Structural Modal Parameter Identification Method Based on Double Exponential Window Function Method
A technology for structural modal and parameter identification, which is applied in the processing of detected response signals, instruments, design optimization/simulation, etc. It can solve problems such as complex damping characteristics, and achieve the effects of less noise interference, elimination of errors, and strong robustness.
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Embodiment example 1
[0069] Implementation case 1: turbocharger impeller (30 blades) model
[0070] Taking a turbocharger with 30 impellers as an example, by solving the differential equation containing 10% blade detuning, the time-domain response signal of the speed of 30 blades when each blade is affected by the impact force is obtained. The signal duration is 1s, and the time The step size is Δt=1×10 -5 s; Table 1 shows the real natural frequency and damping ratio of the impeller by solving the characteristic equation composed of the impeller mass matrix and stiffness matrix.
[0071] Table 1 The real natural frequency and damping ratio of the impeller
[0072]
[0073] In order to verify the robustness of the identification method of this scheme, a 3dB signal-to-noise ratio is added to each group of signals, from figure 2 It can be seen that the signal is seriously polluted by noise at this time. Based on the force time history and velocity time history, a 30×30 structural admittance ma...
Embodiment example 2
[0075] Implementation Case 2: Floor Aluminum Profiles for High-speed Trains
[0076] Aluminum profile is a typical dynamic complex structure, and its finite element model is shown as Figure 4 As shown, 19 points are randomly selected in the upper and lower panels, such as Figure 5 shown. The hammer test is carried out for each measuring point separately, and the acceleration time-history signals of 19 measuring points are collected, the signal duration is 2s, and the time step is Δt=1.2207×10 -4 . Based on the force and acceleration time-history signals, a 19×19 admittance matrix can be obtained according to the steps of the scheme.
[0077] In order to illustrate that this scheme can flexibly select the attenuation rate, the attenuation rate b is given respectively 1 = 0.1dB and b 1 =-20dB exponential window function, the force and acceleration time-history signals are truncated and windowed, and obtained as Figure 6 The shown theoretical truncated windowed admittanc...
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