The plastic strengthening effect after long-term endurance and fatigue verification of aero-engine turbine blade single crystal superalloy

The elastoplastic behaviors of a nickel-based single crystal superalloy at 760 °C, 927 °C and 1100 °C were studied, respectively, after 815 °C/250 MPa lasting for 2000 h, 927 °C/205 MPa lasting for 2000 h and 1100 °C/30 MPa lasting for 1000 h. After 815 °C/250 MPa lasting for 2000 h, the γ^′ phases still maintain the cubic shape, but their size increases compared with the original microstructure. The values of σ_b, σ_0.2, δ₅ and ψ increase. The tensile fracture surface is 45° with the [001] direction and the fracture mechanism is octahedral slip. After 927 °C/205 MPa lasting for 2000 h and 1100 °C/30 MPa for 1000 h, N-type plate-like rafting structure formed, and the latter owns a higher degree. The values of σ_b and σ_0.2 decrease obviously, while δ₅ and ψ basically are unchanged. The mechanism is the mixed fracture of octahedral slip and I-type. The fatigue verification test and simulation further prove the strengthening effect.