Open Access Article
Junchao
Yi
a and
Gary J.
Cheng
*ab
aThe Institute of Technological Sciences, Wuhan University, Wuhan 430072, P. R. China. E-mail: gjcheng@purdue.edu
bSchool of Industrial Engineering, Purdue University, West Lafayette, IN 47906, USA
First published on 21st October 2025
Achieving precision and balanced properties in additive manufacturing (AM) of metallic alloys remains challenging due to rapid melting–solidification cycles, leading to unpredictable microstructures and inconsistent mechanical performance. Conventional AM suffers from high costs, limited adaptability, and brittle secondary phases, compromising load-bearing capacity and structural precision, particularly in alloys like nickel-titanium (NiTi) that are sensitive to high-energy inputs. To overcome these limitations, we present an in situ nanoscale heterostructure engineering (INSHE) strategy that addresses the trade-offs in AM for achieving enhanced mechanical and functional properties. INSHE leverages high-energy laser powder bed fusion (L-PBF) to create uniformly distributed multi-nanoprecipitate assemblies with lattice-matched interfaces, achieving precise modulation of non-equilibrium microstructures from the bottom up. By controlling the inclusion of multi-precipitate seeds and ultrafine heterostructures, INSHE maintains thermodynamic stability under L-PBF's extreme conditions, achieving consistent distribution across the build direction. When applied to a NiTi shape memory alloy, INSHE formulates boron carbide (B4C) additively to form a nanoengineered B2-TiB2-TiC phase heterostructure that enhances both strength and adaptability beyond conventional alloys. INSHE-based shape memory alloys (SMAs) demonstrate an ultrahigh yield strength of up to 2.15 GPa with a delayed plasticity of 12%, more than double the hardness of pristine SMAs (4.94 GPa), and a 66% increase in the hardness-to-modulus ratio (H/Er), which promotes wear resistance via lubricating oxide film formation. INSHE-engineered SMA mechanical metamaterials (SMMMs) demonstrate superior strain recovery and durability under cyclic and gradient loads over conventional SMAs. These SMMMs achieve specific energy absorption (SEA) up to 25 J g−1, surpassing the typical 1–20 J g−1 range of composites and other micro-/nanolattice metals, demonstrating exceptional resilience. The activation of corresponding variant pairs (CVPs)—twin-related martensitic variants—enhances cyclic phase transformations, prevents stabilized martensite retention, and enables efficient energy absorption. INSHE's nanoengineered heterostructure within the B2 phase promotes multiple synergistic deformation mechanisms that resist shear-induced amorphization and prevent crystalline fragmentation. This results in significantly improved damping capacity, linear elastic behavior across transformation temperatures, and nearly ideal shape recovery, achieving superior actuation efficiency over multicomponent and commercial Snoek-type high-damping alloys. Micro-CT imaging confirms INSHE's superior internal quality and precision in complex geometries, addressing powder adhesion and surface roughness through enhanced powder absorption and thermochemical tuning. INSHE also advances printability by refining powder feedstock design and laser processing parameters. This transformative strategy paves the way for the application of alloys with tailored multifunctional properties in topological architectures, unlocking new possibilities for dynamic adaptive materials with superior structural and functional performance.
New conceptsWe introduce an in situ nanoscale heterostructure engineering (INSHE) strategy as a breakthrough in alloy design for additive manufacturing (AM), enabling simultaneous enhancement of printability, structural fidelity, and functional performance. Unlike conventional approaches that rely on equilibrium-phase alloy chemistries or post-processing to introduce functional phases, INSHE leverages laser-driven thermochemical reactions and lattice-matched nanoscale assembly to create uniform dual-nanoprecipitates directly during printing. This strategy enables real-time microstructure modulation across multiple scales, unlocking bottom-up control of alloy behavior and eliminating long-standing trade-offs between strength, ductility, and print precision. Unlike prior works that incorporate passive nanoparticles or metastable additives into feedstock, INSHE actively triggers nanometallurgical transformations in situ, improving thermal stability, increasing laser absorptivity, and achieving high-fidelity 3D structures with smooth surfaces. The resulting adaptive alloys exhibit exceptional mechanical and damping properties—surpassing leading AM alloys in specific energy absorption, fatigue resistance, and phase transformation dynamics—without the need for post-treatment. INSHE represents a paradigm shift in AM alloy design, introducing a dynamic material platform where the microstructure, mechanical performance, and functionality are co-optimized through process-informed design. This concept paves the way for high-performance adaptive materials for advanced applications in sensing, energy harvesting, aerospace, and biomedical devices. |
A further thorny dilemma is that many functional metallic alloys, which are compositionally sensitive, are inevitably exposed to a high energy input (∼105–7 W cm−2) and large temperature gradients (∼105–6 K m−1) during the additive manufacturing process.19,20 It also results in their intended functional performances being particularly susceptible to impact, which poses an additional challenge for the specific applications of smart components made from these alloys. A typical example is the deterioration of the phase transformation behavior of nickel-titanium shape memory alloys (NiTi SMAs) due to the loss of the Ni element by evaporation.21 The reason why these SMAs exhibit remarkable functional characteristics, such as the superelasticity effect (SE) and the shape memory effect (SME), is closely linked to stress-induced thermoelastic martensitic phase transformation (SIMT) and inverse martensitic phase transformation (IMT) occurring in the microstructures.22,23 The alloy design for the secondary phase in such cases encounters non-negligible complexity and applicability difficulties and is thus forced to make trade-offs from numerous mutually exclusive relationships.9 The confluence of these issues has made it exceedingly challenging to achieve balanced mechanical properties and functional performances directly in the as-printed state.
