRs), and it is usually processed <em>via</em> traditional cast <em>&</em> wrought routes. In the present study, the feasibility of processing of this alloy <em>via</em> powder metallurgy-hot isostatic pressing (PM-HIPing) has been explored. Pre-alloyed GH3535 powder was produced by gas atomization and consolidated at representative HIPing temperatures. Microstructure and room-temperature tensile properties of the PM-HIPed blocks were characterized using complementary analytical techniques. The results indicated that nearly full dense GH3535 blocks were obtained at all HIPing temperatures. These blocks exhibited uniformly distributed fine carbide particles and equiaxed grains, although size and morphology of the carbide and grain size uniformity varied with HIPing temperature. The sample had ∼60 % of coincidence site lattice (CSL) grain boundaries when it was HIPed at 1140 °C, and the amount of CSL grain boundaries increased to more than 74 % when HIPing was conducted in the range between 1180 °C and 1260 °C. Yield strength and ultimate tensile strength of the PM-HIPed samples decreased while the elongation increased with the increase of HIPing temperature. Furthermore, the samples all featured with dimple ductile dominant fracture mode. The present study not only verified the feasibility of the PM-HIPing process for alloy GH3535 but also provide a foundation for its further optimization.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149738"},"PeriodicalIF":7.0,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145973518","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.msea.2026.149741
Markus Domogala , Ondrej Muránsky , Joseph Polden , Ulf Garbe , Maxim Avdeev , Nazli Eslamirad , Zhiyang Wang , Tao Wei , Fernando Valiente Dies , Kim Rasmussen , Anna Paradowska
Wire Arc Additive Manufacturing (WAAM) of 316L stainless steel typically results in columnar grains, high dislocation densities, and residual porosity, which limit toughness compared to conventional material. This study evaluates Hot Isostatic Pressing (HIP) as a post-processing route to refine the microstructure and eliminate defects by investigating four HIP cycles (1000–1200 °C, 100–150 MPa) using EBSD-EDS, neutron diffraction, tomography, and mechanical testing. Increasing HIP temperature and pressure promoted dislocation recovery and recrystallisation while dissolving metastable δ-ferrite; however, processing at 1000 °C induced brittle σ-phase formation, while the 1200 °C/150 MPa cycle (HIP-4) produced a fully recrystallised, chemically homogeneous austenitic structure. HIP-4 reduced porosity by 98.8 % and restored a mechanical response comparable to conventionally processed 316L, characterised by improved ductility and strain-hardening capacity despite a reduction in yield strength. Ultimately, HIP-4 establishes an optimal post-processing window for achieving concurrent densification and microstructural homogenisation, significantly enhancing the mechanical performance and reliability of WAAM 316L components.
{"title":"Influence of post-manufacturing Hot Isostatic Pressing (HIP-ing) on the microstructure and mechanical properties of WAAM 316L stainless steel","authors":"Markus Domogala , Ondrej Muránsky , Joseph Polden , Ulf Garbe , Maxim Avdeev , Nazli Eslamirad , Zhiyang Wang , Tao Wei , Fernando Valiente Dies , Kim Rasmussen , Anna Paradowska","doi":"10.1016/j.msea.2026.149741","DOIUrl":"10.1016/j.msea.2026.149741","url":null,"abstract":"<div><div>Wire Arc Additive Manufacturing (WAAM) of 316L stainless steel typically results in columnar grains, high dislocation densities, and residual porosity, which limit toughness compared to conventional material. This study evaluates Hot Isostatic Pressing (HIP) as a post-processing route to refine the microstructure and eliminate defects by investigating four HIP cycles (1000–1200 °C, 100–150 MPa) using EBSD-EDS, neutron diffraction, tomography, and mechanical testing. Increasing HIP temperature and pressure promoted dislocation recovery and recrystallisation while dissolving metastable δ-ferrite; however, processing at 1000 °C induced brittle σ-phase formation, while the 1200 °C/150 MPa cycle (HIP-4) produced a fully recrystallised, chemically homogeneous austenitic structure. HIP-4 reduced porosity by 98.8 % and restored a mechanical response comparable to conventionally processed 316L, characterised by improved ductility and strain-hardening capacity despite a reduction in yield strength. Ultimately, HIP-4 establishes an optimal post-processing window for achieving concurrent densification and microstructural homogenisation, significantly enhancing the mechanical performance and reliability of WAAM 316L components.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149741"},"PeriodicalIF":7.0,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145973514","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.msea.2026.149739
Yuanhong Qian , Liangxian Gu , Rong Chen , Haiou Yang , Zhiyong Li , Zhaowen Cui
This work systematically investigates the evolution of grain morphology and its effect on the mechanical properties of GH4099 nickel-based superalloy fabricated by laser powder bed fusion (L-PBF) under different heat treatment conditions. By comparing the as-built columnar grains (H1), fully recrystallized equiaxed grains (H2), and their respective precipitation-strengthened states (HA1, HA2), it is revealed that high-temperature homogenization (1160 °C) effectively triggers static recrystallization, significantly improving grain sphericity and structural uniformity, thereby enhancing ductility. Aging treatments promote the precipitation of γ′ phases in large volume fractions, markedly increasing yield strength (HA1: 955 MPa, HA2: 761 MPa), albeit with some reduction in ductility. Cyclic loading–unloading tests demonstrate that highly uniform equiaxed grains with complex grain boundary networks (HA2) substantially improve back-stress uniformity, toughness, and energy dissipation capacity. Through comprehensive microstructural characterization and mechanical analysis, the microstructural control paths for optimizing the strength–ductility balance and service reliability of SLM GH4099 are elucidated, providing theoretical support for process optimization and engineering application of additively manufactured superalloys.
