3.1. Phase Composition of Powder Mixtures After Mechanical Activation
According to the results of phase analysis, powders of both compositions have a similar evolution pattern; the difference is observed only in the intensity of individual peaks (see 
Figure 3).
The diffraction patterns of the initial powder mixtures exhibit sharp, intense peaks corresponding to the metallic phases fcc-Ni (a ≈ 3.519 Å), hcp-Ti (a ≈ 2.950 Å, c ≈ 4.686 Å), and fcc-Cu (a ≈ 3.610 Å), indicating a high degree of crystallinity of the starting components.
After ~1 h of high-energy milling, the peaks of all components start to weaken and broaden, reflecting a reduction in the average crystallite size and an increase in microstrain caused by intensive plastic deformation during particle collisions. At 750 rpm, all Cu reflections and most Ti peaks disappear in all compositions examined; at 650 rpm, a similar disappearance of Cu is observed, with only a weak (111) Cu  reflection remaining, while several Ti peaks are still partially present.
The vanishing of Cu reflections and the systematic shift of Ni peaks to lower 2θ angles (increase in lattice parameter) indicate the dissolution of Cu in the Ni lattice and partial dissolution of Ti, leading to the formation of a supersaturated fcc-(Ni, Cu, Ti) solid solution. This is facilitated by the close atomic radii of Cu (≈1.28 Å) and Ni (≈1.24 Å) and the significantly larger radius of Ti (≈1.47 Å), making Cu highly soluble and Ti only partially soluble in fcc-Ni.
After ~3 h of mechanical activation at 650 rpm, the fcc-Ni and hcp-Ti reflections are still identified but strongly broadened; at 750 rpm, they transform into a diffuse halo, indicating progressive amorphization. This behavior occurs due to the accumulation of crystal defects—dislocations, stacking faults, and subgrain boundaries—which reduce diffusion distances and accelerate interdiffusion even under localized moderate heating.
After ~5 h of treatment at 650 rpm, weak peaks of NiTi intermetallics—high-temperature cubic B2 and martensitic monoclinic B19′—appear against the amorphous background. At 750 rpm, the formation of these peaks occurs earlier and more distinctly, as expected from the higher specific impact energy. By ~8 h, the intensities of the B2 and B19′ reflections increase in all compositions, indicating a growth in their volume fraction.
The effect of Cu becomes increasingly pronounced at the NiTi nucleation stage: the composition with 7 at.% Cu demonstrates earlier and more intense formation of B2/B19′ phases compared to 5 at.% Cu. This is consistent with the role of Cu in promoting interdiffusion and atomic ordering in the Ni–Ti–Cu system. The peak broadening throughout milling is attributed to the combined influence of coherent domain refinement and increasing lattice microstrain. The continuous shift of Ni peaks to lower 2θ values confirms lattice expansion due to the substitution of Ni atoms by larger Cu and partially by Ti.
Summary of the evolution during mechanical activation (5–7 at.% Cu).
Initial state: crystalline fcc-Ni, hcp-Ti, fcc-Cu.
1–3 h mechanical activation: dissolution of Cu in Ni, partial dissolution of Ti; formation of supersaturated fcc-(Ni, Cu, Ti); increase in microstrain; onset of amorphization (especially at 750 rpm).
~5 h mechanical activation: weak NiTi (B2/B19′) reflections appear on the amorphous background; at 750 rpm, they appear earlier and more pronounced.
~8 h mechanical activation: an increase in the B2/B19′ proportion in all compositions; at 7 at.% Cu, the phase formation rate is higher compared to 5 at.% Cu.
Thus, high-energy mechanical activation sequentially transforms the system from the initial metallic phases to a supersaturated fcc solid solution, then to a partially amorphous state, and finally to the nucleation and growth of NiTi intermetallics (B2/B19′). Furthermore, raising the Cu content from 5 to 7 atomic percent significantly speeds up all stages related to the formation of NiTi.
