An Improved Proxy Model Based Random Perturbation Method for Eigenvalues of Repeated Frequency Structural Vibration
A surrogate model, structural vibration technology, applied in complex mathematical operations and other directions, can solve problems such as little research work, non-unique eigenvalue derivatives, difficult analysis process, etc., to achieve a wide range of applications, avoid large-scale high-cost sample points Calculate the effect of the problem
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment
[0094] In order to understand more fully the characteristics of this invention and its applicability to engineering practice, the present invention uses figure 2 Taking the dome structure system as an example, the eigenvalue analysis and verification of the repetition frequency structure is carried out. figure 2 The dome structure in is composed of 52 rods and 21 nodes, and the cross-sectional area of each rod is 10cm 2 . The dome structure is symmetrical with respect to the Y axis and the X axis, and the nominal values of the elastic modulus, material density and Poisson's ratio of the rods are respectively E=210GPa, ρ=7850kg / m 3 ,μ=0.3. The coordinates of important representative nodes are shown in Table 1.
[0095] Table 1
[0096]
[0097]
[0098] In this embodiment, the elastic modulus and material density are treated as random variables, and respectively satisfy the distribution N(210,10.5 2 ) and N(7850,392.5 2 ). Applying the method proposed by the ...
PUM
Abstract
Description
Claims
Application Information
- R&D Engineer
- R&D Manager
- IP Professional
- Industry Leading Data Capabilities
- Powerful AI technology
- Patent DNA Extraction
Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.
© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com