A Method for Estimating Vibro-acoustic Fatigue Life of Metal Structures with Uncertainties
An uncertainty, metal structure technology, applied in computing, instrumentation, geometric CAD, etc., can solve problems such as heavy workload, affecting structural mechanical behavior and safety, and only considering the first-order natural frequency.
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[0075] In order to understand more fully the characteristics of the invention and its applicability to engineering practice, the present invention establishes as image 3 The finite element model of the aircraft cavity structure shown is simplified and boundary conditions are applied. The uncertain information of this model is E=[67.45,74.55]GPa, the system transfer function is calculated after the unit surface pressure that changes with frequency is loaded on the model first, and then the random noise load is applied, and table 2 has provided the embodiment in the model Apply the converted noise power spectral density load (unit Pa 2 / Hz), the first ten natural frequencies of the structure are obtained, and the obtained stress power spectral density function of node 373 is as follows: Figure 4 As shown, the introduced material is 7075 aluminum alloy, and its S-N curve is as follows Figure 5 As shown, the cloud map of life distribution is finally calculated as Figure 6 ,...
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