  3.2. Morphology and Phase State of Ni–45Ti–7Cu and Ni–45Ti–5Cu (at.%) Powders After Mechanical Alloying
Figure 4 presents SEM micrographs of the powders after mechanical activation at different milling conditions. Following preliminary mixing (2 h), a simple mechanical mixture of Ni, Ti, and Cu particles is observed, without noticeable fragmentation or interdiffusion; particle contact remains superficial and insufficient to initiate reaction or cold welding in the absence of high-impact energies [
32,
33,
34].
 Transitioning to MA regimes (650–750 rpm) initiates the typical “cold welding ⇄ fracturing” cycle, resulting in the formation of a lamellar or flake-like morphology and the appearance of neck-shaped bridges between compacted layers. Increasing the milling speed from 650 to 750 rpm significantly raises the collision energy, enhances defect accumulation (dislocations, stacking faults, subgrains), and shortens diffusion pathways. Consequently, particles become thinner, agglomerates more consolidated, and partial amorphization is increasingly detected in the powder mass [
35,
36,
37].
The 7 at.% Cu composition demonstrates more intensive and earlier plastic agglomeration compared to 5 at.% Cu, which is attributed to Cu acting as a softer phase—similar in size to Ni—and dissolving more readily into the Ni lattice. In XRD, this is reflected in the faster disappearance of Cu peaks (especially at 750 rpm) and a more pronounced shift of Ni reflections to lower 2θ values, confirming lattice expansion and the formation of a supersaturated fcc-(Ni, Cu, Ti) solid solution characterized by limited Ti solubility [
35,
36,
37].
With increasing milling time (1–8 h), the broadening of diffraction peaks becomes more distinct due to reduced coherent domain size and rising microstrain, while weak reflections of NiTi intermetallics (B2 and B19′) appear and intensify with time. These indicators of reaction-diffusion phase nucleation are more evident at 750 rpm and/or at 7 at.% Cu. At 650 rpm and 5 at.% Cu, longer treatment is required to reach a comparable state. The resulting morphology—thin lamellae with necks and dense agglomerates featuring high defect density—is consistent with published observations for NiTi(–Cu) powders, where increasing milling energy accelerates the transition from crystalline metallic phases to a partially amorphous matrix containing newly formed NiTi phases [
36,
37,
38]. 
Moreover, in Cu-containing NiTi powders, the martensitic transformation has been shown to shift toward a single-step B2 → B19 transition with considerably reduced hysteresis compared to binary NiTi (where B2 → B19′ dominates) [
30,
38]. Transformation temperatures depend strongly on Cu content. For gas-atomized Ti–Ni–Cu powders containing 5, 10, and 20 at.% Cu, reported Ms values are approximately −4.9, −17.6, and +32.1 °C, respectively, while (Af–Ms) decreases markedly with growing Cu content (from ~20 down to ~7 °C). These trends provide solid expectations for our compositions with 5–7 at.% Cu: a narrower hysteresis loop and earlier “maturation” of B2/B19 phases under comparable processing conditions [
30,
39,
40].
For subsequent SPS/U-FAST consolidation, such a lamellar, sheet-like, necked, and defect-enriched structure is advantageous: it reduces diffusion distances and lowers the energy threshold of reactions, thereby facilitating the attainment of high density at moderate sintering temperatures and promoting the formation of a “clean” functional response characteristic of one-step B2 → B19 kinetics. It is expected that Ni–45Ti–7Cu powders will exhibit a narrower hysteresis loop and better cyclic stability of functional properties compared to Ni–45Ti–5Cu, fully consistent with the trends reported for Ti–Ni–Cu powders and bulk materials in the literature.
Figure 5 shows SEM images of the same powder region at magnifications of ×5000 (scale bar 10 µm) and ×33,000 (scale bar 2 µm). At lower magnification ×5000, a polydisperse mixture of particles with pronounced bimodality is clearly visible: along with coarse cores (on the order of several microns), a large number of submicron-scale satellites are present, adhered to their surfaces. Interparticle necks and smoothed edges indicate cycles of cold welding and crushing, characteristic of mechanical alloying. This “core-satellite” morphology corresponds to a stage of intense surface activation and shortening of diffusion paths.
