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10 February 2026, Volume 18 Issue 2
    

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    Process Technology in the Ordnance Industry
  • HUANG Mengjiao, XING Zhihui, CAO Kai, XU Chao, DU Chuanhang, SUN Jipeng, ZHAO Gaozhan, MENG Zhenyu
    Journal of Netshape Forming Engineering. 2026, 18(2): 1-9. https://doi.org/10.3969/j.issn.1674-6457.2026.02.001
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    The work aims to study the effect of different magnetic field frequencies on microstructures and properties of Al/steel bimetal interface to achieve high-quality metallurgical bonding of Al/steel interface. The Al/steel bimetal was prepared by magnetic field assisted liquid-solid composite casting process. The microstructure, phase composition and fracture layer morphology of the interface were analyzed by scanning electron microscope, energy dispersive spectroscopy and optical microscopy. The interface shear strength was tested by universal test machine. The introduction of the magnetic field did not change the phase composition of Al/steel bimetal interface. The reaction layer was mainly composed of Al5Fe2, Al13Fe4, τ1-Al2Fe3Si3 and τ5-Al8Fe2Si phases. With the increase of the magnetic field frequency (1, 3, 6, 9 Hz), the morphology of the reaction layer near the aluminum side was dentiform, necking, dentate and continuous dentate. The thickness of the reaction layer decreased first and then tended to be stable, from 9.21 μm without magnetic field to 6.24 μm at 9 Hz. The interface shear strength exhibited an initial increase followed by a decrease with the increasing magnetic field frequency, reaching the maximum of 39.20 MPa at the frequency of 3 Hz, which was 83.8% higher than that without magnetic field. Thus, the introduction of magnetic field in the liquid-solid composite casting process can effectively improve the microstructure of Al/steel bimetal interface and significantly enhance the interfacial bonding property.
  • MENG Yi, XIANG Jin, LIU Yan
    Journal of Netshape Forming Engineering. 2026, 18(2): 10-20. https://doi.org/10.3969/j.issn.1674-6457.2026.02.002
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    The work aims to clarify the role of extrusion in regulating the subsequent hot deformation behavior and plastic forming performance of spray formed 7055 aluminum alloy, to provide a basis for optimizing the composite forming process path. Isothermal compression tests were conducted with a Gleeble thermal simulator on both as-sprayed and extruded 7055 aluminum alloy. The flow stress characteristics, dynamic recrystallization behavior, and hot processing performance at both states were systematically compared. Constitutive equations based on the Arrhenius-type hyperbolic sine model were established, and processing maps were constructed. The results indicated that the extrusion markedly improved the hot deformation behavior of the alloy. The hot deformation activation energy of the extruded alloy decreased by 16.9%, and the average peak stress was reduced by 8.5% compared with those of as-sprayed alloy. At 425 ℃ and 0.01 s-1, the recrystallization fraction reached 59.5%, which was 15.2% higher than that of the as-sprayed alloy. Processing maps showed that the extruded alloy exhibited a wider safe processing window (η>0.34) with enhanced deformation stability. Extrusion optimizes the initial microstructure through porosity elimination, grain refinement, and second-phase homogenization, thereby reducing deformation resistance and promoting dynamic recrystallization during subsequent hot deformation.
  • DONG Yangping, ZHAO Shuming, ZHU Jinyu, ZHANG Huihua, ZHAO Wentian, MA Guonan, ZHUANG Xinpeng, SUN Yulin, YANG Pengwei, ZHANG Qun, FAN Ziyu, ZHONG Liang, YANG Guang, LU Renyi, CAO Lei, MA Zhiyuan, WANG Feng
    Journal of Netshape Forming Engineering. 2026, 18(2): 21-30. https://doi.org/10.3969/j.issn.1674-6457.2026.02.003
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    Since the Ti6Al4V alloy exhibits insufficient mechanical properties during the laser powder bed fusion (PBF-LB) process, the work aims to introduce the rare earth oxide Y2O3 to improve its properties. The Ti6Al4V composite powder with different Y2O3 contents was prepared by mechanical ball milling, and the alloy pieces were formed by PBF-LB technology. The microstructure, phase composition and element distribution of the composite powder and the formed alloy were systematically analyzed through scanning electron microscopy, X-ray diffraction, electron backscatter diffraction and transmission electron microscopy. The mechanical properties were evaluated through room temperature tensile tests, and the fracture mechanism was investigated by fracture analysis. Y2O3 uniformly adhered to the surface of the Ti6Al4V powder after ball milling. During the PBF-LB forming process, the Y2O3 significantly refined the original β grains and the size of α/α' martensite, and dispersed in the matrix in a nanoscale form, forming a semi-continuous relationship with the α-Ti matrix. When the mass fraction of Y2O3 was 0.2%, the tensile strength and yield strength of the alloy increased to 1 331 MPa and 1 208 MPa respectively. However, when the mass fraction of Y2O3 increased to 0.3%, the plasticity decreased. The fracture morphology changed from a ductile crack pit to a brittle fracture dominated by cleavage planes. Adding 0.2% Y2O3 can refine the original β grains and α/α' martensite structure, and achieve dispersion strengthening through nano-scale Y2O3 particles. However, when the Y2O3 content increases to 0.3%, the rare earth oxide particles agglomerate, causing local stress concentration, resulting in a significant decrease in material plasticity. This study provides theoretical and experimental basis for the quantitative modification of rare earth oxides in additive manufacturing titanium alloys.
