Design Simulation of the Low Fatigue Life of a Fan Blisk Using the Simulating Specimen Approach

Author:

Du Qing,Liu Yixiong,Zhang Jian,Guo Yong,Wu Yunwu

Publisher

Springer Singapore

Reference13 articles.

1. Liu, C.L.: Reliability analysis for an aero-engine turbine disk under low cycle fatigue condition. Acta Metallyrgica Sinica 17(4), 514–520 (2009)

2. Gan, L.P., Huang, G.Z., Zhu, S.P., et al.: Fatigue reliability analysis of turbine disk alloy using saddlepoint approximation. Int. J. Turbo Jet-Engines 30(3), 217–229 (2013)

3. Liu, T.Y., Geng, R., Zhang, J.F.: Design of simulated specimen for low-cycle fatigue of turbine engine disk. J. Aerosp. Power 23(1), 32–39 (2008). (in Chinese)

4. Zheng, X.M., Sun, Y.T., Yang, X.Y., Xiao, X.H., Liao, X.J.: Design of low cycle fatigue simulating specimen for bolt holes of a turbofan engine high pressure turbine. J. Aerosp. Power 33(10), 2351–2358 (2018). (in Chinese)

5. Li, D., Wang, Y.R., Liao, L.F., Wang, J.G., Wei, F.F.: Investigation of high and low cycle fatigue experiment for a curved dovetail assembly. Aeroengine 42(3), 61–66 (2016). (in Chinese)

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