We present an in situ nanoscale heterostructure engineering (INSHE) strategy to address this challenge by precisely introducing a uniform dual nanoprecipitation through the in situ formation of nanoscale new phases and systematic engineering of heterostructures within functional metallic alloys. The INSHE design framework focuses on the controlled synthesis and lattice-matched assembly of nanocrystals to ‘'bottom-up'’ modulate non-equilibrium microstructures. This advancement enables us to fully harness the exceptional properties of functional metallic alloy systems, such as NiTi SMAs,19 in response to the increasing demand for structural complexity and functional integration. By overcoming the mechanical versus functional behavior trade-off through nanoscale synergistic deformation mechanisms—including locally shear-induced amorphization of the B2 matrix and crystalline fragmentation of dual nanoprecipitates—we have achieved an exceptional combination of mechanical properties and multifunctional responses directly from additive manufacturing. Furthermore, our approach offers significant advantages in printability for complex spatial structures, providing a framework that could inform the design of other alloy systems.
Specifically, we have harnessed the extreme metallurgical environment of laser powder bed fusion additive manufacturing (LPBF-AM) and an adaptive alloy design strategy to enable dual-nanoprecipitates in situ embedded within eutectic colonies in near-equiatomic Ni50.8Ti49.2 (at%) SMAs. Through crystallographic design, we engineered the flawless nanoscale assembly of two distinct lattice structures—hexagonal structure (Hex) and face-centered cubic (FCC)—to create a unique reinforcement with ultrafine heterostructures. This differs from previous concepts in alloy design based on ‘ex situ’ doping modifications, as the laser-excited transient nanometallurgical behavior during the build-up process will drastically modulate the non-equilibrium microstructures across multiple scales.10Fig. 1A schematically illustrates the design principle for creating dual-nanoprecipitates by lattice assembly in the in situ nanometallurgical SMA (INSMA hereafter). Specifically, boron carbide (B4C) nanoreactants are used as in situ reactants, hydrostatically adsorbing onto and mixing with SMA micropowder to serve as the reaction medium. A detailed description of the powder preparation process can be found in the Materials and methods section. Subsequently, a high-energy-density laser beam selectively melts the powder feedstock while continuously driving thermochemical reactions in the micron-sized melt pool.29 In this process, the SMA melt continuously supplies a stable titanium source, facilitating the rapid nucleation of free-state carbon and boron atoms, which preferentially grow with a low mismatch and a highly ordered interfacial structure. The subsequent rapid solidification ultimately results in the in situ formation of dual-nanoprecipitates within the matrix grain interior, consisting heterogeneously of titanium carbide (TiC, NaCl-type, space group pm
m) and titanium diboride (TiB2, C32-type, space group P6/mmm).
To elaborate the feasibility of tailored reaction paths from a thermodynamic perspective, we calculated both the phase diagram and the chemical potential diagram of the Ti–B–C ternary system to predict the relationship between constituent phases, the chemical potential of each element, and the stability region of each phase (Fig. 1B and C). Across a wide compositional space, TiC and TiB2 emerge as the most energetically and structurally stable phases, favoring their in situ formation within the high-temperature melt pool—a prerequisite for controlled nanoprecipitate synthesis. To support this, we evaluated the temperature-dependent standard Gibbs free energy and enthalpy changes for all relevant reactions (Fig. S1 and Table S1). The target reactions exhibit a large negative standard Gibbs free energy change (ΔfG0298) and a standard enthalpy change (ΔfH0298) across the processing window (Table S2), indicating thermodynamic favorability and the potential for self-sustained exothermic reactions during LPBF-AM.30 This suggests that ultrafast laser interactions with nanoreactant-functionalized SMA powders can reliably form lattice-matched TiC and TiB2 nanoprecipitates within ∼80 μs. Additional validation is provided through convex hull and chemical potential analyses of relevant binary systems (Fig. S2), which reinforce the stability of the proposed phase configurations in the molten SMA matrix. This thermodynamically guided framework enables precise dual-nanoprecipitate formation through lattice-matched in situ reactions between tailored nanoreactants and the SMA matrix. The comprehensive thermodynamic analyses—including phase diagrams, chemical potential mapping, and Gibbs free energy calculations—collectively establish the viability of the INSHE strategy during LPBF-AM. While the martensitic phase transformation behavior is indeed a key factor governing the mechanical and functional properties of NiTi alloys, our experimental investigations systematically integrate both phase transformation characteristics and mechanical performance metrics, thereby providing a holistic validation of this approach. Importantly, the INSHE strategy is not confined to NiTi shape memory alloys. The thermodynamic design framework and in situ precipitation engineering demonstrated here are broadly applicable across a wide range of metallic systems. In particular, the methodology can be readily extended to Ti-based alloys and beyond through rational reactant selection and reaction pathway design. As a preliminary demonstration of its broader applicability, the INSHE strategy was also implemented in an additional Ti–6Al–4V alloy system (Fig. S47), where uniform nanoreactant-functionalized powders led to refined microstructures and the in situ formation of coherent dual-nanoprecipitates, thereby validating the versatility of the approach beyond NiTi alloys. To this end, we are currently employing high-throughput computational screening to identify compatible precursor–matrix pairs, with the aim of generalizing the INSHE strategy for the development of next-generation multifunctional alloys tailored for additive manufacturing applications.
