CRITICAL PLANE BASED MULTI-AXIAL FATIGUE METHOD IN FREQUENCY DOMAIN

    公开(公告)号:US20240362379A1

    公开(公告)日:2024-10-31

    申请号:US18309292

    申请日:2023-04-28

    申请人: FCA US LLC

    IPC分类号: G06F30/23

    CPC分类号: G06F30/23 G06F2111/10

    摘要: A method for predicting fatigue life of a structure includes providing a finite element (FE) model of the structure; calculating a modal stress and a frequency response function (FRF) of the FE model; calculating a stress power spectral density (PSD) matrix; calculating a damage transformation matrix [A]; calculating a covariance matrix from the stress PSD matrix; determining angles θ, φ, and ψ in a plane with maximum equivalent variance based on the calculated covariance matrix; and calculating a variance—damage parameter with the angles θ, φ, and ψ incremented in a predetermined amount of degrees to thereby identify critical planes where a fatigue crack will occur in the structure.