螺栓连接薄板结构等效刚度模拟方法研究

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2024-03-26 DOI:10.1155/2024/8648996
Zhe Chen, Qi-jun Zhao, Guo-chen Zhou
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引用次数: 0

摘要

螺栓连接在装配式结构中应用广泛,其动态特性往往受到刚度、阻尼、激励等因素的影响。为了解决螺栓结构精细建模计算效率低、线性化等效建模计算误差大的问题,本文提出了一种基于多尺度方法并考虑非线性因素影响的螺栓结构动态特性参数识别方法。在该方法中,螺栓连接特性以剪切刚度、扭转刚度、非线性刚度和粘性阻尼系数的组合形式进行模拟,并根据测试测量频率和频率响应函数进行识别。同时,通过建立螺栓结构的非线性动态模型,研究了不同螺栓预紧力和激振力对螺栓结构动态特性的影响。
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Research on the Simulation Method for Equivalent Stiffness of Bolted Connection Thin Plate Structures
Bolted connections are widely used in assembly structures, and their dynamic characteristics are often affected by stiffness, damping, excitation, and other factors. In order to solve the problems of low computational efficiency of fine modeling and large computational error of linearized equivalent modeling of bolted structures, this paper proposes a dynamic characteristic parameter identification method for bolted structures based on the multiscale method and considering the influence of nonlinear factors. In this method, the bolted connection characteristics are simulated in the form of a combination of shear stiffness, torsional stiffness, nonlinear stiffness, and viscous damping coefficient and identified according to the test measurement frequency and frequency response function. At the same time, by establishing the nonlinear dynamic model of bolted structure, the influence of different bolt preloads and excitation forces on the dynamic characteristics of bolted structure is studied.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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