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

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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… Click to show full abstract

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 $\gamma '$ phases still maintain the cubic shape, but their size increases compared with the original microstructure. The values of $\sigma _{\mathrm{b}}$ , $\sigma _{0.2}$ , $\delta _{5}$ and $\psi $ 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 $\sigma _{\mathrm{b}}$ and $\sigma _{0.2}$ decrease obviously, while $\delta _{5}$ and $\psi $ 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.

Keywords: fatigue verification; lasting 2000; single crystal; crystal superalloy; mpa; mpa lasting

Journal Title: Mechanics of Time-dependent Materials
Year Published: 2021

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