The bright-field transmission electron microscopy (TEM) image (Fig. 1D) reveals the typical heterogeneous architectures in a dual-nanoprecipitate. More information on the morphology of the dual-nanoprecipitates diffusely dispersed within the B2 austenite matrix grains can be found in Fig. S3, with an average size of ∼100 nm. Among the observed precipitates, each of the ultrafine heterostructures had notable facets, indicating the presence of a preferred crystallographic orientation relationship (OR) between the two constituent phases.31 We further conducted structural investigation on the interfacial features at the atomic and nanoscale. The high-resolution TEM (HRTEM) image (Fig. 1E) shows that the ultrafine heterostructure consists of nano-TiC as the primary nucleation phase assembled with nano-TiB2 as the heterogeneous phase, as confirmed by the fast Fourier transform (FFT) pattern. According to high-angle annular dark-field (HAADF) scanning TEM (STEM) imaging and energy-dispersive x-ray spectroscopy (EDS) mapping (Fig. 1H), multiple intragranular concentration gradients are evident alongside the TiC–TiB2-B2 interphase interface region, leaving a short-range diffusion zone of C and B elements at the outer edge. The observation taken along the [01
]TiC//[2![[1 with combining macron]](https://www.rsc.org/images/entities/char_0031_0304.gif)
0]TiB2 zone axis shows the presence of crystalline domains, and the acquired higher-magnification HRTEM images and associated FFT patterns depict the detailed nanostructures near the phase interface in the heterostructure (Fig. 1F and G). It is clear that the interfacial structure between the TiC and TiB2 phases displays full lattice coherence and has a preferential OR along the close-packed planes: (111)TiC//(0001)TiB2 and [01
]TiC//[2![[1 with combining macron]](https://www.rsc.org/images/entities/char_0031_0304.gif)
0]TiB2, which verifies our original intention of designing the lattice-matching strategy. Moreover, the calibration results of the remaining partitioned heterostructures in Fig. 1D after specific indexation are shown in Fig. S4. We found that all ultrafine heterostructures at different partitions have an equivalent OR and a typical coherent interface without mismatch dislocations. Even the structural analysis of other dual-nanoprecipitates undergoing lattice assembly matches perfectly with the above features (Fig. S5).
In essence, laser-excited thermochemical reactions aim to minimize the critical nucleation energy barrier for the system in the vast majority of the cases.32 The primary precipitation of the TiC phase in the B2 matrix provides perfectly flat and clean bare interfacial sites for the heterogeneous nucleation and growth of a lattice-matched TiB2 phase. On the other hand, as the B4C nanoprecursors were involved in the in situ reaction in the molten pool, they would be spontaneously and continuously consumed and eventually used up. The exsolution of C atoms with the TiC phase causes the B atoms to be expelled to the solid–liquid (S–L) interface, i.e., the solidification front,33 creating an elemental aggregation zone, which, in turn, promotes the formation of the B-rich TiB2 phase. Consequently, a symbiotic relationship between the TiC phase and the adjacent TiB2 phase can be identified. Notably, when the spatial dimensions of the primary nucleation phase are too small (less than 50 nm), it is frequently unable to in situ generate a heterogeneous phase (Fig. S6). The symbiotic mechanism demonstrates that this is attributed to the presence of a large boundary curvature at the primary stage, and the B-atom concentration aggregated by solute redistribution has not yet reached the critical nucleation threshold. In Ti-rich alloy melts, the driving force for the growth of TiC crystal nuclei is the continuous diffusion of supersaturated free-state C atoms in the liquid phase to the phase interface.34 Nevertheless, once the TiB2 lattice groups begin to be assembled and deposited on its surface, short-range diffusion along the close-packed planes to which they are docked will be impeded. The TiC lattice then turns to expand to both sides, thereby developing significant bulges, while the TiB2 lattice can only be stacked along the longitudinal direction at this time (Fig. S3G–I). Benefiting from the combined constraints of minimized lattice misfit, similar atomic packing along matched crystallographic planes, and thermodynamic stability in the desired products, this unique configuration strategy, which is both synergistic and competitive, facilitated the precise in situ synthesis of fine dual-nanoprecipitates. Although the current mechanistic understanding primarily relies on ex situ HRTEM/STEM observations combined with thermodynamic calculations, future integration of time-resolved in situ characterization techniques, such as in situ high-energy X-ray imaging,35operando synchrotron X-ray diffraction,36 and in situ neutron diffraction,37 may offer direct insights into the nucleation barriers and growth kinetics of dual-nanoprecipitates during rapid solidification (cooling rates ∼103−–6 K s−1) in AM, particularly their dependence on processing parameters (e.g., laser power and scan speed).
