<p>TA15/AlSi10Mg functionally graded material (FGM) was produced via laser deposition manufacturing (LDM). The microstructural characteristics were analyzed using scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), and microhardness testing. This study clarified the regularities of phase changes and the mechanisms of crack formation within the graded interface. The TA15/AlSi10Mg FGM designed volume fraction gradient was as follows: Layer I: 100% TA15; Layer II: 75% TA15 + 25% AlSi10Mg; Layer III: 50% TA15 + 50% AlSi10Mg; Layer IV: 25% TA15 + 75% AlSi10Mg; Layer V: 100% AlSi10Mg. It was found that the primary phases in the TA15/AlSi10Mg FGM evolve along the gradient direction as follows: Ti(I) → Ti<sub>3</sub>Al(II) → TiAl + Ti<sub>5</sub>Si<sub>3</sub>(III) → TiAl<sub>2</sub> + TiAl + Ti<sub>5</sub>Si<sub>3</sub>(IV) → Al + Si(V). Cracks were observed in Layer IV. Macroscopic cracks initiated at the top surface of this layer and propagated downward, perpendicular to the deposition plane. Microcracks predominantly originated at the edges and tips of Ti<sub>5</sub>Si<sub>3</sub> precipitates. The formation of macroscopic cracks was primarily driven by transverse tensile stresses induced by constrained solidification in Layer IV. The core mechanism of microcrack formation was stress concentration around Ti<sub>5</sub>Si<sub>3</sub> precipitates, induced by accumulated residual tensile stress during cooling and subsequent thermal cycles after the deposition of Layer IV.</p>

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Microstructural Evolution and Crack Formation Mechanisms in TA15/AlSi10Mg Functionally Graded Material Fabricated by Laser Deposition Manufacturing

  • Bo He,
  • Jingbo Su,
  • Ting Wang,
  • Guang Yang

摘要

TA15/AlSi10Mg functionally graded material (FGM) was produced via laser deposition manufacturing (LDM). The microstructural characteristics were analyzed using scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), and microhardness testing. This study clarified the regularities of phase changes and the mechanisms of crack formation within the graded interface. The TA15/AlSi10Mg FGM designed volume fraction gradient was as follows: Layer I: 100% TA15; Layer II: 75% TA15 + 25% AlSi10Mg; Layer III: 50% TA15 + 50% AlSi10Mg; Layer IV: 25% TA15 + 75% AlSi10Mg; Layer V: 100% AlSi10Mg. It was found that the primary phases in the TA15/AlSi10Mg FGM evolve along the gradient direction as follows: Ti(I) → Ti3Al(II) → TiAl + Ti5Si3(III) → TiAl2 + TiAl + Ti5Si3(IV) → Al + Si(V). Cracks were observed in Layer IV. Macroscopic cracks initiated at the top surface of this layer and propagated downward, perpendicular to the deposition plane. Microcracks predominantly originated at the edges and tips of Ti5Si3 precipitates. The formation of macroscopic cracks was primarily driven by transverse tensile stresses induced by constrained solidification in Layer IV. The core mechanism of microcrack formation was stress concentration around Ti5Si3 precipitates, induced by accumulated residual tensile stress during cooling and subsequent thermal cycles after the deposition of Layer IV.