Strength and modal analysis of aviation turbine based on ansys

Author: 
Yongyue Yuan

Turbine is an important component of aero-engine. Once a fault occurs, especially when the load exceeds the yield strength, the turbocharger will be damaged in a very short time. Therefore, the structural reliability analysis of turbocharger becomes more and more important. A simplified turbine model is established by Catia. The static strength of the model is analyzed based on ANSYS Workbench finite element analysis software. The distribution of stress and deformation is obtained, and the relationship between rotational speed and maximum stress is studied. In addition, the modal analysis of the model can obtain the natural frequencies and modes, which can provide the basis for the optimization design and dynamic analysis.

Paper No: 
2529