To gain a deeper insight into the non-equilibrium solidified microstructures, we performed electron backscatter diffraction (EBSD) characterization of as-printed SMAs. Reconstructed 3D views of the EBSD inverse pole figure (IPF) maps depict the spatially dependent grain structure features, including the grain morphology and crystal orientations (Fig. 2A). The microstructures of pristine SMAs mainly consist of elongated columnar grains across multiple molten pools along the build direction (BD). The presence of severe 〈001〉 and 〈101〉 orientations due to epitaxial growth in these coarse grains, exhibiting a strong typical 〈100〉//BD fiber texture (Fig. S7A), is also evidenced by XRD analysis (Fig. S19A). Although the rapid solidification rates associated with the LPBF-AM process are conducive to achieving refined microstructures, the easy growth directions of grains tend to correlate closely with the maximum temperature gradient of the melt pool owing to the need to balance the heat flux distribution.15 This phenomenon was commonly observed in BCC metals with poor thermal conductivity, particularly when subjected to temperature distribution restrictions characterized by repetitive thermal cycling.38 The resulting preferential solidification drives continued grain growth vertically through the partially melted layers and eventual dominance, which will inevitably exacerbate mechanical property anisotropy. Comparatively, it can be noticed that the grain structure and the relevant crystalline texture of our INSMA undergo a slight modulation and the orientation distribution is more random, although the epitaxial growth trend persists (Fig. 2A and Fig. S7B). Close examination of the microstructure reveals that the columnar growth of a small fraction of the B2 austenite grains was interrupted [side view along the transverse direction (TD)]. The reason is that the disturbing effect of the thermochemical reactions occurring in the molten pool on the Marangoni flow makes the grain growth orientation unaligned with the heat flow direction. Thus, the average grain sizes and aspect ratios of the INSMA are shifted towards lower values compared with the pristine SMA (Fig. S8).
We further present the resultant maps based on on-axial, high-precision transmission Kikuchi diffraction (TKD) observations to illustrate the dual-nanoprecipitation configuration at both the micro- and nanoscale (Fig. 2B, C and Fig. S7C, D). Phase maps show the dual-nanoprecipitates diffusely distributed in the B2 matrix, consistent with the TEM results (Fig. S3). Correspondingly, the image quality (IQ) plus grain boundary (GB) maps reveal the low-angle GBs (2° ≤ LAGBs ≤ 15°) between the dual-nanoprecipitates and the B2 matrix. The nearly zero lattice misfit is located in heterostructure regions because of the strong coherency, and their misorientation angles are below the minimum evaluated value (<2°). In addition, the kernel average misorientation (KAM) maps provide the localized misorientation distribution within the matrix grains. A brighter color indicates a greater orientation deviation from the reference value, which is defined as the average orientation of the grain. It is evident that high KAM values are predominantly concentrated surrounding the dual-nanoprecipitates, which are considered as rearrangement and intensive accumulation of interface dislocations.39 This observation indicates a positive correlation between KAM distribution and the fraction of LAGBs in non-equilibrium microstructures, along with evidence of reaching higher average levels in the INSMA relative to the pristine SMA (Fig. S9 and S10). This large number of LAGBs arising from dual-nanoprecipitation behaviors are directly responsible for dislocation multiplication in the parent phase. We attribute the emergence of interfacial dislocations in our INSMA to lattice misfit at the nanoprecipitate–B2 interface, which further develops into the dislocation walls (i.e., subgrain boundaries) constituted by large-scale mismatched dislocation networks in localized regions. The accumulation of stored distortion energy associated with these remarkable microstructural evolutions is advantageous for enhancing the mechanical properties and is expected to produce intense hetero-deformation-induced (HDI) strengthening and strain hardening.
