Novel method for recognizing rigidity between shearing type structure layers under environmental excitation
An environmental excitation and shear type technology, which is applied in the field of structural physical parameter identification, can solve problems such as difficult measurement and non-repeatable environmental excitation, and achieve the effects of improving efficiency, facilitating computer program implementation, and suppressing noise interference
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Embodiment 1
[0037] Take the shear structure with the number of degrees of freedom n=6 as an example (such as figure 2 ), carry out the numerical simulation for the identification of the stiffness between layers, because the vibration magnitude of the environmental excitation is very small, it can be considered that the structure is in a state of linear vibration. The basic parameters of the structure are given in Table 1, the proportional damping is assumed, and the damping ratio is taken as 0.02. The environmental excitation acting on the substrate is simulated by a white noise acceleration signal with a bandwidth of 0.5Hz to 40Hz, and the maximum amplitude of the substrate acceleration is 5×10 4 m / s 2, take 8000 sampling points, the sampling interval is 0.01s, such as image 3 As shown, the Wilson-θ method is used to solve the acceleration response of each layer of the structure under environmental excitation.
[0038] Table 1 Basic parameters of the structural model
[0039]
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Embodiment 2
[0049] Taking the shear structure model with the number of degrees of freedom n=10 as an example, the identification method proposed by the present invention is tested and verified. The height between layers of the model is 250mm, the length and width of each layer of steel plates are 400mm, and the thickness is 6mm. The four columns between each layer are made of φ6 steel rods, and the steel rods are welded to the upper and lower steel plates. One acceleration sensor is arranged along the horizontal one-way on each layer of steel plate, totaling 10. The mass estimate for each layer is 4kg.
[0050] Due to the small size of the model, the geometric deviation in the manufacturing process has a great influence on the inter-story stiffness of the structure. Therefore, the inter-story stiffness value calculated by the design parameters is not accurate enough, and the accurate value of the inter-story stiffness of the model needs to be obtained through actual measurement. .
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