This paper aims to reveal the effect of aging temperature on strength, impact toughness and fracture toughness of TC21 alloy with multi-level lamellar microstructure. The multi-level lamellar microstructures of TC21 alloy were prepared by solid solution at 1000 °C, annealing at 800 °C and respectively aging at 550 °C, 600 °C and 650 °C. The multi-level structures include β grains, α colony (αc), primary α phase (αp) and aged α plates (αs). The microstructures were performed on using optical microscope (OM), scanning electron microscope (SEM), transmission electron microscope (TEM), laser scanning confocal microscope (LSCM) and image analysis software. Results show that as aging temperature goes up, the size of αs increases and the segregation of alloy elements increases, while the β grain, grain boundary α phase (Gα) and αc almost remain unchanged. Hall-Petch formula is used to reveal that αs phase is the minimum control unit of strength. Fine grain strengthening, volume fraction of α phase (Vα) and element segregation have great influence on mechanical properties. In the impact experiment, microstructure deformation and secondary cracks consume more energy, while cleavage fracture consumes less energy. The TEM analysis found that the coordination of microstructure deformation became worse after aging. Fracture analysis shows that the size of αc plays an important role in crack propagation, and the crack propagation path always tends to cut αc vertically and pass through it. Whether the size of αc is large or small, it is not conducive to the increase of crack propagation path. Crack propagation path length and the interface energy consumed by different fracture mechanisms should be taken into consideration when there are more crack propagation paths and the fracture toughness decreases in the multi-level lamellar microstructure of TC21 alloy.
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