Two different SMAs from our work were tested by quasi-static micropillar compression at a rated strain of 30% to compare their plastic stress–strain responses (Fig. 2D). In situ recorded load-displacement data were converted into nominal stress–strain curves to eliminate size-dependent errors. The INSMA we examined has an ultrahigh compressive strength (σmax) of 4.1 GPa and exhibited an extraordinary strain hardening capability during the plastic deformation stage. The substantial increase in deformation resistance (up to 2 GPa) primarily arises from Orowan mechanism-related dislocation avalanches during extrusion upsetting, which markedly surpass that of the pristine SMA. The uniaxial tensile and compressive test results of the printed macroscopic specimens of both the pristine SMA and INSMA at room temperature also show the advantage of the INSHE strategy (Fig. S40). One notable observation is the occurrence of non-uniform deformation characterized by a low slope strain plateau in the INSMA, accompanied by delayed yielding (Fig. 2D, top right inset, and Movie S1). We also found multiple crossover slip bands and bulges emerged at the surface of the micropillar after plastic yielding (Fig. S11A–C). In the absence of any pinning effect, the pristine SMA micropillar continuously slides and ultimately overflows the surface under elevated shear to develop a submicron-scale step (∼185 nm) (Fig. 2D, bottom right inset, and Movie S2). To elucidate the underlying synergistic deformation mechanism originating from the in-grain dual-nanoprecipitates, we examined the postmortem nanostructures of INSMA micropillars. Under large plastic deformation, we detected the shear-induced amorphization exemplarily found in previously studied nanocrystalline NiTi micropillars.40 The HRTEM observations suggest that the amorphous phase was formed in the region with strong plastic strain localization, whereas the polycrystalline phases with interface dislocations were formed in the less-strained region (Fig. S11D–G). Correspondingly, the masked FFT pattern revealed the coexistence of B2 austenite and B19′ martensite in the polycrystalline phases (Fig. S11G, inset). Except for amorphization, plenty of nanocrystallites generated by the dual-nanoprecipitate interacting with dislocation activities appear in the B2 matrix (Fig. S11H and I). They initially evolved from intensive lattice shearing within the dual-nanoprecipitates at dislocation avalanches.41 The formation of numerous nanocrystallites through crystalline fragmentation of dual-nanoprecipitates is a critical finding in the INSMA under extreme loading, as this mechanism not only allows them to accommodate severe deformation but also introduces ductility through sequential torsion with ongoing deformation.
To investigate the initial strain burst (‘pop-in’) phenomenon, we provide the critical stress (σs) and strain (εs) values related to slip banding, as shown in the engineering stress–strain curves in Fig. 2E. The results revealed that, unlike in the pristine SMA, the critical stress and strain required to induce the start of the strain burst in the INSMA were considerably increased, by approximately 124% and 100%, respectively. This observation was similar to the mechanical behavior of micropillars before yielding when subjected to a plastic strain of ∼30%, which collectively suggests an enhanced shear resistance by diffusely distributed dual-nanoprecipitates impeding dislocation movements (Movies S3 and S4). At a medium compressive strain of ∼12% reaching the strain burst point, we observed stacking slip bands close to 45° at the surface of the INSMA micropillar (Fig. 2E, top right inset, and Fig. S12A–C). The features of the associated slip-deformed matrix were uncovered using the inverse FFT (IFFT) image recorded along the reciprocal lattice vectors g(1
0) (Fig. S12G), which showed distorted lattice fringes and widespread dislocations in the B2 matrix. The shear-induced amorphization was not obvious (Fig. S12D–F) and the dual-nanoprecipitates therein maintained an intact crystalline structure (Fig. S12H and I), attributed to the dislocations having to overcome the high strength level of lattice distortions for further slip and penetration. These slip events are triggered by intermittent strain bursts, which are intrinsically contingent upon the unstable kinetic behaviors of the microscopic deformation activated after the stress-induced phase transformation from B2 austenite to B19′ martensite.42 Furthermore, the fatigue performances of the micropillars were evaluated by subjecting them to 104 cycles of compression under stress of 450 MPa (Fig. 2F and G). The pristine SMA showed prominent functional degradation, where the recoverable strain (εrec) decreased by 6.7% and the residual strain (εr) reached 4%, after 104 cycles of compression. The reduction in cyclic stability reflects the presence of reversible phase transformation induced dislocations that result from microscopic strain incompatibility at the moving phase boundaries (habit planes).43 Considering the relatively higher B19′ phase fraction in the pristine SMA's phase composition (Fig. S19), the reorientation of B19′ martensite variants during cyclic loading can serve as a contributing factor in the accumulation of residual strains. In contrast, under the same cyclic stress and cyclic period, we confirmed in the INSMA a larger hysteresis loop area (A) and a roughly halved residual strain, with negligible losses in deformation recovery and energy dissipation capabilities. At a low strain of ∼2% caused by fatigue, we detected the R phase, a typical transformation intermediate common in NiTi SMAs (Fig. S13D). The R phase's low strain characteristics, high reversibility, and stress-dispersing capability can significantly enhance the low-cycle fatigue life and cyclic stability, whereas the accumulation of concentrated dislocations at the R-phase/parent-phase interface and the superposition of multiphase transformations may exacerbate fatigue damage at the high-cycle stage. The surface of the INSMA micropillar remained very smooth throughout cyclic loading with no major difference from the just-fabricated state, and the postmortem nanostructure showed a few concentrated dislocations with a Burgers vector of a 〈001〉 contained within the monocrystalline B2 phase, as we confirmed by HRTEM images at the deformation stage of ∼12% strain (Fig. S13 and Movie S5). In particular, this suggests that the material is endowed with a more stable cyclic response, thereby making the actual fatigue life well exceed the achieved 104 cycles. Although in situ TEM under mechanical loading was not accessible, our postmortem TEM analyses at different deformation levels (Fig. S11–S13), combined with geometric phase analysis (GPA) based strain mapping (Fig. S5), provide indirect evidence that the coherent interfaces between dual-nanoprecipitates and the B2 NiTi matrix promote nanoscale deformation mechanisms that resist shear-induced amorphization and support the enhanced mechanical and functional performance of the INSMA.
