An Advanced Creep Model Allowing for Hardening and Damage Effects

:  In this work an original creep prediction model is presented with a unified comprehensive formulation with primary, secondary and tertiary stages for variable stresses and temperature fields. The creep model is implemented in the ANSYS FEM code, using the Fortran subroutine usercreep, specifically suited for the cases examined, in order to assess the material behaviour more accurately than that provided by the mono-dimensional approach. Furthermore, the residual stresses that arise from thermo-mechanical loading and unloading cycles, under the temperature-dependent bilinear elastic–plastic hypothesis, are considered. In order to validate the model proposed, an investigation into the final stages of turbine blade is presented and discussed. The nonlinear properties of the material are taken from an industrial context and the literature. In addition to the temperature dependence of the properties of the material, geometric nonlinearities are also considered. The material adopted for model calibration is a polycrystalline Ni-based superalloy. Load conditions used in the simulations are obtained using a computational fluid dynamics (CFD) analysis under working conditions provided by industrial research and the constraints modelled are representative of the real joining condition of the blade. Finally, the simulation results are compared with those obtained by the Norton–Bailey prediction model.

[1]  Albrecht Bertram,et al.  Anisotropic creep modelling of the single crystal superalloy SRR99 , 1996 .

[2]  Thomas H. Hyde,et al.  Prediction of creep failure in aeroengine materials under multi-axial stress states , 1996 .

[3]  Modelling of the mechanical behaviour of the single-crystal turbine alloy CMSX-4 during thermomechanical loading , 2000 .

[4]  Rolf Mahnken,et al.  Creep simulation of asymmetric effects at large strains by stress mode decomposition , 2005 .

[5]  M. Maldini,et al.  Modelling creep of single crystal CM186LC alloy under constant and variable loading , 2005 .

[6]  Holm Altenbach A NONCLASSICAL MODEL FOR CREEP-DAMAGE PROCESSES , 2001 .

[7]  Rolf Mahnken,et al.  Anistropic creep modeling based on elastic projection operators with applications to CMSX-4 superalloy , 2002 .

[8]  Th.B. Kermanidis,et al.  A three‐dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading , 2001 .

[9]  A. Zolochevsky,et al.  A creep damage model for initially isotropic materials with different properties in tension and compression , 1998 .

[10]  Brian Dyson,et al.  Use of CDM in Materials Modeling and Component Creep Life Prediction , 2000 .

[11]  Seyed Mojtaba Zebarjad,et al.  Tensile deformation mechanisms at different temperatures in the Ni-base superalloy GTD-111 , 2004 .

[12]  Ashok Saxena,et al.  Creep deformation and rupture behaviour of directionally solidified GTD 111 superalloy , 2006 .

[13]  Peter E. McHugh,et al.  Modelling of creep in a Ni base superalloy using a single crystal plasticity model , 1997 .

[14]  R. Reed,et al.  Creep of CMSX-4 superalloy single crystals: effects of rafting at high temperature , 1999 .

[15]  M. Yaguchi,et al.  A viscoplastic constitutive model for nickel-base superalloy, part 2: modeling under anisothermal conditions , 2002 .

[16]  Holm Altenbach,et al.  Topical Problems and Applications of Creep Theory , 2003 .