  • SHI Haicheng, WANG Qiangsong, CAI Tingjun, CHEN Tianyu, HE Yu, CAO Shuguang
    Journal of Netshape Forming Engineering. 2026, 18(2): 31-47. https://doi.org/10.3969/j.issn.1674-6457.2026.02.004
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    W-Ni-Cu alloys demonstrate significant application potential in magnetic field-sensitive precision instruments and high-power electrical components due to their high density, non-magnetic properties, excellent electrical and thermal conductivity, and tunable thermal expansion coefficient. Traditional W-Ni-Cu alloys commonly suffer from a poor strength-ductility match which severely limits their engineering applicability. To address this issue, this study focuses on these alloys, aiming to elucidate the intrinsic relationship between their microstructure and mechanical properties, thereby providing a theoretical basis for overcoming this performance bottleneck. A systematic review was conducted on recent advances in the microstructural regulation and mechanical property optimization of W-Ni-Cu alloys with the emphasis placed on analyzing the effects of composition design (e.g., Ni/Cu ratio optimization), alloying elements (e.g., addition of Fe, Co, La2O3), and advanced preparation techniques (including microwave sintering, spark plasma sintering, hot pressing sintering and selective laser melting) on the alloys' microstructure, densification behavior, and comprehensive properties. Research showed that adjusting the Ni/Cu ratio effectively improved the strength-ductility balance of the alloys. The introduction of trace Co or La2O3 could induce dispersion strengthening and interface optimization, significantly enhancing hardness and wear resistance. The addition of Fe effectively inhibited the coarsening of W particles and enhanced the continuity of W-W interfaces, thereby improving the compressive and bending strengths of the alloys. In terms of preparation techniques, spark plasma sintering and hot isostatic pressing promoted rapid densification while suppressing grain coarsening. Selective laser melting provided a new approach for forming complex components, though challenges such as porosity control and property anisotropy remained. Furthermore, deformation strengthening and heat treatment processes (e.g., quenching-induced spinodal decomposition of the γ phase) further optimized the interfacial structure of the alloy, achieving simultaneous improvements in strength, plasticity, and low-temperature toughness. By optimizing the Ni/Cu ratio, introducing alloying elements, and refining multi-step sintering processes, the grain size of W could be effectively refined and the interfacial bonding state improved, thereby synergistically enhancing the strength and ductility of W-Ni-Cu alloys. This provides critical support for their application in high-end technological fields. Finally, this study outlines future research directions, aiming to offer theoretical insights and technical references for developing high-specific-gravity, high-strength, and high-toughness W-Ni-Cu alloys
  • SUN Shouzheng, GUO Zhenyu, RAN Xudong, LI Kuntai, HU Pan, HAN Zhenyu
    Journal of Netshape Forming Engineering. 2026, 18(2): 48-59. https://doi.org/10.3969/j.issn.1674-6457.2026.02.005
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    The work aims to address the technical challenges of fiber accumulation and bridging at nodes in traditional filament winding for manufacturing composite multi-level grid structures, as well as the difficulty in achieving effective compaction of prepreg tows within deep groove molds. In this study, a dedicated prepreg tow winding head with a lightweight modular design and its precision control system were independently developed. The winding head integrated an adjustable tow guidance channel, a closed-loop tension control system for stable winding, an active thermal management unit combining “hot air heating” and “vortex tube cooling”, and a cutting and restart mechanism for complex paths. Based on the geometric characteristics of the Kagome multi-level grid, a “three-stage layered filling” winding strategy was planned, and corresponding equipment control code was generated via Python scripting. To ensure successful demolding of the complex component, a flexible silicone-plaster composite mold with a “negative draft angle” was designed and employed. Automated winding, forming, and curing experiments of composite cylindrical multi-level grid components were successfully conducted. The winding process was stable, fiber accumulation at the nodes was significantly reduced, the rib morphology was complete with tight interlayer bonding, and the cured, demolded component demonstrated good dimensional accuracy. Axial compression tests revealed a maximum ultimate load of 24 060.60 N, and the failure process exhibited a progressive damage mode characterized by interlayer separation and overall buckling, demonstrating the structure's high load-bearing capacity and damage tolerance. This research validates the feasibility of the developed winding head and staged winding process for fabricating complex multi-level grid structures, providing a new approach for the low-cost, high-quality automated manufacturing of high-performance composite grid structures.
  • GAO Jianfei, FU Jia, XIA Meiling, MU Lang, YU Yunhe, HOU Jixin, XIA Zhixin
    Journal of Netshape Forming Engineering. 2026, 18(2): 60-72. https://doi.org/10.3969/j.issn.1674-6457.2026.02.006
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    In response to the demand for high-quality bonding of martensitic heat-resistant steel/ nickel-based alloy in the field of ultra supercritical thermal power, the work aims to design the composition of the transition layer, and explore the effects of alloy systems and element diffusion on the microstructure and properties. Taking the resistance of high temperature and corrosion into account, and combining with solid solution criteria such as ratio parameter-atomic size difference (Ω-δ), mixing enthalpy (∆Hmix), and valence-electron concentration (VEC), the FeNiCr transition layer was preliminarily screened. The diffusion effects of Fe, Ni, and Cr elements on the phase equilibrium, physical properties, and mechanical properties of G115 martensitic heat-resistant steel and 617B nickel-based alloy were simulated with JMatPro. The calculation results indicated that the FeNiCr alloy was more likely to form a simple solid solution with face-centered cubic (FCC) structure. The diffusion of Cr element caused the disappearance of M6C phase in G115 steel, and the formation of the σ phase was induced when the Cr content reached 9%. Fe diffusion promoted the formation of MC phases in 617B alloy, whereas Cr diffusion eliminated the M6C phase and resulted in the appearance of MC phases. Additionally, the diffusion of Ni element significantly affected the coefficient of thermal expansion and mechanical properties of G115 steel. The diffusion of Fe element led to a decrease in the mechanical properties of 617B alloy, and the diffusion of Cr element improved the hardness and strength of 617B alloy. In conclusion, the transition layer of FeNiCr alloy can achieve infinite solid solution of Fe and Ni elements, while achieving a smooth transition of interface composition gradient. The gradient distribution of physical properties can be formed and mechanical properties can be improved by controlling element diffusion, providing important theoretical reference for the design and performance optimization of dissimilar metal interfaces of martensitic heat-resistant steel and nickel-based alloy.