Subsequently, we conducted high-speed nanoindentation mapping to assess the distribution and stability of the nanomechanical properties of SMAs (Fig. 3A–C). This high-throughput characterization approach allows for parsing the local variations in mechanical responses induced by dual-nanoprecipitation, while facilitating distribution statistics. Our INSMA exhibited significantly higher average hardness (H) and reduced Young's modulus (Er) values at a maximum applied load of 50 mN [as determined by continuous stiffness measurements (CSM), Fig. S14], compared to a more than two-fold increase in hardness even over the pristine SMA (4.94 ± 0.33 GPa versus 2.43 ± 0.19 GPa) (Fig. 3A and B). Moreover, we found that the hardness and reduced Young's modulus decreased with increasing indentation depth in the contact depth (hc) range of 100–1100 nm (Fig. 3C and Fig. S15). Such an indentation size effect revealed the dependence of the nanomechanical properties on the trial depth and can therefore be well described for their stability. Despite the distributions of the nanomechanical properties all tending to be homogeneous, the values measured in the INSMA were markedly more scattered (Fig. 3A). The differences in the indentation morphology at high magnification explained this observation (Fig. S16), attributed to the small size of dual-nanoprecipitates, which resulted in matrix mixing within the indentation volume. The ratio of hardness-to-reduced Young's modulus (H/Er) is an important characteristic value for analyzing the friction and wear behavior of superelastic materials.44 The H/Er ratio of the INSMA we examined reached 6.5 ± 0.2% compared to the pristine SMA (only 3.9 ± 0.8%), which is consistent with further tribological results (Fig. 3F, G and Fig. S17). The worn surface morphology indicated that INSMA's excellent wear resistance was derived from the formation of lubricating oxide films on its high hardness surfaces, which were typically characterized by an adhesive wear mechanism (Fig. S18). The synergistically enhanced resistance to plastic deformation plays a crucial role in inhibiting brittle microcrack extension, groove deepening and wear debris spalling. The dual-nanoprecipitates we introduced acted as reinforcements, substantially strengthening the SMA matrix, with reported values surpassing those of previous studies.45,46 In addition, the wearing properties of NiTi alloys are also largely affected by the unique transformation behavior. The wear resistance advantage of the INSMA arises from its super-elasticity emphasized by SIMT, which enables dynamic hardening and partially recoverable deformation, ultimately contributing to reduced wear rates. In contrast, the pristine SMA primarily resists wear through stress-induced reorientation of martensitic variants and twin boundary sliding, with the coordination between the SME and plastic deformation contributing relatively little to wear resistance. Electrochemical measurements consistently show that the surface-modified INSMA exhibits lower corrosion current density, higher polarization resistance, and a more stable passive film than pristine SMA. These results confirm its markedly enhanced corrosion resistance across open circuit potential (OCP), potentiodynamic polarization, and electrochemical impedance spectroscopy (EIS) analyses (see SI 12).
Utilizing the time-temperature superposition (TTS) principle,47 we explored the damping capacity (internal friction, tan
δ) of SMAs by stress relaxation at a low strain level of 0.02% (Fig. 3D). Due to the recovery stage of elastic deformation similar to the ‘clockwork’ release, the stored residual stresses decreased rapidly within the early ∼10 min dwell time and then leveled off. After the final relaxation at room temperature for 30 min, we detected the loss factor of the pristine SMA plummeted to 6.2 × 10−3. In contrast, the INSMA still maintained a rather high stress relaxation resistance (up to 7.6 × 10−3). The activation energy required for dislocation motion gradually decreases during residual stress release. The dislocation network pinned by the dual-nanoprecipitates in the microstructural configuration participates in energy dissipation via dislocation unpinning, gliding, and repinning, thereby contributing to the damping capacity. Meanwhile, the twin boundaries between variants and the austenite/martensite (A/M) phase boundaries induced by the earlier martensitic transformation undergo localized reorientation. The dual-nanoprecipitates located at these interfaces readily increase the frictional resistance to twin boundary migration and grain boundary sliding, which further improves internal friction. We further present the damping capacity variations recorded by strain sweeps at a frequency of 1 Hz over a strain amplitude range of 0–9 × 10−4 to illustrate the energy-absorbing characteristics during mechanical vibration, as shown by the curves consisting of correlated data points in Fig. 3E. Undoubtedly, the damping capacity of the INSMA shows a significantly increasing trend, especially at relatively large strain amplitudes (over 8 × 10−4), which is then nearly 2–3 times that of the pristine SMA. These distinct functional performances arise from a reversible martensitic transformation that occurs within its microstructural configuration. The increased mobility of internal boundaries facilitated the movement of boundaries under alternate stress to achieve sufficient dissipation of vibrational energy to the surrounding environment.48 Analysis of the literature reveals that our LPBF-AM as-printed state INSMA gives superior reported values for damping response over a wide strain range than the multicomponent and commercial Snoek-type high-damping alloys produced by traditional time-consuming and energy-intensive thermomechanical processes, e.g., melt-casting,49,50 forging,51 sintering,52 pressure infiltration,53,54 and post-treatment.55,56 In addition, we performed thermomechanical shape memory experiments within a low-temperature window in the martensitic state to illustrate the material's stress–strain-temperature responsive nature (Fig. 3H and I). The