Eigenfrequency analyses of laser-welded web core sandwich panels

被引:30
|
作者
Jelovica, J. [1 ]
Romanoff, J. [1 ]
Klein, R. [1 ]
机构
[1] Aalto Univ, Sch Engn, Dept Appl Mech, POB 12200, Aalto 00076, Finland
关键词
Eigenfrequency; Laser-weld; T-joint; Sandwich; Web-core; Steel; Orthotropic; FORCED VIBRATION; PLATES; STIFFNESS;
D O I
10.1016/j.tws.2016.01.002
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
A web-core steel sandwich panel is a lightweight structure where thin plates are welded together by laser-welding technique. The plates form a T-joint which has in the center a weld thinner than the plates themselves. Thus the rotational stiffness of the joint is not infinite. The paper investigates the influence of T-joint rotational stiffness on the lowest natural vibration frequency of the panel. The methods used in the study have different kinematic assumptions. Equivalent single-layer (ESL) theory is used to obtain the frequency of the global vibration. The local vibrations are predicted using an isolated part of the panel, the I-beam model. In addition, three-dimensional model of a sandwich panel is analyzed. Finite element method (FEM) and analytical solution are used to obtain the frequencies. First-order shear deformation theory (FSDT) is used. The joint is considered through its rotational stiffness whose quantitative values are presented in the literature. Four different cross-sections with industrial relevancy are considered. The rotational stiffness of the T-joint affects the transverse shear stiffness of the panels. The results show up to 22% reduction of the fundamental frequency when compared with the case of the rigid joint for the global vibration mode. The effect on local vibrations is up to 11% in the case of asymmetric rotation in the T-joint and is otherwise insignificant. The study furthermore outlined the limitations of the ESL approach for assessment of natural frequencies in web-core sandwich panels depending on the vibration mode shape. The results show that the rotational stiffness of the T-joint has to be considered in the conceptual design of these structures. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:120 / 128
页数:9
相关论文
共 50 条
  • [1] Laser-welded steel sandwich panels
    不详
    NAVAL ARCHITECT, 1998, : 30 - 30
  • [2] Bending response of laser-welded web-core sandwich plates
    Romanoff, J.
    Varsta, P.
    ADVANCEMENTS IN MARINE STRUCTURES, 2007, : 263 - 271
  • [3] Fatigue crack growth rate in laser-welded web core sandwich panels - fatigue crack propagation in welded base metal
    Cernescu, Anghel
    Remes, Heikki
    Lehto, Pauli
    Romanoff, Jani
    11TH INTERNATIONAL FATIGUE CONGRESS, PTS 1 AND 2, 2014, 891-892 : 1212 - 1216
  • [4] Laser-welded web-core sandwich plates under patch loading
    Romanoff, Jani
    Varsta, Petri
    Remes, Heikki
    MARINE STRUCTURES, 2007, 20 (1-2) : 25 - 48
  • [5] Ultimate Strength Behaviour and Optimization of Laser-Welded Web-Core Sandwich Panels under In-Plane Compression
    Elsaka, Mohamed
    Guedes Soares, C.
    JOURNAL OF MARINE SCIENCE AND ENGINEERING, 2023, 11 (11)
  • [6] Laser-welded sandwich panels evaluated for US Navy ships
    不详
    ADVANCED MATERIALS & PROCESSES, 2008, 166 (09): : 20 - 21
  • [7] Optimisation of laser-welded sandwich panels with multiple design constraints
    Kolsters, Hans
    Wennhage, Per
    MARINE STRUCTURES, 2009, 22 (02) : 154 - 171
  • [8] Buckling of laser-welded sandwich panels: ultimate strength and experiments
    Kolsters, H.
    Zenkert, D.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART M-JOURNAL OF ENGINEERING FOR THE MARITIME ENVIRONMENT, 2010, 224 (M1) : 29 - 45
  • [9] Buckling and free vibration of laser-welded web-core sandwich panels: Extreme sensitivity to variation of weld rotational stiffness
    Yan, Shengyu
    Jelovica, Jasmin
    ENGINEERING STRUCTURES, 2021, 244
  • [10] Analysis and Experiment on Bending Performance of Laser-Welded Web-Core Sandwich Plates
    Sun, Yuping
    Saafi, Mohamed
    Zhou, Weili
    Zhang, Chen
    Li, Hui
    MATERIALS TODAY-PROCEEDINGS, 2015, 2 : 279 - 288