Fatigue Life Prediction of Fan Blade Using Nominal Stress Method and Cumulative Fatigue Damage Theory

References

1. Xu C. Gas turbine engine. Beijing: Weapon Industry Press, 2006.Search in Google Scholar

2. Lv Z, Huang HZ, Gao H, Zuo FJ, Wang HK. Lifetime prediction for turbine discs based on a modified Walker strain model. J Mech Sci Technol 2015;29(10):4143–4152.10.1007/s12206-015-0908-1Search in Google Scholar

3. Huang HZ, Cui P, Peng W, Gao H, Wang HK. Fatigue lifetime assessment of aircraft engine disc via multi-source information fusion. Int J Turbo Jet Engines 2014;31(2):167–174.10.1515/tjj-2013-0043Search in Google Scholar

4. Huang HZ, Gong J, Zuo MJ, Zhu SP, Liao Q. Fatigue life estimation of an aircraft engine under different load spectrums. Int J Turbo Jet Engines 2012;29(4):259–267.10.1515/tjj-2012-0017Search in Google Scholar

5. Gan L, Huang HZ, Zhu SP, Li YF, Yang Y. Fatigue reliability analysis of turbine disk alloy using saddlepoint approximation. Int J Turbo Jet Engines 2013;30(3):217–230.10.1515/tjj-2013-0020Search in Google Scholar

6. Li YF, Huang HZ, Liu Y, Xiao N, Li H. A new fault tree analysis method: Fuzzy dynamic fault tree analysis. Eksploatacja I Niezawodnosc – Maintenance and Reliability 2012;14(3):208–214.Search in Google Scholar

7. Li YF, Lv Z, Cai W, Zhu SP, Huang HZ. Fatigue life analysis of turbine disks based on load spectra of aero-engines. Int J Turbo Jet Engines 2016;33(1):27–33.10.1515/tjj-2015-0004Search in Google Scholar

8. Peng Z, Huang HZ, Wang HK, Zhu SP, Lv Z. A new approach to the investigation of load interaction effects and its application in residual fatigue life prediction. Int J Damage Mech 2016;25(5):672–690.10.1177/1056789515620910Search in Google Scholar

9. Peng Z, Huang HZ, Zhu SP, Gao H, Lv Z. A fatigue driving energy approach to high-cycle fatigue life estimation under variable amplitude loading. Fatigue Fract Eng Mater Struct 2016;39(2):180–193.10.1111/ffe.12347Search in Google Scholar

10. Zuo FJ, Huang HZ, Zhu SP, Lv Z, Gao H. Fatigue life prediction under variable amplitude loading using a non-linear damage accumulation model. Int J Damage Mech 2015;24(5):767–784.10.1177/1056789514553042Search in Google Scholar

11. Lv Z, Huang HZ, Zhu SP, Gao H, Zuo F. A modified nonlinear fatigue damage accumulation model. Int J Damage Mech 2015;24(2):168–181.10.1177/1056789514524075Search in Google Scholar

12. Li N. Turbocharger compressor blade static and dynamic characteristics research and optimize design. Dalian: Dalian Jiaotong University, 2007.Search in Google Scholar

13. Li CW, Sun Q, Yin BJ, Chen DL, Zhang ZP. An approximate calculation of aerodynamic load for a certain type of aero-engine compressor blade. J Air Force Eng Univ (Natural Science Edition) 2004;5(4):1–3.Search in Google Scholar

14. Wang WG. Research on prediction model for disc LCF life and experiment assessment methodology. Nanjing: Nanjing University of Aeronautics and Astronautics, 2006.Search in Google Scholar

15. Wang XL. Research on Uncertain methods for fatigue life prediction. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009.Search in Google Scholar

16. Yuan X, Li SM. Research status and development of forecast method of fatigue life. Aeronaut Manuf Technol 2005;(12):80–85.Search in Google Scholar

17. Li YF, Zhu SP, Li J, Peng W, Huang HZ. Uncertainty analysis in fatigue life prediction of gas turbine blades using Bayesian inference. Int J Turbo Jet Engines 2015;32(4):319–324.10.1515/tjj-2014-0037Search in Google Scholar

18. Lu X, Zheng SL. Experimental investigation on cumulative fatigue damage of strengthening under low amplitude loading for automobile structures. China Mech Eng 2007;18(8):994–997.Search in Google Scholar

19. Marco SM, Starkey WL. A concept of fatigue damage. ASME Trans 1954;76(4):627–632.10.1115/1.4014922Search in Google Scholar

20. Lin JW, Zhang JH, Zhang GC, Yang S, Gao HH. Study on fatigue damage of aero-engine blade based on non-linear continuum damage model. J Mech Eng 2010;46(18):66–70.10.3901/JME.2010.18.066Search in Google Scholar