{"title":"Effect of grain morphology on the mechanical properties of GH4099 superalloy fabricated by laser powder bed fusion","authors":"Yuanhong Qian , Liangxian Gu , Rong Chen , Haiou Yang , Zhiyong Li , Zhaowen Cui","doi":"10.1016/j.msea.2026.149739","DOIUrl":"10.1016/j.msea.2026.149739","url":null,"abstract":"<div><div>This work systematically investigates the evolution of grain morphology and its effect on the mechanical properties of GH4099 nickel-based superalloy fabricated by laser powder bed fusion (L-PBF) under different heat treatment conditions. By comparing the as-built columnar grains (H1), fully recrystallized equiaxed grains (H2), and their respective precipitation-strengthened states (HA1, HA2), it is revealed that high-temperature homogenization (1160 °C) effectively triggers static recrystallization, significantly improving grain sphericity and structural uniformity, thereby enhancing ductility. Aging treatments promote the precipitation of γ′ phases in large volume fractions, markedly increasing yield strength (HA1: 955 MPa, HA2: 761 MPa), albeit with some reduction in ductility. Cyclic loading–unloading tests demonstrate that highly uniform equiaxed grains with complex grain boundary networks (HA2) substantially improve back-stress uniformity, toughness, and energy dissipation capacity. Through comprehensive microstructural characterization and mechanical analysis, the microstructural control paths for optimizing the strength–ductility balance and service reliability of SLM GH4099 are elucidated, providing theoretical support for process optimization and engineering application of additively manufactured superalloys.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149739"},"PeriodicalIF":7.0,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145973657","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-03DOI: 10.1016/j.msea.2025.149705
Yafei Wang , Shuangjie Chu , Xing Zhang , Wanting Sun , Qifei Zhang , Qian Liu , Soban Muddassir Dar , Bohao Zhou , Jifeng Sun , Gaofei Liang , Haiyan Zhao , Bo Mao
In this study, the deformation mechanisms and damage evolution behavior in a bimodal Ti-6Al-3Nb-2Zr-1Mo (wt.%) alloy were systematically investigated via the combination of advanced in-situ EBSD analysis of tensile testing and transmission electron microscopy (TEM) observation. The slip trace analysis demonstrates that the early stage of plastic deformation is dominated by the prismatic <a> and basal slip systems, whereas the pyramidal <a> and <c+a> slip systems are gradually activated and become the primary deformation mechanisms at high strain levels. Specifically, the plastic deformation is mainly accommodated by the presence of α phase through the basal and the prismatic slip systems. Besides, the Schmid factors of the basal and prismatic slip systems under the given loading direction are significantly lower than that of the pyramidal slip system, and thereby the pyramidal slip is preferential activated during the plastic deformation. With increasing strain, the lamellar α phase progressively activates the pyramidal <c+a> slip systems to accommodate the imposed strain along the c-axis. TEM observations exhibit the presence of high-density dislocation tangles near twin boundaries, and thus the synergistic interaction between dislocation slip and twining can induce the micro-void nucleation and growth, which is driven by the localized stress concentration. This work elucidates the damage mechanisms dominated by the slip-twinning interactions, which can provide theoretical guidance for strength-ductility optimization in bimodal titanium alloys.
{"title":"In-situ investigation of the slip activities, deformation twinning, and cracking behavior of a bimodal Ti-6Al-3Nb-2Zr-1Mo alloy","authors":"Yafei Wang , Shuangjie Chu , Xing Zhang , Wanting Sun , Qifei Zhang , Qian Liu , Soban Muddassir Dar , Bohao Zhou , Jifeng Sun , Gaofei Liang , Haiyan Zhao , Bo Mao","doi":"10.1016/j.msea.2025.149705","DOIUrl":"10.1016/j.msea.2025.149705","url":null,"abstract":"<div><div>In this study, the deformation mechanisms and damage evolution behavior in a bimodal Ti-6Al-3Nb-2Zr-1Mo (wt.%) alloy were systematically investigated via the combination of advanced in-situ EBSD analysis of tensile testing and transmission electron microscopy (TEM) observation. The slip trace analysis demonstrates that the early stage of plastic deformation is dominated by the prismatic <a> and basal slip systems, whereas the pyramidal <a> and <c+a> slip systems are gradually activated and become the primary deformation mechanisms at high strain levels. Specifically, the plastic deformation is mainly accommodated by the presence of α phase through the basal and the prismatic slip systems. Besides, the Schmid factors of the basal and prismatic slip systems under the given loading direction are significantly lower than that of the pyramidal slip system, and thereby the pyramidal slip is preferential activated during the plastic deformation. With increasing strain, the lamellar α phase progressively activates the pyramidal <c+a> slip systems to accommodate the imposed strain along the c-axis. TEM observations exhibit the presence of high-density dislocation tangles near twin boundaries, and thus the synergistic interaction between dislocation slip and twining can induce the micro-void nucleation and growth, which is driven by the localized stress concentration. This work elucidates the damage mechanisms dominated by the slip-twinning interactions, which can provide theoretical guidance for strength-ductility optimization in bimodal titanium alloys.</div></div>","PeriodicalId":385,"journal":{"name":"Materials Science and Engineering: A","volume":"953 ","pages":"Article 149705"},"PeriodicalIF":7.0,"publicationDate":"2026-01-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145973522","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}