Journal of Aeronautical Materials (Aug 2016)

Creep Rupture Life Prediction Based on Analysis of Large Creep Deformation

  • YE Wenming,
  • HU Xuteng,
  • MA Xiaojian,
  • SONG Yingdong

DOI
https://doi.org/10.11868/j.issn.1005-5053.2016.4.011
Journal volume & issue
Vol. 36, no. 4
pp. 78 – 83

Abstract

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A creep rupture life prediction method for high temperature component was proposed. The method was based on a true stress-strain elastoplastic creep constitutive model and the large deformation finite element analysis method. This method firstly used the high-temperature tensile stress-strain curve expressed by true stress and strain and the creep curve to build materials' elastoplastic and creep constitutive model respectively, then used the large deformation finite element method to calculate the deformation response of high temperature component under a given load curve, finally the creep rupture life was determined according to the change trend of the responsive curve.The method was verified by durable test of TC11 titanium alloy notched specimens under 500 ℃, and was compared with the three creep rupture life prediction methods based on the small deformation analysis. Results show that the proposed method can accurately predict the high temperature creep response and long-term life of TC11 notched specimens, and the accuracy is better than that of the methods based on the average effective stress of notch ligament, the bone point stress and the fracture strain of the key point, which are all based on small deformation finite element analysis.

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