  • HU Yanchen, DENG Zhenyu, SUN Zhiyuan, LIU Bo, SHI Haicheng
    Journal of Netshape Forming Engineering. 2026, 18(2): 73-80. https://doi.org/10.3969/j.issn.1674-6457.2026.02.007
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    To address the problems of poor Explosively Formed Projectile (EFP) formation and insufficient armor-piercing power of EFP warheads with low-density material shells, the work aims to conduct a combined shell design to improve the performance. Firstly, detonation models of EFP warheads with different shell materials were established by means of numerical simulation. The overpressure and detonation wave impulse at different positions of the liner were obtained to analyze the law of how shell materials affecting EFP formation. Then, numerical simulation and comparison were carried out on the EFP formation of combined shell schemes with different embedding positions, so as to study the effect of embedding positions on EFP formation. Finally, experiments were adopted to verify the flight stability and armor-piercing power of the designed combined shell EFP warheads. Numerical simulation results showed that among the three monolithic shell materials (aluminum, steel, copper), the steel shell EFP warhead provided a higher overpressure peak and the highest detonation wave impulse for EFP driving, and its driving effect on the EFP tail was relatively smooth and durable, which was beneficial to EFP formation. In the combined shell design, embedding a steel ring near the liner in the aluminum shell was conducive to improving the compactness of the EFP head and enhancing the EFP's armor-piercing capability. Experimental results indicated that the EFP formed by the designed combined shell EFP warhead had good flight stability and armor-piercing power. Among aluminum, steel and copper, steel is the most favorable shell material for EFP formation. In the combined shell design, embedding a steel ring near the liner in the aluminum shell helps to increase the detonation wave impulse at the EFP tail during detonation and improve the EFP's armor-piercing capability. Through the simulation and experiment of the combined shell EFP warhead, the goals of improving EFP formation and enhancing EFP's armor-piercing power are achieved.
  • Composites Forming
  • ZHU Qiang, ZHANG Ziang, CHEN Ming, ZHANG Linfu, LIU Kang, FAN Guohua, LI Daoqian, LU Hongguo, ZHANG Jie, SI Yuxiao, ZHANG Peng
    Journal of Netshape Forming Engineering. 2026, 18(2): 81-90. https://doi.org/10.3969/j.issn.1674-6457.2026.02.008
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    The work aims to investigate the influence of layer thickness ratio on the crack propagation mechanisms in Ti/Al laminated composites, so as to provide atomic-scale insights into their excellent strength-toughness synergy. Molecular dynamics simulations were conducted to construct three Ti/Al laminated composite models with varying titanium layer thickness ratio (25%, 50%, 75%) and systematically analyze their tensile behavior and crack dynamic characteristics. During the simulations, uniaxial tensile loads were applied, and the OVITO software was used for real-time tracking and quantitative analysis of atomic motion, stress distribution, dislocation evolution, and crack tip propagation. Results indicated that as the titanium layer thickness ratio increased from 25% to 75%, the peak stress rose by 38.8%. This was primarily attributed to the hetero-deformation- induced hardening effect, where interfacial dislocations enhanced back stress and suppressed plastic instability. The crack propagation mode also transitioned: the 25% Ti model predominantly exhibited Al-dominated nano-void nucleation and growth, leading to a tortuous crack path; while the 75% Ti model showed Ti-constrained crack blunting, resulting in a straighter crack path, suppressed nano-void nucleation, and improved toughness. Notably, the 50% Ti model achieved optimal strength-toughness synergy through balanced dislocation storage and stacking fault confinement, realizing the best strength-toughness synergy. The molecular dynamics simulation results clearly elucidate the critical impact of titanium layer thickness fraction on the mechanical properties and crack propagation mechanisms of Ti/Al laminated composites. Atomic-scale analysis reveals that the layer thickness ratio governs stress redistribution, plastic zone evolution, and interfacial delamination, providing design principles for harmonizing crack resistance and mechanical performance.
  • XU Licui, LIU Siyu, LYU Jun, PAN Changshuai, WANG Zhenmin, LIU Shankui
    Journal of Netshape Forming Engineering. 2026, 18(2): 91-100. https://doi.org/10.3969/j.issn.1674-6457.2026.02.009
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    Focusing on multilayer copper foil composite hot rolling, the work aims to address the challenge of direct tension measurement caused by insufficient initial bonding strength and limited copper strip bendability by proposing an innovative control method to enhance coiling stability. A tension control mathematical model was established to analyze influencing factors and examined motor coiling characteristics to identify key tension fluctuation variables. For dynamic coil diameter measurement, an integrated approach combining encoder-based measurements with linear speed calculations was developed to fuse results through weighted averaging. A Kalman filter was introduced to optimize encoder signals for handling time-varying characteristics, with performance systematically compared against weighted averaging. Real-time tension was indirectly calculated via motor current, while a fuzzy PID controller adjusted rotational speed to maintain constant tension. Simulations on MATLAB/Simulink demonstrated the Kalman filter's superior performance: faster dynamic response, improved abrupt change handling, average coil diameter error <2 mm, and maximum error of 13.12 mm, significantly lower than weighted averaging. In conclusion, the roll diameter result obtained based on the Kalman filter is more accurate. The fuzzy PID control strategy can effectively enhance process stability, providing a reliable technical solution for multilayer copper foil composite rolling.
  • LIU Zhibin, HU Wenjie, YAN Hong
    Journal of Netshape Forming Engineering. 2026, 18(2): 101-109. https://doi.org/10.3969/j.issn.1674-6457.2026.02.010
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    The work aims to study the microstructure, immersion corrosion and electrochemical corrosion properties of Al6061-2 wt.% Ti3C2Tx composites at different solution treatment temperature. The composites were fabricated by vacuum induction melting, and the microstructure and corrosion morphology of the samples were analyzed by optical microscope, scanning electron microscope and three-dimensional profiler. In addition, dynamic potential polarization curves and electrochemical impedance spectra were measured with an electrochemical workstation, and their trend patterns were analyzed. The results showed that the corrosion potential of the composites showed a positive and then negative trend with the increase of solution temperature. Specimens subject to solution treatment at 540 ℃ exhibited optimal corrosion resistance, with a corrosion potential shifted positively by 43 mV compared with untreated specimens and had the lowest corrosion current density (2.18 μA/cm2). Furthermore, electrochemical impedance spectroscopy analysis indicates that solution treatment significantly improved the charge transfer resistance of the composites. After solution treatment at 540 ℃, the charge transfer resistance Rct reached 15 024 Ω·cm2, which was about 2.4 times higher than that of the as-cast specimens. The diffusion coefficient of the Mg2Si phases in the composites after solution treatment at 540 ℃ significantly increased, accelerating the dissolution of these phases into the matrix, which enhanced the corrosion resistance of the composites.
