Journal of Aeronautical Materials (Dec 2016)

Thermal Simulation Test of AA-FGH95 Superalloy

  • WANG Xuqing1,
  • ZHANG Mincong,
  • LUO Junpeng,
  • PENG Zichao,
  • SHENG Junying,
  • YAN Jian

DOI
https://doi.org/10.11868/j.issn.1005-5053.2016.6.002
Journal volume & issue
Vol. 36, no. 6
pp. 9 – 14

Abstract

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The hot deformation behavior of AA-FGH95 superalloy was investigated by hot compressive tests on Gleeble-1500D thermal simulation test machine in different temperatures and strain rates. The true stress-strain curves were obtained, and based on the deformation data, the constitutive equation and processing map of FGH95 superalloy were built. The deformation active energy of AA-FGH95 is Q=695.78 kJ/mol. The results show that the simulated maximum stresses are in agreement with the experimental data, and the average error is about 6%. Based on the processing map, the safety processing parameters of 1070-1100℃ and 0.01-0.001 s-1 are confirmed. When the temperature reached 1100℃, the maximum strain rate increased to 0.5 s-1.

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