HE Chen, LI Jiadong, WANG Junhao, ZHAO Yuhui, ZHAO Jibin, WANG Zhiguo, HE Zhenfeng
High-strength 7075 aluminum alloy exhibits several disadvantages, including low laser absorption, high laser reflectivity, high thermal conductivity, and a strong tendency toward oxidation. Furthermore, it contains a significant number of low-boiling-point alloying elements and demonstrates a pronounced susceptibility to hot cracking. These factors lead to oxidation of the alloy, volatilization of low-boiling-point elements, pore formation, thermal cracking, warping deformation, and heat-affected zones during laser repair, thereby resulting in reduced mechanical properties of the repaired components. To enhance the mechanical properties in the repair region of 7075 aluminum alloys, laser melting deposition technology was employed in combination with (Ti + B4C) / AA7075 aluminum alloy composite powder. The repaired samples were subsequently treated using a sintering furnace (KSL-1700X) and a vacuum furnace (VBF-1200X). The strengthening of the repaired region was achieved through solution treatment followed by single-stage aging. The effects of various aging durations on the microstructure and mechanical properties of the samples were systematically investigated. The results indicated that solution treatment followed by single-stage aging significantly improved the compositional uniformity of both the repair zone and the heat-affected zone. The process facilitated the phase transition from TiAl3 to Ti3Al in the repair region, thereby enhancing the mechanical properties of the samples. Moreover, heat treatment effectively refined the grain structure in the heat-affected zone, which contributed to improved microhardness and tensile strength in that region. As the aging time increased from 0 h to 6 h, the average microhardness of the repair area was measured at 130.75, 136.93, 142.22, and 149.38 HV, respectively. Correspondingly, the average microhardness of the substrate was recorded as 96, 155.67, 156.88, and 164.28 HV. These findings demonstrated that increasing the aging time led to a continuous increase in hardness in both the repair zone and the substrate, with the substrate showing a significantly higher rate of hardness improvement compared to the repair area. This disparity is attributed to the fact that the 7075 aluminum alloy is a heat-treatable, high-strength aluminum alloy. Following solution treatment, alloying elements such as Zn and Mg, which were originally present in insoluble heterogeneous phases, were transformed into a supersaturated solid solution. During aging, fine η (MgZn2) precipitates formed within the substrate, resulting in increased hardness. In contrast, within the repair area, Zn and MgZn2 present in the aluminum-based repair powder were partially lost during laser repair, thereby diminishing the formation of the η (MgZn2) phase during aging. Additionally, the fine TiAl phase originally present in the repair region transformed into a dendritic Ti3Al phase during heat treatment. Although Ti3Al exhibits high strength, its grain refinement capability is weaker, thereby resulting in a smaller overall hardness increase in the repair area compared to the substrate. As aging time increased from 0 h to 6 h, the tensile strength of the samples improved progressively, with recorded values of 329.59, 372.17, 422.12, and 436.30 MPa, respectively. Compared to the non-heat-treated condition, this represents a 32.4% increase in tensile strength. However, the elongation decreased to 6.86%, 4.23%, 2.86%, and 2.27%, respectively, with the fracture mode characterized as brittle fracture. This behavior is attributed to the gradual transformation of TiAl3 into the stronger yet more brittle Ti3Al phase in the repair region during heat treatment, thereby increasing tensile strength while reducing toughness. With increasing aging time, the width of the grinding marks on the sample surface did not change significantly; however, the depth of the marks progressively decreased from approximately 25 µm (in the untreated condition) to 10 µm after 6 h of aging. This indicates that the dense distribution of the Ti3Al phase precipitated during heat treatment contributes to enhanced wear resistance of the aluminum matrix. After 1 h of solution treatment and 6 h of aging, the mechanical properties of the samples reached optimal levels. Under these conditions, the microhardness and tensile strength of the samples reached approximately 80% of those of forged 7075 aluminum alloy. Compared with the untreated condition, the microhardness of the substrate and repair area increased by 12.7% and 69.1%, respectively. The tensile strength increased by 32.4%, and the wear rate decreased from 10.4 × 10⁻5 mm3·N⁻1·m⁻1 to 4.63 × 10⁻5 mm3·N⁻1·m⁻1, reflecting significant improvement in wear resistance.