  • Advanced Joining Technology
  • HAN Yue, CAO Yiming, CHONG Benben, CHEN Yu, SHAN Debin, XU Wenchen
    Journal of Netshape Forming Engineering. 2026, 18(2): 110-122. https://doi.org/10.3969/j.issn.1674-6457.2026.02.011
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    Aiming at the problems of poor forming accuracy and severe spring-back of workpiece shapes in flexible spinning technology, the work aims to study the influencing factors of spring-back during the spinning process, analyze the influence laws of different process parameters, and propose relevant measures to improve workpiece accuracy and reduce spring-back. With 5A06 aluminum alloy conical spun components as research objects, the spring-back angle was introduced as an evaluation criterion. Through a combined approach of finite element simulation and experiments, the influence of process parameters on the spring-back of spinning components was analyzed to determine the optimal process parameters and spring-back compensation methods. Based on simulation and experimental analysis, adopting equal circumferential strain, a small feed ratio, and a small pass deformation could effectively suppress the spring-back of the workpiece. The spring-back compensation of adding 3° target deflection angle reduced the spring-back deviation of the main part of the component to -0.21°. By combining the finite element method with process tests, the rebound compensation measures for flexible spinning are summarized, providing effective theoretical guidance for controlling spring-back in flexible spinning components.
  • YU Peng, ZHANG Timing, CHEN Yuhua, YE Zhikang, XIE Jilin, WANG Shanlin, ZHANG Shiyi
    Journal of Netshape Forming Engineering. 2026, 18(2): 123-133. https://doi.org/10.3969/j.issn.1674-6457.2026.02.012
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    The work aims to investigate the influence of process parameters on the microstructure and mechanical properties of the interface of AA1060/DP690T dissimilar metal magnetic pulse welded joints and the effect of nickel plating of the substrate on the joint properties. Welded joints were prepared by magnetic pulse welding equipment, and the effects of process parameters on the microstructure and mechanical properties of the joints were systematically investigated through microstructure observation, energy spectrum analysis, electron backscattering technique and shear strength test. In addition to this, the effect of nickel plating on the performance of the joints was investigated. The highest shear strength of the joints was obtained at a discharge energy of 30 kJ and an initial gap of 1.5 mm, reaching 82.5% of the strength of the aluminum parent material AA1060. The average grain size of the interfacial intermetallic compound (IMC) (0.8 µm) was significantly smaller than that of AA1060 (15 µm) and AA1060 (5 µm), and the indentation depth of the aluminum base material (1 000 nm)<depth of the IMC layer (570 nm)<depth of the steel base material (420 nm), the interface showed the typical hardness transition characteristics. As the discharge energy increased, the interface IMC thickness increased from 3 µm to 20 µm, and the interface failure mode changed from ductile fracture to brittle fracture. At a discharge energy of 30 kJ and an initial gap of 1.5 mm, the maximum shear load of AA1060/nickel-plated DP690T decreased by 22.7% from 4.65 kN to 3.59 kN, and the elongation length increased from 3.02 mm to 4.78 mm, which was a 57.9% increase in elongation length, as compared with that of the joints with AA1060/ DP690T. The intermediate hardness property of the IMC layer (between the two parent materials) realizes the gradient transition of mechanical properties, thus relieving the residual stress caused by the difference in the coefficients of thermal expansion of aluminum/steel, and enhancing the joint performance; the nickel-plated layer makes the joints change from strength-dominated to toughness-dominated, which is more suitable for impact-resistant engineering applications.
  • LI Jingxuan, MAO Yuqing, XU Liang, XU Muzhong, ZHENG Hua, YAN Xianwei, LU Lili, Berdnikova Olena
    Journal of Netshape Forming Engineering. 2026, 18(2): 134-144. https://doi.org/10.3969/j.issn.1674-6457.2026.02.013
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    The work aims to address the problem of the formation of brittle intermetallic compounds (IMCs) such as Ti-Fe during the welding of titanium alloy and stainless steel. Pure vanadium was used as the interlayer material for double-pass laser welding of 5 mm thick TA17 titanium alloy and 321 stainless steel dissimilar materials. After welding, metallographic microscope, scanning electron microscope, universal testing machine, etc. were used to analyze and characterize micro morphology and mechanical properties of the joints, and reveal the joining mechanism at the interface. When the laser power was 4.1 kW (titanium side) and 3.6 kW (stainless steel side), the welding speed was 20 mm/s, and the laser beam shifted to the base material by 0.5 mm, the unmelted vanadium layer could effectively block Ti and Fe elements, and formed a good metallurgical bonding with the fusion zones on both sides. Due to the diffusion of V element, a diffusion layer with a width of about 30 μm was generated between the fusion zone and the vanadium interlayer. The microstructure in the WZ1 diffusion layer was composed of (βTi, V) solid solution, while the WZ2 diffusion layer consisted of γ-Fe and (Fe, V) Fe-based solid solution. Meanwhile, the vanadium layer was softened by twice welding thermal cycles, and the average hardness was about 85.9HV, which was significantly lower than that of the fusion zone and the base material. In addition, the cracks initiated from the vanadium particles precipitated inside the vanadium layer, which resulted in the fracture of the joints into the vanadium layer. The maximum tensile strength was up to 330.6 MPa. The double-pass laser welding of titanium/steel with vanadium as the interlayer can significantly improve the quality of the joints by inhibiting the formation of brittle Ti-Fe intermetallic compounds, which provides the process optimization and theoretical basis for the engineering application of thick titanium-steel composite structures.