 At higher magnification (×33,000), the surface of a large particle exhibits a coarse-grained, “cauliflower-like” relief formed by aggregates on the nanometer–submicron scale (approximately 0.1–0.3 µm), with a system of shallow grooves and shear steps. The presence of numerous necks between nano-aggregates and micropores confirms intense plastic deformation and multicycle rewelding, leading to nanocrystallization/partial amorphization of the surface layer.
The results (see 
Table 3) of the powder particle analysis reveal three key findings.
First, during the early stages of milling, 7 at.% Cu accelerates the refinement of particles, resulting in smaller sizes by the 60th minute; this is consistent with the higher plasticity of the Ni–Cu-rich matrix and enhanced interdiffusion.
Second, the minimum average particle size is reached at around 300 min under all conditions; among these, 750 rpm produces the finest dispersion (7.97–8.32 µm).
Third, during prolonged milling (480 min), particle coarsening begins due to cold welding; however, this effect can be significantly mitigated by combining a higher rotation speed (750 rpm) with a higher Cu content (7 at.%).
After 8 h of mechanical activation, the average particle size increased noticeably, with large welded agglomerates reaching 20–27 µm compared to 8–10 µm after 3–5 h of milling. This growth is attributed to a shift from fracture-dominated refinement to cold welding and particle coalescence during prolonged milling, as highly deformed ductile surfaces tend to adhere upon repeated impacts. Such a transition from fragmentation to agglomeration has been widely reported in mechanically alloyed systems [
37,
38], including NiTi and NiTiCu alloys, where extended milling promotes the formation of welded clusters and changes in particle morphology. These observations are consistent with results and confirm that the increase in agglomerate size is a natural consequence of cold welding during long-term mechanical alloying.
From a practical standpoint, the optimal mode for minimizing particle size and suppressing subsequent coarsening is approximately 5 h at 750 rpm; if the priority is the fastest size reduction at early stages, the Ni–45Ti–7Cu composition also shows an advantage. The measurement errors are small (±0.004–0.11 µm), making the observed differences statistically reliable at a descriptive-comparative level. Consequently, for subsequent sintering work, samples milled for 5 h at 750 rpm were selected.
  3.3. Microstructure and Phase Composition of Composites of Ni-Ti-Cu Powder Mixtures
Figure 6 presents the X-ray diffraction patterns of the compact samples obtained by spark plasma sintering (SPS) at 900 °C from powders of Ni-45Ti-5Cu and Ni-45Ti-7Cu compositions (at.%), hereafter referred to as “5% Cu” and “7% Cu.” In both materials, the phases of the NiTi system are clearly identified: austenitic B2, martensitic B19′, and the Ni-rich intermetallic Ni
4Ti
3. The sharp and intense reflections indicate a high degree of ordering and recrystallization during SPS, consistent with the well-known enhancement of diffusion, localized Joule heating at particle contacts, and rapid neck formation under simultaneous pulsed current and applied pressure. As a result, sintering at 900 °C leads to the formation of a highly dense structure with predominant B2 austenite and a reduced fraction of secondary phases [
32].
 A comparison of the diffraction patterns reveals that in the 7% Cu sample, the relative intensity of B2 reflections is higher, whereas the B19′ and Ni
4Ti
3 peaks are noticeably suppressed compared with the 5% Cu sample. This trend aligns with the established role of copper as a stabilizer of the single-step B2 → B19 transformation in Ti–Ni–Cu alloys and its ability to reduce thermal hysteresis, in contrast to binary NiTi, which typically undergoes the B2 → B19′ transition with a wider hysteresis loop. Thus, Cu addition enhances chemical and phase homogeneity, promotes B2 formation, and reduces the precipitation of Ni-rich particles such as Ni
4Ti
3 [
30].
The presence of Ni
4Ti
3 in both samples is attributed to SPS processing kinetics: rapid heating and cooling, combined with transient nickel enrichment at interparticle interfaces, promote precipitation of Ni-rich intermetallics. However, with a higher Cu content (7 at.%), improved diffusion-driven homogenization suppresses their accumulation, which is reflected in the lower intensities of the corresponding reflections. According to published data on SPS-fabricated NiTi(–Cu) alloys, increasing the sintering temperature enhances the austenitic matrix and minimizes secondary phases such as Ni
3Ti, Ti
2Ni, and Ni
4Ti
3 due to more complete diffusion [
32]. The observed dominance of B2 at 900 °C is also fully consistent with earlier reports for SPS-processed NiTi/NiTiCu systems [
38], where elevated temperatures and pulsed current markedly accelerate densification and recrystallization, enabling high density (up to ~98% under comparable conditions) while effectively “cleaning” the matrix of excess phases.