phase transformation temperatures (TTs) and enthalpies were accurately determined from differential scanning calorimetry (DSC) thermograms (Fig. S19 and Table S3). The INSMA displayed typical linear elastic behavior during high-stress forward loading at 203 K, whereas the pristine SMA prematurely converged to nonlinear deformation behavior (Fig. 3H). Indeed, no obvious nonlinearities similar to those mentioned above were developed when applying lower pre-strains (Fig. 3I). It should be emphasized that this difference in apparent loading-unloading behavior stems from the plastic deformation due to the low matrix strength in the pristine SMA. In the heating range from the martensitic transformation finish temperature (Mf) to the austenitic transformation finish temperature (Af), the unloaded residual strain undergoes a large-scale strain recovery by the reverse martensitic transformation (M to A) (Fig. S20). As a result, the INSMA was found to maintain a nearly ideal shape recovery rate (Rr) comparable to those of the majority of Ni-rich and near-equiatomic NiTi SMAs. As an important aspect of demonstrating the ability to memorize permanent shapes, a machined INSMA filament is mechanically deformed into a ‘paperclip’ in a high-temperature austenitic state (Fig. 3J). After removal of the deformation force allows fixing of this set shape, it is transferred back to room temperature which completes the programming step. After switching to any temporary shape, it was connected to a regulated DC circuit supplied by a source meter. It can be noticed that infrared temperature monitoring demonstrates that the heat transport resulting from the Joule heating effect actuated the paperclip to complete the programmed shape recovery within 110 s.
Given the synergistic strengthening potential offered by dual-nanoprecipitation, we have fabricated four types of shape-memory mechanical metamaterials (SMMMs) with representative topological microarchitectures by leveraging the flexibility of LPBF-AM. One prominent feature of these SMMMs is that their structural porosity decreases sequentially, while the relative density increases accordingly (Fig. S21). As shown in zoomed-in SEM images (Fig. 4A and Fig. S22), we examined an unprecedented printing fidelity in as-built SMMMs. The surface finish of the pristine SMA microlattices is suboptimal, with poorly fused powder particles adhering to both the nodes and struts, accompanied by several obvious nodules. This phenomenon must not be overlooked, as rough surfaces tend to become nucleation sites for cracks during deformation, leading to a substantial reduction in the material's damage-tolerant load-bearing capacity.57 To a certain extent, our INSMA counterparts provide a distinct advantage in printability, with deposited traces displaying an acceptable surface morphology and stable processed dimensions. We further conducted a quantitative analysis to assess dimensional accuracy by 3D surface profile measurements, which revealed that several surface roughness indicators were simultaneously reduced for the INSMA relative to the pristine SMA (Fig. S23 and Fig. S24E–G). It was also found that the surface roughness of SMMMs was positively correlated with their structural porosity. For printing of dense bulk materials, the formation of squamous discrete bands on the printed surface results from layer-by-layer stacking of molten pools under a continuously moving high-energy laser beam (Fig. S24A–D). The well-fused surface states of our INSMA caused a corresponding decrease in the contact angle (Fig. S25). To rigorously disentangle the respective contributions of physical and chemical factors to this phenomenon, additional XPS characterization (Fig. S42) and contact angle measurements (Fig. S43) were performed on both pristine SMA and INSMA samples after surface polishing. The survey and high-resolution XPS spectra (Ni 2p, Ti 2p, C 1s, and B 1s) revealed no significant differences in the chemical composition, elemental valence states, or surface energy components, and the contact angles of the two materials were nearly identical under smooth and flat surface conditions (∼52°). These findings indicate that the influence of chemical factors from surface modification by nanoparticles can be safely ruled out, thereby confirming that the reduced contact angle of the INSMA arises reliably from its substantially lower surface roughness compared to the pristine SMA, which directly accounts for the enhanced surface wettability and hydrophilicity (see SI 9). 3D visualization images reconstructed by microfocus computed tomography (micro-CT) further verified the feasibility of INSMA's overall optimization on internal quality (Fig. S26 and Movie S6). This observation contrasts strikingly with the manufacturing accuracy limitations in previous studies,58 which were particularly prevalent when forming complex spatial structures. We attribute the disappearance of powder adhesion and rough surface in our INSMA lattices to the elevated energy absorption efficiency of the functionalized powder under laser radiation coupled with the extended thermal history encountered during the thermochemical reaction (Fig. S33 and Table S2). Under the extreme non-equilibrium solidification conditions of L-PBF, the additional thermal effects resulting from the reduced laser reflectivity of the powder (down 46%) and the exothermic heat released from internal reactions (ΔfH0298 = −743.078 kJ mol−1) altered the temperature gradient distribution within the tiny melt pool. This leads to higher liquid-phase temperatures and longer residence times, which allows the alloy melt a sufficient time for smooth wetting and spreading. We also found that this prominent heat generation can compensate part of the laser heat source to avoid the detrimental effects by overheating evaporation due to high laser power density, which causes Ni element loss and surface balling. Consequently, the above behavior facilitates the elimination of powder adhesion and rough surface features caused by inadequate melting during the printing of high-resolution, intricately detailed complex spatial structures.