  • DENG Jiahao, CHEN Yuhua, XIE Jilin, LIU Guanpeng, WANG Shanlin, ZHANG Timing
    Journal of Netshape Forming Engineering. 2026, 18(2): 145-154. https://doi.org/10.3969/j.issn.1674-6457.2026.02.014
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    The work aims to weld NiTi/Ti6Al4V dissimilar materials by electromagnetic pulse welding technology, compare and analyze welding effects of single-phase NiTi and dual-phase NiTi with Ti6Al4V and study effects of welding process parameters on the interface morphology and mechanical properties of NiTi/Ti6Al4V electromagnetic pulse welded joints. The electromagnetic pulse welding effect of NiTi/Ti6Al4V with different original microstructures was studied by means of scanning electron microscopy, energy dispersive spectrometer, X-ray diffractometer and room temperature tensile test. The interface structure, element distribution, mechanical properties and fracture morphology of the dual-phase NiTi/Ti6Al4V welded joint were analyzed. The interface failure of single-phase NiTi/Ti6Al4V occurred due to the difference of brittle IMCs and thermal expansion. The dual-phase NiTi achieved thermal expansion matching through B19'→B2 phase transformation, reduced stress and achieved metallurgical bonding. The interface waveform of the dual-phase NiTi/Ti6Al4V electromagnetic pulse welded joint was dominated by irregular waveform interface and shear wave interface. The tangential component of the collision velocity of oblique collision caused a series of unstable motions at the interface, and the interface shears formed an irregular wavy interface. Under the action of high-speed shear, the interface was unstable and gradually evolved into shear wave, and the brittle intermetallic compound in the transition layer of the welded joint deteriorated the mechanical properties of the joint. The mechanical properties of the dual-phase NiTi/Ti6Al4V joint reached 26.6% of the mechanical properties of the base metal. The joint fractured at the interface, and the ductile-brittle mixed fracture dominated by toughness occurred in the joint. Interface failure occurs during single-phase NiTi/Ti6Al4V welding. Shear wave increases the mechanical properties of the dual-phase NiTi/Ti6Al4V joint, and the brittle intermetallic compounds in the transition layer reduce the mechanical properties of the joint.
  • Additive Manufacturing
  • HUANG Kai, ZHANG Wei, BAI Dehu, WANG Xi, BAI Yuxi, LU Chenyang, GAO Rui
    Journal of Netshape Forming Engineering. 2026, 18(2): 155-168. https://doi.org/10.3969/j.issn.1674-6457.2026.02.015
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    Targeting the potential application requirements of the second-generation FeCrAl alloy (C35MN) in accident-tolerant fuel claddings for nuclear reactors, the work aims to investigate the effect of selective laser melting (SLM) additive manufacturing on the alloy's microstructure, thereby optimizing and enhancing its mechanical properties. X-ray diffraction (XRD), scanning electron microscopy (SEM), transmission electron microscopy (TEM), and electron backscatter diffraction (EBSD) were employed to characterize and analyze the density, phase and grain morphology of FeCrAl alloys fabricated under different parameters (e.g., layer thickness, scanning speed). The laser volumetric energy density (VED) had a significant impact on the alloy's density, grain morphology, and texture. At lower energy densities (e.g., VED<1.6×102 J/mm³), the fabricated materials exhibited weak preferred orientation, and grains tended to grow in various directions. However, excessively high energy density (e.g., 2.67×102 J/mm³) led to columnar grain structures with stronger texture and relatively lower density. Increasing the laser scanning speed promotes the multiplication of dislocations and the precipitation of high-density nanoscale particles. When the scanning speed is 500 mm/s and the energy density is 2×102 J/mm³, the alloy achieves a tensile strength of up to 800 MPa with a uniform elongation of 4%. The residual stress of the alloy decreases after annealing at 1 100 ℃ for 1 h. Although the Laves precipitation phase grows up, the Vickers hardness decreases by 86HV compared with the pristine alloy.
  • FANG Lijia, SUN Bingbing, ZHAO Haisheng, ZHANG Qiang, HE Ruikai
    Journal of Netshape Forming Engineering. 2026, 18(2): 169-182. https://doi.org/10.3969/j.issn.1674-6457.2026.02.016
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    The work aims to investigate the formation causes of micro-defects during the forming process of K477 nickel- based superalloy via selective laser melting, as well as the evolution rules of microstructure with respect to process parameters, thereby providing theoretical support and practical guidance for achieving high-quality forming processes. With K477 alloy formed under two typical SLM (Selective Laser Melting) process parameters of high power and low power as the research objects, the affecting factors of microcracks were analyzed by observing their microscopic morphology, as well as the distribution and content of various elements. Subsequently, K477 alloy specimens were formed by adjusting different laser scanning speeds (700, 800, 900, 1 000, 1 100, and 1 200 mm/s) and laser powers (150, 200, 250, 300, 350, and 400 W). Optical microscopy was employed to analyze internal defects, X-ray diffraction (XRD) was used to examine the phase composition, and scanning electron microscopy (SEM) was combined to investigate the evolution rules of the microstructure. Under two typical process parameters, a γ+γ° eutectic phase was observed at crack sites within the materials formed by selective laser melting. The distribution maps of aluminum (Al) at the cracks corresponded to those of carbon (C) and oxygen (O). Moreover, notable local enrichment of carbon and oxygen elements was observed near the cracks. By adjusting different laser powers and scanning speeds, it was found that as the laser scanning speed increased to 800 mm/s, the relative density reached 99.970%. When the laser power increased to 350 W, the relative density reached 99.977%. The presence of the γ+γ° eutectic phase within the selective laser melted K477 material is the primary cause of crack formation. During the solidification process, aluminum (Al) elements contribute to the formation of carbides, oxides, as well as nickel-chromium oxides, which acts as crack initiation sites near the grain boundaries. The variation in heat flow distribution caused by differences in laser scanning energy indicates that optimizing process parameters can suppress crack formation to a certain extent.