Residual B19′ peaks after SPS at 900 °C are expected and may be associated with local internal stresses (including areas with residual porosity) and with the retention of part of the defective substructure not fully relieved during the short dwell time. Similar observations (the presence of austenite at room temperature and the transition to martensite upon cooling) have been reported for compact NiTi specimens after SPS [
31]. Additional increases in SPS temperature/time and/or a brief subsequent annealing generally further stabilize B2 and reduce the fraction of nickel-rich precipitates.
A semi-quantitative phase analysis was performed using the Rietveld refinement method (
Table 4), based on which the volume fractions of each phase were determined (in 
Figure 6).
The analysis revealed that both alloys comprise three primary phases: the high-temperature austenitic B2 phase, the martensitic B19′ phase, and the secondary Ni4Ti3 phase. In the alloy with 5 at.% Cu, the phase fractions were 29.7% B2, 42.6% B19′, and 27.7% Ni4Ti3. Increasing the Cu content to 7 at.% resulted in a higher proportion of the B2 phase (34.4%) and a reduction in both the B19′ (40.9%) and Ni4Ti3 (24.6%) phases. These results indicate that Cu addition stabilizes the B2 austenitic phase and suppresses the formation of Ni-rich secondary phases. This is consistent with the known role of Cu in enhancing phase homogeneity and reducing crystallographic incompatibility in Ni–Ti–Cu systems.
Scanning electron microscopy (SEM) micrographs of samples sintered by Spark Plasma Sintering (SPS) at 900 °C reveal significant microstructural differences between the Ni–45Ti–5Cu and Ni–45Ti–7Cu alloys (
Figure 7). At low magnification, the 5 at.% Cu alloy exhibits heterogeneous particle clusters, an incomplete interparticle neck network, and pronounced residual porosity. In contrast, the 7 at.% Cu alloy displays a more uniform structure with a well-developed neck network and predominantly closed micropores, indicating a higher degree of densification.
At higher magnification, the contrast is more evident. The 5 at.% Cu sample shows broken or narrow necks and a coarse matrix surface with scattered islands of small precipitates. Conversely, the 7 at.% Cu sample features continuous necks, a dense nanodispersed coating on the matrix surface, and isolated closed micropores. This microstructural evolution confirms that Cu increases the plasticity of the Ni-rich matrix and accelerates diffusion within the Ti–Ni–Cu system. This facilitates homogenization and the development of the B2 austenitic matrix during SPS, while reducing the tendency for Ni-rich precipitate accumulation (e.g., Ni
4Ti
3) and residual porosity. These trends align with published data on Ti–Ni–Cu powders and compacts, wherein Cu promotes a single-step B2 → B19 transformation with narrow thermal hysteresis compared to binary NiTi, and SPS enables high density and recrystallization at moderate temperatures [
31,
32,
38].
Scanning Electron Microscopy (SEM) analysis reveals that increasing the copper content from 5 to 7 at.% significantly improves consolidation during spark plasma sintering (SPS) at 900 °C. At low magnification, the 5 at.% Cu compact exhibits heterogeneous particle clustering, an underdeveloped network of interparticle necks, and visible residual porosity. In contrast, the 7 at.% Cu compact displays a more uniform architecture with a well-connected neck network and predominantly closed micropores.
At higher magnification, the 5 at.% Cu sample shows a coarse matrix surface with narrow or locally fractured necks, along with scattered small precipitates. The 7 at.% Cu sample, however, features continuous necks and a dense nanodispersed surface layer, indicative of enhanced diffusion and plastic flow within the Ni–Cu-rich matrix. Consequently, the 7 at.% Cu alloy achieves higher effective density and microstructural homogeneity, providing a more favorable foundation for stabilizing the B2 austenite phase and suppressing Ni-rich secondary phases after SPS.
