Hierarchical model updating strategy of complex assembled structures with uncorrelated dynamic modes

被引:52
作者
Fei, Chengwei [1 ]
Liu, Haotian [1 ]
Choy, Yatsze [3 ]
Han, Lei [1 ]
Patricia Liem, Rhea [2 ]
机构
[1] Fudan Univ, Dept Aeronaut & Astronaut, Shanghai 200433, Peoples R China
[2] Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Hong Kong 999077, Peoples R China
[3] Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Peoples R China
基金
中国国家自然科学基金;
关键词
Aeroengine casings; Assembled structures; Correlated mode pair; Hierarchical model updating; Objective function; Uncorrelated modes; RESPONSE-SURFACE METHOD; SENSITIVITY-ANALYSIS; BOLTED JOINTS; RELIABILITY;
D O I
10.1016/j.cja.2021.03.023
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In structural simulation and design, an accurate computational model directly determines the effectiveness of performance evaluation. To establish a high-fidelity dynamic model of a complex assembled structure, a Hierarchical Model Updating Strategy (HMUS) is developed for Finite Element (FE) model updating with regard to uncorrelated modes. The principle of HMUS is first elaborated by integrating hierarchical modeling concept, model updating technology with proper uncorrelated mode treatment, and parametric modeling. In the developed strategy, the correct correlated mode pairs amongst the uncorrelated modes are identified by an error minimization procedure. The proposed updating technique is validated by the dynamic FE model updating of a simple fixed-fixed beam. The proposed HMUS is then applied to the FE model updating of an aeroengine stator system (casings) to demonstrate its effectiveness. Our studies reveal that (A) parametric modeling technique is able to build an efficient equivalent model by simplifying complex structure in geometry while ensuring the consistency of mechanical characteristics; (B) the developed model updating technique efficiently processes the uncorrelated modes and precisely identifies correct Correlated Mode Pairs (CMPs) between FE model and experiment; (C) the proposed HMUS is accurate and efficient in the FE model updating of complex assembled structures such as aeroengine casings with large-scale model, complex geometry, high-nonlinearity and numerous parameters; (D) it is appropriate to update a complex structural FE model parameterized. The efforts of this study provide an efficient updating strategy for the dynamic model updating of complex assembled structures with experimental test data, which is promising to promote the precision and feasibility of simulation-based design optimization and performance evaluation of complex structures. (c) 2021 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:281 / 296
页数:16
相关论文
共 52 条
  • [1] Modelling and updating of large surface-to-surface joints in the AWE-MACE structure
    Ahmadian, H
    Mottershead, JE
    James, S
    Friswell, MI
    Reece, CA
    [J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2006, 20 (04) : 868 - 880
  • [2] Parameter selection strategies in finite element model updating
    Ahmadian, H
    Gladwell, GML
    Ismail, F
    [J]. JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1997, 119 (01): : 37 - 45
  • [3] Finite element and isogeometric correlation analysis using modal assurance criterion
    Asma, F.
    Kacel, S.
    [J]. MECHANIKA, 2017, 23 (01): : 132 - 137
  • [4] Distributed Collaborative Response Surface Method for Mechanical Dynamic Assembly Reliability Design
    Bai Guangchen
    Fei Chengwei
    [J]. CHINESE JOURNAL OF MECHANICAL ENGINEERING, 2013, 26 (06) : 1160 - 1168
  • [5] THEORY OF INCOMPLETE MODELS OF DYNAMIC STRUCTURES
    BERMAN, A
    FLANNELLY, WG
    [J]. AIAA JOURNAL, 1971, 9 (08) : 1481 - +
  • [6] UPDATING FINITE-ELEMENT MODELS USING STATIC DEFORMATIONS
    BERRIET, R
    COGAN, S
    [J]. COMPUTERS & STRUCTURES, 1992, 45 (04) : 649 - 654
  • [7] A direct method for model updating with incomplete measured data and without spurious modes
    Carvalho, Joao
    Datta, Biswa N.
    Gupta, Abhijit
    Lagadapati, Maitreya
    [J]. MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2007, 21 (07) : 2715 - 2731
  • [8] Model validation for structural dynamics in the aero-engine design process
    Zang C.
    Ewins D.J.
    [J]. Frontiers of Energy and Power Engineering in China, 2009, 3 (4): : 480 - 488
  • [9] Structural dynamic model updating based on multi-level weight coefficients
    Chen, Luyun
    Guo, Yongjin
    Li, Leixin
    [J]. APPLIED MATHEMATICAL MODELLING, 2019, 71 : 700 - 711
  • [10] Structural dynamics model updating with interval uncertainty based on response surface model and sensitivity analysis
    Chen, Xueqian
    Shen, Zhanpeng
    Liu, Xin'en
    [J]. INVERSE PROBLEMS IN SCIENCE AND ENGINEERING, 2019, 27 (10) : 1425 - 1441