  • ZHOU Shengjie, LIAO Luhai, LI Fengguang, HU Shengbo, LIU Jianyong
    Journal of Netshape Forming Engineering. 2026, 18(2): 183-195. https://doi.org/10.3969/j.issn.1674-6457.2026.02.017
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    The work aims to analyze the mechanical properties of six lattice structure units (Octet, Kelvin, Fluorite, Diamond, Schwarz, and Gyroid) under different working conditions, and screen out the optimal lattice structure for lightweight design so as to address the lightweight design requirements of racing car suspension rocker arms. The six array lattice structure units were constructed using nTopology software with a porosity set to 50%. Finite element analysis was employed, with consistent mesh division for all six structures. Their displacement and stress performances were compared under four working conditions (tension, compression, torsion, and bending) with a 4 kN load. Under compression and bending conditions, the Schwarz lattice exhibited the optimal displacement (0.013 3 mm, 0.025 mm) and stress (128.10 MPa, 256.96 MPa). When applied to the racing car suspension rocker arm, the redundant materials were removed through hollow design, resulting in a reduction in volume from 424 236.70 mm3 to 269 888.33 mm3, a decrease in mass from 1.192 kg to 0.758 kg, and an increase in specific strength by approximately 57.3%. The maximum stress of the racing car suspension rocker arm was 38.62 MPa, which was much lower than the maximum stress of 251.5 MPa under high safety factor; the maximum displacement was 0.27 mm, far below the displacement threshold of 1.155 mm under high safety factor; the maximum strain was only 0.05%, significantly lower than the ultimate strain of 0.35% under high safety factors. The material did not enter the plastic deformation stage, indicating sufficient safety margin. The application of the Schwarz lattice in racing car suspension rocker arms achieves significant lightweighting with sufficient safety margin, further expanding the application scenarios of lattice structures in automotive engineering. It is particularly valuable for key components subject to complex loads, providing an innovative solution for the lightweight design of automotive parts.
  • SU Xuan, ZHANG Zhaohui, CHEN Xiaoyan
    Journal of Netshape Forming Engineering. 2026, 18(2): 196-207. https://doi.org/10.3969/j.issn.1674-6457.2026.02.018
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    The work aims to propose a high-performance multi-material integrated extrusion head and its control system to address the problems of mechanical performance dispersion and insufficient structural accuracy of printed components caused by asynchronous extrusion of multiple materials, uneven temperature field, and unstable interface bonding quality in the melt deposition molding of continuous carbon fiber composites, so as to achieve precise collaborative control of the printing process of composites. Firstly, based on the analysis of the flow characteristics of short fiber filaments and the online impregnation mechanism of continuous fibers, the design of a multi-channel extrusion head structure was completed. The extrusion head featured partitioned, independent temperature control modules to provide precise thermal management for extrusion printing of various materials. It also incorporated an integrated micro wire cutting mechanism, enabling precise fiber cutting and restart during the printing process. Secondly, an integrated printing control system was constructed to adjust the power of the heater in real time through a PID algorithm, and synchronously coordinate the three-axis motion platform, wire feeding motor, and fiber feeding servo mechanism. Finally, the mechanical properties of unreinforced matrix and continuous carbon fiber reinforced composite specimens were compared and analyzed with a universal testing machine. Experimental data showed that, compared with the unreinforced matrix, the mechanical properties of composites reinforced with continuous carbon fibers were significantly improved, with a tensile strength of 653.7 MPa and a tensile modulus of elasticity increased to 32 675.95 MPa. In conclusion, the proposed multi extrusion head design and control system effectively improves the printing quality and mechanical properties of continuous carbon fiber composites, achieves stable coordination and control of multi-material printing, and provides a reliable process solution for additive manufacturing of complex fiber-reinforced structures.
  • Light Alloy Forming
  • LU Zuchao, LU Laixiao, SUN Jie, SHI Qilong, ZHAN Hong, SHU Dayu
    Journal of Netshape Forming Engineering. 2026, 18(2): 208-217. https://doi.org/10.3969/j.issn.1674-6457.2026.02.019
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    The work aims to study the static and dynamic mechanical properties of ZL114A aluminum alloy under different strain rates and temperature, and combine quasi-static tensile tests and dynamic Hopkinson bar tests to systematically analyze its flow stress behavior and establish a Johnson-Cook constitutive model. Quasi-static tensile tests were conducted with an electronic universal testing machine to obtain the stress-strain curve of the material under quasi-static conditions. Combined with a Split Hopkinson Pressure Bar (SHPB) equipped with an electromagnetic heating device, dynamic compression tests were conducted to obtain stress-strain curves of the material under different temperature and strain rates. The effects of temperature (20-420 ℃) and strain rate (1 500-5 800 s-1) on the mechanical properties of the material were investigated. Through the method of least squares fitting of the experimental data, a Johnson-Cook constitutive model applicable under high temperature and high strain rate conditions was established. The results indicated that the material exhibited relatively weak strain rate sensitivity under room temperature and low strain rate conditions; It showed higher temperature sensitivity under high-temperature conditions; The flow stress of the material significantly increased with strain, while an increase in temperature led to a thermal softening effect, resulting in a decrease in flow stress. The established J-C constitutive model, fitted using the least squares method, can effectively couple the effects of strain, strain rate, and temperature, and its predictions are generally consistent with the experimental data within a certain range of error. In conclusion, the established Johnson-Cook constitutive model can effectively predict the mechanical response of materials under complex working conditions, providing a theoretical basis for structural design and optimization in the fields of aerospace, automotive, and mechanical engineering.