Isolated unreacted Ti particles are also observed on the surface, which appear as rounded pits or cavities, likely where particles were dislodged during mechanical polishing and chemical etching. This effect is more pronounced in the 5 at.% Cu alloy, consistent with its less complete diffusional homogenization and a lower Ni–Ti interdiffusion rate compared to the 7 at.% Cu variant.
Following single-stage annealing, the microstructure of the 5 at.% Cu sample remains heterogeneous (
Figure 8a). It consists of recrystallized grains with blurred boundaries, chains of predominantly closed micropores, and localized particle clusters. The interparticle neck network is incomplete and locally interrupted, reflecting uneven densification after SPS and aging. On the matrix surface (
Figure 8b), fine-dispersed bright precipitates—identified as Ni
4Ti
3 particles formed during aging at ~350–500 °C—are visible. Isolated dark depressions from dislodged Ti-enriched particles and locally narrow or broken necks are also present.
In contrast, the microstructure of the 5 at.% Cu sample after three-stage annealing is markedly more uniform (
Figure 8c). It exhibits a coherent grain architecture with a well-defined necking network. Closed micropores predominate, alongside clear signs of homogenization and increased density. The number of bright Ni-rich precipitates is sharply reduced (
Figure 8d). The matrix relief is smoothed, with continuous necks and only sparse traces of spalling.
After single-stage annealing, the microstructure of the samples containing 7 at.% Cu is significantly more homogeneous than that of the 5 at.% Cu alloy (
Figure 9a). A well-developed, continuous network of interparticle necks is observed, with predominantly closed micropores and rounded, clearly defined grains. Small bright particles corresponding to Ni-rich precipitates are sparsely distributed within a smooth B2 matrix (
Figure 9b). The surface relief is uniform, signs of spalling are minimal, and porosity is low and mostly closed. These characteristics indicate enhanced diffusion and ductility of the Ni–Cu–rich matrix, which promotes more complete homogenization and compaction compared with the 5 at.% Cu alloy.
Transitioning to the three-stage treatment (900 °C solution annealing → water quenching → 300 °C stress-relief annealing) leads to a pronounced reduction in the fraction of bright Ni
4Ti
3 precipitates and further improves the uniformity of the grain structure (
Figure 9c,d). This behavior conforms to the known dissolution of Ni
4Ti
3 near 900 °C and the suppression of its re-precipitation due to rapid quenching, while subsequent low-temperature annealing relaxes internal stresses without entering the active aging range (≈350–500 °C). In SEM images, the evolution manifests as a transition from a fractured to a continuous neck network and as a decrease in both porosity and surface roughness. Based on earlier studies of Ti–Ni–Cu alloys, decreasing the density of Ni-rich precipitates and improving chemical homogeneity stabilizes the B2 austenite and promotes a single-step B2 → B19 transformation with reduced thermal hysteresis, particularly in Cu-alloyed systems.
Even after the simpler single-stage aging regime, the alloy containing 7 at.% Cu exhibits a more continuous interparticle bonding network and a more uniform microstructure than the 5 at.% Cu alloy. The three-stage heat treatment enhances these effects further by reducing secondary phases, smoothing the surface morphology, and lowering residual porosity.
The X-ray diffraction patterns of the Ni–45Ti–xCu (x = 5, 7 at.%) samples after heat treatments (
Figure 10) reveal a systematic shift in phase balance toward higher fractions of highly ordered B2 austenite and a suppression of Ni-rich Ni
4Ti
3 precipitates. Both higher Cu content and the use of the three-stage regime increase this effect.
After single-stage annealing (500 °C, 2 h), both compositions exhibit B2 and B19′ reflections, along with weak Ni4Ti3 peaks. For 7 at.% Cu, the B2 reflections are more intense and narrower (lower FWHM), whereas the B19′ and Ni4Ti3 contributions are diminished, indicating improved diffusion-driven homogenization and partial relaxation of internal stresses. In the 5 at.% Cu alloy, the stronger coexistence of B2 + B19′ and more noticeable Ni-rich precipitates correspond to higher residual microstrain and heterogeneity, as evidenced by peak broadening and an increased diffuse background.
