基于临界面-损伤参量法的高压涡轮盘多轴疲劳寿命预测

doi:10.7527/S1000-6893.2018.21930

Abstract

Abstract: Multiaxial fatigue life prediction for a High Pressure Turbine (HPT) disc and a GH4169 alloy sample was performed using critical plane methods. Results show that the SWT (Smith-Watson-Topper) model can accurately predict uniaxial fatigue life, but demonstrates poor accuracy for multiaxial fatigue life prediction. The Fatemi-Socie (FS) model shows a good ability for uniaxial fatigue life prediction, but gives conservative multiaxial fatigue life predictions as it takes into account only the effect of the normal stress of the maximum shear strain amplitude plane on fatigue damage. In this paper, a new multiaxial fatigue critical plane-damage parameter model is proposed by considering the maximum shear strain amplitude as the main damage control parameter, and the correction parameter formed by normal stress/strain on the maximum shear strain amplitude plane as the second control parameter for fatigue damage prediction. Experimental data of a GH4169 alloy sample and an HPT disc show that the proposed damage parameter model can provide better predictions than the SWT, FS and Wang-Brown (WB) models.

Key words: critical plane methods, multiaxial fatigue, life prediction, turbine disc, damage parameter

CLC Number:

V215.5

XU Shen, ZHU Shunpeng, HAO Yongzhen, LIAO Ding. Multiaxial fatigue life prediction of an HPT disc based on critical plane-damage parameter[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 221930-221937.

References

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Multiaxial fatigue life prediction of an HPT disc based on critical plane-damage parameter

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