Finite Element Prediction of the Cracking Tendency of a Laser Metal Forming Process for the Repair of High Temperature Turbine Blades

Canadian Institute of Mining, Metallurgy and Petroleum
F. Fournier Dit Chabert F. Tancret R. Le Gall J. François Castagné
Organization:
Canadian Institute of Mining, Metallurgy and Petroleum
Pages:
14
File Size:
1356 KB
Publication Date:
Jan 1, 2006

Abstract

During the repair of turbine blades by a laser cladding process, it is observed that interdendritic cracking occurs in the heat affected zone (HAZ). Auger electron spectroscopy, performed on sample broken at high temperature, reveals interfacial sulfur segregation, which is known to be one of the main causes of microcraking in the HAZ during welding processes. Moreover, thermal gradients generated by the process are responsible for important thermomechanical stresses. In the present work, the finite element code Comsol Multiphysics is used to simulate the laser cladding process in order to determine both the thermal field and, using an elastoplastic law, the stress field inside the component. The originality is that the temperature history calculated in the thermomechanical model is extracted then injected in a segregation model in order to calculate the local segregation behavior. This model can be eventually used to predict the risk of cracking as a function of process parameters and alloy chemistry.
Citation

APA: F. Fournier Dit Chabert F. Tancret R. Le Gall J. François Castagné  (2006)  Finite Element Prediction of the Cracking Tendency of a Laser Metal Forming Process for the Repair of High Temperature Turbine Blades

MLA: F. Fournier Dit Chabert F. Tancret R. Le Gall J. François Castagné Finite Element Prediction of the Cracking Tendency of a Laser Metal Forming Process for the Repair of High Temperature Turbine Blades. Canadian Institute of Mining, Metallurgy and Petroleum, 2006.

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