TY - JOUR
T1 - The analysis and estimation of vibration fatigue for pipe fitting in aviation hydraulic system
AU - Zhang, Fuli
AU - Yuan, Zhaohui
AU - Zhang, F.
AU - Liang, Na
N1 - Publisher Copyright:
© 2019 Elsevier Ltd
PY - 2019/11
Y1 - 2019/11
N2 - In aviation hydraulic systems, the pipe always operates under vibration, high pressure and variable temperature conditions, which leads to pipe fatigue or even hydraulic system failure. Therefore, this paper proposes a method to analyze and evaluate the fatigue properties of pipe fittings. Firstly, based on the D'Alembert principle and force analysis, the forced vibration model of the pipe is established. Thermal stress is obtained by using the temperature field model and the thermal stress function. Furthermore, the coupled stress model of the pipe is built by the superposition principle. Secondly, the fatigue damage evolution model of the pipe fittings is established by using the fatigue damage mechanics and the coupled stress model. Finally, the above model was validated based on the bending fatigue platform and software COMSOL. The studies concluded that the experimental value of fatigue life is close to the theoretical value. Analysis and estimation models are effective. The stress is concentrated at the fixed end and distributed in the axial direction. As the stress increases, the fatigue life is shortened. The frequency change has little effect on fatigue life compared to pressure. The effect of temperature on fatigue is minimal. These studies provide a theoretical basis for the safety of hydraulic systems.
AB - In aviation hydraulic systems, the pipe always operates under vibration, high pressure and variable temperature conditions, which leads to pipe fatigue or even hydraulic system failure. Therefore, this paper proposes a method to analyze and evaluate the fatigue properties of pipe fittings. Firstly, based on the D'Alembert principle and force analysis, the forced vibration model of the pipe is established. Thermal stress is obtained by using the temperature field model and the thermal stress function. Furthermore, the coupled stress model of the pipe is built by the superposition principle. Secondly, the fatigue damage evolution model of the pipe fittings is established by using the fatigue damage mechanics and the coupled stress model. Finally, the above model was validated based on the bending fatigue platform and software COMSOL. The studies concluded that the experimental value of fatigue life is close to the theoretical value. Analysis and estimation models are effective. The stress is concentrated at the fixed end and distributed in the axial direction. As the stress increases, the fatigue life is shortened. The frequency change has little effect on fatigue life compared to pressure. The effect of temperature on fatigue is minimal. These studies provide a theoretical basis for the safety of hydraulic systems.
KW - Aviation hydraulic systems
KW - Fatigue lifetime estimation
KW - Pipe fittings
KW - Vibration fatigue
UR - https://www.scopus.com/pages/publications/85069647914
U2 - 10.1016/j.engfailanal.2019.07.038
DO - 10.1016/j.engfailanal.2019.07.038
M3 - 文章
AN - SCOPUS:85069647914
SN - 1350-6307
VL - 105
SP - 837
EP - 855
JO - Engineering Failure Analysis
JF - Engineering Failure Analysis
ER -