Fatigue Life and Crack Initiation of K and N Type Jacket Structure Using 3D Fatigue FE Analysis

Authors

  • Zhen-Ming Wang
    Affiliation
    Department of Civil, Environment and Plant Engineering, Chung-Ang University, 84 Heukseok-ro, Dongjak-gu, Seoul 06974, Republic of Korea
  • Kyong-Ho Chang
    Affiliation
    Department of Civil, Environment and Plant Engineering, Chung-Ang University, 84 Heukseok-ro, Dongjak-gu, Seoul 06974, Republic of Korea
  • Mikihito Hirohata
    Affiliation
    Department of Civil Engineering, School of Engineering, Osaka University, 2–1 Yamadaoka, Osaka 565–0871, Japan
https://doi.org/10.3311/PPci.23474

Abstract

Jacket structures are widely used as foundation structures for offshore wind energy. The jacket structure as a truss shape structure is not deformed easily and has the advantage of keeping the structure stable under wind load. The offshore jacket structures are subjected to unstable repetitive loads such as wind, and wave loads in the deep sea. These harsh environments lead to the deterioration of material performance and fatigue failure with cracks in the structure. It is crucial to locate fatigue cracks since they might compromise a structure's overall stability.
In this study, fatigue life and crack initiation for different braced jacket structures were investigated. First, 3D non-steady heat conduction analysis and thermal elastic-plastic analysis were performed to reproduce the initial state of the weld joint in the jacket structure. The heat history obtained from the 3D non-steady heat conduction analysis was enforced as an input in thermal elastic-plastic analysis to calculate welding deformation and residual stress. Next, the fatigue FE analysis of the jacket welding structure was carried out using the residual stress and welding deformation as initial values along with the external cyclic loadings. The 3D fatigue FE analysis employed cyclic hysteresis constitutive equations and fatigue damage theory to calculate the fatigue life and crack initiation. The 3D fatigue FE results were compared with the S-N curve by European code 3 and the hot spot stress (HSS) method. The results show that the 3D fatigue FE method effectively calculates the fatigue life and finds crack initiation.

Keywords:

jacket structure, truss structure, residual stress, fatigue life, fatigue crack initiation, 3D fatigue FE analysis

Citation data from Crossref and Scopus

Published Online

2024-04-25

How to Cite

Wang, Z.-M., Chang, K.-H., Hirohata, M. “Fatigue Life and Crack Initiation of K and N Type Jacket Structure Using 3D Fatigue FE Analysis”, Periodica Polytechnica Civil Engineering, 68(3), pp. 883–891, 2024. https://doi.org/10.3311/PPci.23474

Issue

Section

Research Article