Probabilistic-based design can efficiently quantify the risk and improve the reliability of the turbine blade. In this context, a probabilistic framework concerning the uncertainty quantification for the turbine blade’s TMF life based on the cyclic damage accumulation (CDA) method and Bayesian inference is proposed in this study. Firstly, the damage factors in the critical plane are obtained by the finite element method using Walker constitutive model, during which the discretization error is calibrated using Richardson extrapolation method. After that, the probabilistic TMF life model is established using CDA theory, in which the uncertainty of the material parameters is quantified using Bayesian inference. Finally, TMF life prediction on a single crystal nickel superalloy turbine blade is conducted using the probabilistic framework considering uncertainty quantification. The accuracy and validity of the proposed method is revealed by the comparison between the numerical and experimental results of real turbine blades.
Skip Nav Destination
ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5113-5
PROCEEDINGS PAPER
Probabilistic TMF Life Evaluation of a Single Crystal Turbine Blade Concerning Uncertainty Quantification
Rongqiao Wang
Rongqiao Wang
BeiHang University, Beijing, China
Search for other works by this author on:
Xi Liu
BeiHang University, Beijing, China
Dianyin Hu
BeiHang University, Beijing, China
Bin Zhang
BeiHang University, Beijing, China
Rongqiao Wang
BeiHang University, Beijing, China
Paper No:
GT2018-75927, V07AT32A007; 7 pages
Published Online:
August 30, 2018
Citation
Liu, X, Hu, D, Zhang, B, & Wang, R. "Probabilistic TMF Life Evaluation of a Single Crystal Turbine Blade Concerning Uncertainty Quantification." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 7A: Structures and Dynamics. Oslo, Norway. June 11–15, 2018. V07AT32A007. ASME. https://doi.org/10.1115/GT2018-75927
Download citation file:
30
Views
0
Citations
Related Proceedings Papers
Related Articles
Improved Performance Rhenium Containing Single Crystal Alloy Turbine Blades Utilizing PPM Levels of the Highly Reactive Elements Lanthanum and Yttrium
J. Eng. Gas Turbines Power (January,1999)
Development and Turbine Engine Performance of Three Advanced Rhenium Containing Superalloys for Single Crystal and Directionally Solidified Blades and Vanes
J. Eng. Gas Turbines Power (July,1998)
Critical Plane Fatigue Modeling and Characterization of Single Crystal Nickel Superalloys
J. Eng. Gas Turbines Power (April,2004)
Related Chapters
Advances in the Stochastic Modeling of Constitutive Laws at Small and Finite Strains
Advances in Computers and Information in Engineering Research, Volume 2
Crystal Orientation Optimization of Nickel-Based Single Crystal Turbine Blade
International Conference on Optimization Design (ICOD 2010)
A PSA Update to Reflect Procedural Changes (PSAM-0217)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)