Lifetime Prediction of Turbine Blade of Turbocharger for Diesel Engine Based on Fatigue and Creep Damage Model

Jie Wang, Jingjing Zhang, Wei Zhao, Haiping Dong

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

To predict the lifetime of turbocharger turbine blades, a lifetime prediction method based on fatigue-creep damage is proposed. Firstly, by referring to diesel engines on armor vehicles bench test methods, the thermal-structural coupling of a radial turbine blade is analyzed by the finite element method. Based on the stress distribution characteristics of the turbocharger turbine blade, the root of the blade is identified as the dangerous area. Then, the fatigue-creep damage of the turbine blade is calculated and the lifetime is predicted by using the time-life fraction method. Last, the number of the turbine blade's failure cycles is predicted to be 2956 which are equivalent to 591200km mileage. The proposed method provides a reference basis for predicting the working lifetime of the turbine blades and improving their working reliability.

Original languageEnglish
Title of host publication2021 Global Reliability and Prognostics and Health Management, PHM-Nanjing 2021
EditorsWei Guo, Steven Li
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781665401302
DOIs
Publication statusPublished - 2021
Event12th IEEE Global Reliability and Prognostics and Health Management, PHM-Nanjing 2021 - Nanjing, China
Duration: 15 Oct 202117 Oct 2021

Publication series

Name2021 Global Reliability and Prognostics and Health Management, PHM-Nanjing 2021

Conference

Conference12th IEEE Global Reliability and Prognostics and Health Management, PHM-Nanjing 2021
Country/TerritoryChina
CityNanjing
Period15/10/2117/10/21

Keywords

  • Creep
  • Fatigue
  • Lifetime prediction
  • Thermal-structural coupling analysis
  • Turbine blade

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