The mechanical properties of all as-printed SMMMs were further evaluated under cyclic and gradient loads with a maximum applied strain of 10%. The INSMA-type mechanical metamaterials we examined exhibited excellent strain recovery behaviors after 10 cycles of compression training, while providing higher strength versus pristine SMA-type (Fig. 4B and Fig. S27). These advantages are also quite obvious in the gradient stress–strain responses acquired with the maximum strain level increasing from 2% to 10% (Fig. 4C and Fig. S28). To demonstrate and scale up the potential applications of the designed INSMA, we carried out quantitative analysis on its unique mechanical response. Of particular note, the obtained stress–strain curves provided valuable information regarding the characteristic strains and characteristic energies. We found that as the maximum strain level or the number of cycles intensified, both the amelioration in the elastic recovery strain (εel) value and the elimination in the irreversible strain (εir) value of the INSMA greatly exceeded those of the pristine SMA, while the superelastic strain (εse) value differed little (Fig. S29). For instance, at a gradient strain level of 10%, the εel and εir values were determined to be 3.4% and 0.7%, respectively, for the pristine SMA and increased to 4.8% and decreased to zero for the INSMA, respectively. Based on this trend, Fig. 4D depicts in detail the positive correlation between the strain level and recoverability [i.e., the ratio of recoverable strain to total applied strain (εtot)]. Linear fitting of the scattering points stabilized at high strains revealed that the INSMA exhibited a higher slope of the fitted line, culminating in a 100% recoverability. These commendable characteristics are contingent upon the activation of correspondent variant pairs (CVPs), representing two twin-related martensitic variants,59 during cyclic phase transformation and grain reorientation. When the partially reoriented martensite induced to form by mechanical stress was stabilized by the multiplying activated dislocations, as reflected in the conventional SMAs, it resulted in retaining stabilized martensite that failed to be activated by free energy and elastic strain energy during the whole cyclic loading process.60,61 In addition, the quantitative results on the integral area in Fig. S30 showed that our INSMA still maintained its finite dissipated energy (Edissipated) with around twofold gain in absorbed energy (Eabsorbed). This facilitates an overall improvement in their energy storage efficiency [i.e., the ratio of absorbed energy to total energy (Etot)] and slows down the decreasing trend at high strains (Fig. 4E), which is well supported by the fatigue behavior observed under micropillar compression (Fig. 2F). Thus, unlocking the energy absorption characteristics of SMMMs actuated by cyclic phase transformation is indeed a notable achievement. We demonstrate an Ashby plot of energy absorption per unit volume versus density for the INSMA-type mechanical metamaterial in the present work and compared with other reported micro-/nanolattices62–64 and a wider range of functional materials65,66 (Fig. 4F and Fig. S41). To ensure transparency and improve the comparability of the Ashby plot, the detailed testing parameters (including the strain rate, number of cycles, and sample topology) of the comparative micro-/nanolattices are summarized in Table S7. To further ensure the reliability of the reported mechanical and functional properties, detailed statistical analyses were performed. The mean values and standard deviations of key parameters, including hardness, yield strength, compressive strength, energy absorption per unit volume, damping capacity, shape recovery rate, and other related metrics, are summarized in Fig. S46 and Table S10. These results confirm the reproducibility of the measured properties and provide a statistically robust basis for comparison. Generally, the energy absorption of our adaptive SMMM outperforms the majority of composites and technical ceramics with micro-/nanolattice architectures and surpasses these by 2–3 orders of magnitude when compared to some functional metallic materials with ductile structures (e.g., hollow Au, Ni–B, and Ag). An in-depth analysis of the specific energy absorption (SEA) as a critical application parameter suggested that the adaptive SMMM reached an unprecedented specific energy absorption of 25 J g−1, which broke through the well-known performance bottleneck of 1 J g−1 to 20 J g−1 for structural materials with low solid densities. Such resilience to energy absorption actuated by cyclic phase transformation is regarded as sustainable, together with the rarely observed multiple synergistic strengthening mechanisms unleashed by in situ dual-nanoprecipitation, thus promising to build upon by exploring the topological architectures for further well-designed and targeted adaptive materials.
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