  • XU Yong, CHEN Fakai, ZHANG Chi, XIE Wenlong, ZHANG Shihong, CHEN Liansheng, TIAN Yaqiang
    Journal of Netshape Forming Engineering. 2026, 18(2): 218-225. https://doi.org/10.3969/j.issn.1674-6457.2026.02.020
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    To develop manufacturing technologies suitable for pure titanium bipolar sheets, the work aims to investigate the effect of polyurethane soft mould forming process parameters on the forming quality of the fine and dense microchannel structures in pure titanium sheets. With 0.1 mm thick TA1 pure titanium as the experimental material, forming experiments were conducted by varying the equipment pressure, polyurethane thickness, and hardness during the polyurethane soft mould forming process. The differences in microchannel forming depth and wall thickness distribution under different parameters were compared and analyzed. The microchannel forming depth increased with increases in equipment pressure, polyurethane thickness, and hardness, with equipment pressure having the greatest impact. When the equipment pressure increased from 10 MPa to 50 MPa, the microchannel depth increased from 142.7 μm to 348 μm. In polyurethane soft mould forming, the two regions with the greatest overall thinning of the microchannels were the upper and lower rounded corners. When the equipment pressure and polyurethane thickness were consistent and the depth reached the expected depth, the average wall thickness reduction rate of microchannels under polyurethane with a hardness of 75 Shore A was 23.08%, while under polyurethane with a hardness of 85 Shore A, the average wall thickness reduction rate was 9.84%. By adjusting process parameters such as equipment pressure, polyurethane hardness, and thickness, local thinning of pure titanium sheets can be effectively suppressed, thereby improving the forming quality of microchannels.
  • WU Fengbiao, LYU Hang, LIU Xinyan, NING Fangkun, KANG Xiaoping, JIA Weitao
    Journal of Netshape Forming Engineering. 2026, 18(2): 226-235. https://doi.org/10.3969/j.issn.1674-6457.2026.02.021
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    The work aims to elucidate the dynamic evolution mechanisms of mixed-grain structures in AZ31 magnesium alloy sheets during annealing, to address the issue of alternating grain refinement and coarsening along with mixed-grain formation caused by repeated inter-pass reheating in conventional multi-pass hot rolling, clarify the influence of annealing on microstructure and mechanical properties, and provide a theoretical foundation for precise control of the final rolled sheet's performance. Based on mixed-grain samples containing multi-scale grains, shear bands, and twins, their microstructural evolution under varying annealing temperature (170-300 ℃) and holding periods (0.5-3 h) were systematically investigated. The corresponding effects on mechanical properties were analyzed. When the annealing temperature exceeded 200 ℃, the mixed-grain structure was significantly improved, enhancing microstructural homogeneity. The grain size demonstrated a characteristic evolution pattern of initial refinement followed by coarsening with prolonged annealing time, a trend that became more pronounced at elevated temperature. Within the 170-300 ℃ range, annealing temperature dominated tensile strength, while the holding period primarily affected ductility. The maximum elongation (24.5%) occurred at 250 ℃-2 h, attributed to sufficient recrystallization nucleation and pronounced twin reduction. At fixed temperature, hardness typically peaked after 1 h. This nonlinear behavior stemmed from competing mechanisms between grain equiaxed transformation and twin evolution. Rational selection of annealing temperature and time can enhance microstructural uniformity and balance strength-ductility trade-offs, offering critical guidance for optimizing annealing processes in wide AZ31 magnesium alloy sheets.
  • Copper Alloy Forming
  • LIU Yuan, LIN Zhilin, XU Cheng, ZHANG Qingke, SONG Zhenlun
    Journal of Netshape Forming Engineering. 2026, 18(2): 236-247. https://doi.org/10.3969/j.issn.1674-6457.2026.02.022
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    The work aims to study the influence law of cold rolling deformation on the grain growth and direct bonding performance of high temperature oxygen-free copper for IGBT modules, so as to provide a cold rolling process reference for obtaining a controllable and uniform grain structure after high-temperature treatment. The microstructure of oxygen-free copper with different cold rolling deformation amounts as well as its microstructure after high-temperature treatment at 1 000 ℃ was characterized by metallographic and electron backscatter diffraction (EBSD) techniques to explore the relationship between grain boundary characteristics and grain orientation with grain size and distribution of oxygen-free copper subjected to high temperatures treatment. The direct-bonding performance of oxygen-free copper strip and ceramic composite at high temperatures was also investigated by simulating the direct bonding process. The results show that the effect of cold rolling deformation on the high-temperature grain growth of oxygen-free copper is mainly influenced by substructure, dislocation structure, and grain orientation of the material. With the increase of cold rolling deformation, the grain size of oxygen-free copper after high-temperature treatment increases first and then decreased, and the size distribution gradually becomes uniform. The simulated direct bonding performance evaluation shows that as the cold-rolling deformation increases, the bonding between oxygen-free copper and ceramic plates became tighter and the grain size was more uniform. When the cold rolling deformation exceeds 13%, a competitive mechanism is put forward for grain growth. As the deformation increases, the average grain size decreases and the size distribution becomes more uniform. After the samples with 57% rolling deformation are subject to simulated direct bonding, a relatively uniform grain structure with the smallest size is obtained.