The high-temperature step of the three-stage treatment at 900 °C results in dissolution of Ni4Ti3 and matrix recrystallization: B2 peaks narrow and increase in intensity, while B19′ reflections are nearly eliminated (most clearly in the 7 at.% Cu alloy). Rapid quenching preserves the supersaturated state, preventing re-precipitation of Ni-rich phases, whereas the subsequent 300 °C annealing relieves internal stresses without activating aging reactions. As a consequence, the alloy with 7 at.% Cu approaches a nearly single-phase B2 state. In contrast, the 5 at.% Cu alloy retains minor traces of martensite and exhibits localized reflections of the R-phase—commonly associated with lower Cu contents and incomplete stress relaxation.
Mechanistically, Cu acts via isomorphic substitution of Ni in the B2 sublattice, which reduces elastic incompatibilities at B2↔martensite interfaces and enhances interdiffusion. This shifts the transformation pathway toward a single-step B2 → B19 transition, narrows thermal hysteresis, and improves thermomechanical stability.
Overall, the combination of characteristics — increased B2 ordering, suppression of Ni4Ti3, and reduction of B19′/R-phase contributions — clearly shows that the Ni–45Ti–7Cu alloy subjected to the three-stage annealing achieves the most favorable phase state for enhanced functional performance. The 5 at.% Cu composition, in contrast, requires more intensive or longer diffusion treatments to fully suppress Ni-rich precipitates and residual martensite.
A semi-quantitative phase analysis was performed using the Rietveld refinement method (
Table 5) in order to determine the volume fractions of the structural components in the Ni–Ti–Cu alloys after different heat-treatment regimes (
Figure 10).
The obtained results show that both the Cu content and the annealing scheme have a pronounced effect on the phase composition. For the single-stage annealed samples, the 5 at.% Cu alloy contained 42.6% of the austenitic B2 phase, 39.8% of the martensitic B19′ phase, and 17.6% of the Ni4Ti3 phase. Increasing the Cu content to 7 at.% led to a higher fraction of the B2 phase (54.3%) and a reduction of B19′ (33.2%) and Ni4Ti3 (12.5%), indicating partial stabilization of the austenitic structure.
A significant transformation was observed after applying the three-stage heat-treatment scheme. In the 5 at.% Cu alloy, the B2 fraction increased to 80.7%, while the B19′ and Ni4Ti3 phases decreased sharply to 10.8% and 1.2%, respectively; additionally, a small amount of R-phase (7.3%) was detected. For the 7 at.% Cu alloy, the B2 phase became dominant (93.6%), and the fractions of B19′ (4.6%), Ni4Ti3 (0.4%), and R-phase (1.4%) were minimal. These results clearly demonstrate that the combination of increased Cu content and multistage annealing promotes the stabilization and homogenization of the B2 austenitic matrix while suppressing secondary Ni-rich and martensitic phases.
The decisive factor in achieving high B2-phase purity and suppressing Ni4Ti3 precipitation is the synergistic effect of combining 7 at.% Cu with the multistage annealing regime, as confirmed by a series of comparative experiments.
X-ray diffraction analysis shows that only under the combined influence of these two factors (7 at.% Cu + three-stage annealing) does the intensity of B2 reflections increase significantly, the B19′ peaks disappear to the background level, and the Ni4Ti3 signals become nearly absent. In samples with lower Cu content or when only heat treatment is applied without compositional optimization, pronounced Ni4Ti3 peaks and a two-phase B2+B19′ state persist.
Microstructural SEM data support this conclusion: in alloys containing 7 at.% Cu subjected to multistage annealing, a continuous neck network, minimal porosity, and an almost complete absence of bright Ni4Ti3 inclusions are observed. In contrast, alloys with lower Cu content or after single-stage annealing exhibit coarse Ni-rich precipitates and residual martensitic regions.
Thus, the XRD and SEM results unambiguously indicate that only the combined action of optimized Cu content and the three-stage heat treatment cycle creates the conditions necessary for forming a maximally homogeneous B2 matrix. Neither an increase in Cu beyond the optimal concentration nor heat treatment alone produces a comparable effect.