High cycle fatigue is the most common cause of failure in gas turbine engines. Different design tools have been developed to predict number of cycles to failure for a component subjected to fatigue loads. An energy-based fatigue life prediction framework was previously developed in recent research for prediction of axial and bending fatigue life at various stress ratios. The framework for the prediction of fatigue life via energy analysis was based on a new constitutive law, which states the following: the amount of energy required to fracture a material is constant. A finite element approach for uniaxial and bending fatigue was developed by authors based on this constitutive law. In this study, the energy expressions that construct the new constitutive law are integrated into minimum potential energy formulation to develop a new QUAD-4 finite element for fatigue life prediction. The newly developed QUAD-4 element is further modified to obtain a plate element. The Plate element can be used to model plates subjected to biaxial fatigue including bending loads. The new QUAD-4 element is benchmarked with previously developed uniaxial tension/compression finite element. The comparison of Finite element method (FEM) results to existing experimental fatigue data, verifies the new finite element development for fatigue life prediction. The final output of this finite element analysis is in the form of number of cycles to failure for each element in ascending or descending order. Therefore, the new finite element framework can predict the number of cycles to failure at each location in gas turbine engine structural components. The new finite element provides a very useful tool for fatigue life prediction in gas turbine engine components. The performance of the fatigue finite element is demonstrated by the fatigue life predictions from Al6061-T6 aluminum and Ti-6Al-4V. Results are compared with experimental results and analytical predictions.
Skip Nav Destination
ASME Turbo Expo 2010: Power for Land, Sea, and Air
June 14–18, 2010
Glasgow, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4401-4
PROCEEDINGS PAPER
A New Finite Element Approach to Biaxial Fatigue Life Prediction in Gas Turbine Engine
Wasim Tarar,
Wasim Tarar
National University of Sciences & Technology, Rawalpindi, Pakistan
Search for other works by this author on:
M.-H. Herman Shen
M.-H. Herman Shen
The Ohio State University, Columbus, OH
Search for other works by this author on:
Wasim Tarar
National University of Sciences & Technology, Rawalpindi, Pakistan
M.-H. Herman Shen
The Ohio State University, Columbus, OH
Paper No:
GT2010-23095, pp. 557-567; 11 pages
Published Online:
December 22, 2010
Citation
Tarar, W, & Shen, MH. "A New Finite Element Approach to Biaxial Fatigue Life Prediction in Gas Turbine Engine." Proceedings of the ASME Turbo Expo 2010: Power for Land, Sea, and Air. Volume 6: Structures and Dynamics, Parts A and B. Glasgow, UK. June 14–18, 2010. pp. 557-567. ASME. https://doi.org/10.1115/GT2010-23095
Download citation file:
15
Views
Related Proceedings Papers
Related Articles
Development of an Improved High Cycle Fatigue Criterion
J. Eng. Gas Turbines Power (January,2007)
Nonlinear Dynamic Analysis of Surface Mount Interconnects: Part I—Theory
J. Electron. Packag (March,1999)
An Equivalent Constitutive Model of Cancellous Bone With Fracture Prediction
J Biomech Eng (December,2020)
Related Chapters
Introduction and Definitions
Handbook on Stiffness & Damping in Mechanical Design
Fatigue Analysis in the Connecting Rod of MF285 Tractor by Finite Element Method
International Conference on Advanced Computer Theory and Engineering, 4th (ICACTE 2011)
Simple Structural Elements
Introduction to Plastics Engineering