  • SHANG Yu, CEN Guibin, YAN Xuehua, WU Jili, LU Tao
    Journal of Netshape Forming Engineering. 2026, 18(2): 248-258. https://doi.org/10.3969/j.issn.1674-6457.2026.02.023
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    High-strength and high-conductivity copper alloys serve as key materials in rail transit, power transmission, and electronic packaging, where the synergistic optimization of strength and electrical conductivity remains a central research challenge. As a representative material system, Cu-Cr alloys struggle to simultaneously achieve both properties. This paper systematically reviews recent progress in composition design and phase formation mechanisms of Cu-Cr alloys, emphasizing the regulatory role of multi-component alloying strategies on microstructure and performance. Studies demonstrate that Mg suppresses precipitate coarsening through interfacial enrichment while promoting heterogeneous nucleation of nano-Cr phases, whereas Si can reduce stacking fault energy thus accelerate Cr precipitation and induce twin strengthening. Zr effectively can refine grains but it needs mitigation of oxidation during melting, while Ti can enhance thermal stability by forming Cr-depleted zones via rapid diffusion. Ag can optimize dendritic morphology at the expense of higher costs, and Nb can significantly improve strength and high-temperature performance by forming high-melting-point Cr2Nb phases with Cr. Notably, the synergistic interaction of Mg and Si may introduce Laves phases (e.g., Cu2Mg, Mg2Si), offering novel strategies to balance strength and plasticity. Further analysis reveals the coupled effects of deformation, solid solution, precipitation, and grain refinement on mechanical properties and conductivity. While severe plastic deformation markedly enhances strength, it drastically degrades conductivity. In contrast, nano-precipitates such as Cr and Cu4Sc enable strength breakthroughs under high conductivity through the Orowan mechanism. Building on these findings, this study proposes an alloy design framework centered on establishing a “composition-structure-property” mapping relationship, and highlights emerging trends involving novel precipitates (e.g., Laves phases) and multi-scale simulation methods. These insights provide theoretical and technical foundations for designing advanced Cu-Cr-based alloys, paving the way for their expanded applications in high-temperature environments, electronic packaging, and extreme operational conditions.
  • YANG Yunxi, QIANG Fengming, WANG Wen, ZHANG Yuye, XUE Zetian, MA Qianzhi, LI Yunbo, LIU Yilin, SUN Yongliang, WANG Kuaishe
    Journal of Netshape Forming Engineering. 2026, 18(2): 259-265. https://doi.org/10.3969/j.issn.1674-6457.2026.02.024
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    The work aims to investigate the re-dissolution behavior of the primary phase in Cu-3.4Ti alloys and its effect on the synergistic regulation of microstructural evolution and mechanical properties under different solution treatment temperature, so as to provide a theoretical basis for the optimization of subsequent aging and forming processes for Cu-Ti alloys. Based on the Cu-Ti phase diagram, solution treatments were performed at 800, 850, 900, and 950 ℃. X-ray diffraction (XRD) was used to analyze the phase composition. Optical microscopy (OM) was employed for microstructural observation to examine the grain morphology. Scanning electron microscopy (SEM) equipped with energy dispersive spectroscopy (EDS) and electron backscatter diffraction (EBSD) was utilized for compositional and microstructural analysis. Tensile tests were conducted at room temperature to measure the tensile strength and elongation of the alloys. The results indicated that at solution treatment temperature of 800-950 ℃, the Cu3Ti primary phase in the as-forged alloy was largely re-dissolved, significantly increasing the matrix's supersaturation. As the temperature increased, the alloy grain size grew progressively, with abnormal grain growth and grain boundary overburning observed at 950 ℃, leading to a decrease in structural stability. Mechanical testing revealed that the tensile strength increased initially and then decreased with the temperature rise, while the elongation continuously decreased. The solution treatment temperature has a significant impact on the microstructure, mechanical properties, and formability of the forged alloy. After solution treatment at 850 ℃ for 1 h, the Cu-3.4Ti alloys exhibit the best overall performance, with a tensile strength of 527.3 MPa and an elongation of 51.1%, along with improved formability.
  • Superalloy Forming
  • LIU Manping, ZONG Zhouyingyi, MA Hui, CHEN Yulin, LI Haohao, ZHAO Guoping, SUN Shaochun
    Journal of Netshape Forming Engineering. 2026, 18(2): 266-274. https://doi.org/10.3969/j.issn.1674-6457.2026.02.025
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    To investigate the causes of crack formation of nickel-based superalloys during use, the work aims to analyze the grain boundary cracks in directionally solidified CM247LC alloy, and study the effect of microsegregation of alloy elements and carbides on cracking behavior. The microstructure of CM247LC alloy in as cast and heat-treated states was observed with a light microscope. The distribution of fine γ/γ' eutectic precipitates and MC carbides inside the alloy was analyzed by scanning electron microscopy, and the segregation of elements in different regions was obtained. The cross-sectional microstructure of directionally solidified cast CM247LC alloy was dendritic, with obvious MC carbides and γ/γ' eutectic structures between dendrites. The alloy exhibited severe segregation in the as cast state. Compared with the heat-treated state, the grain boundary cracks in the as cast state were wider, and the microstructure and morphology of the grain boundary cracks were clearer. The location of the grain boundary cracks was still in the interdendritic region. Owing to the mismatch in elastic and thermophysical properties between MC carbides and the matrix, stress concentration is prone to occur at their interface regions, which may induce microcracks. When MC carbides become enriched in local areas, the stress concentration effect is further intensified. Once the local stress exceeds the fracture strength of the material, cracks initiate and propagate, ultimately leading to alloy cracking.
  • SI Haoxue, LANG Zhenqian, TENG Junfei, ZHANG Song, LI Hong
    Journal of Netshape Forming Engineering. 2026, 18(2): 275-281. https://doi.org/10.3969/j.issn.1674-6457.2026.02.026
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    To realize the high-precision hot forming of superalloy sheets, the work aims to design reasonable forming process parameters and effectively control springback deformation. Based on the central composite experimental design and finite element simulation technology, the three-dimensional numerical simulation of the hot forming process of GH3230 alloy sheet was carried out. The areas of maximum thickness reduction and maximum springback were located at the arc edge of the sheet. The maximum springback of the sheet decreased gradually with the increase of forming temperature and friction coefficient, while it increased obviously with the increase of punching speed. Hot forming process parameters had minor effect on the thickness of GH3230 alloy sheet. A second-order response surface model of the maximum springback and the maximum thickness reduction during hot forming of GH3230 alloy sheet with the change of forming process parameters was established. Based on this model, the optimized forming process parameters were as follows: the forming temperature was 937 ℃, the friction coefficient was 0.18, and the punching speed was 1 mm/s. The maximum springback of GH3230 alloy sheet after hot forming at the optimized forming process parameters was 0.33 mm, and the maximum thickness reduction was 0.053 mm, which could meet the actual production requirement. The results obtained by simulation are close to the calculated values of the theoretical model, verifying the accuracy of the response surface model.