RESEARCH ON OPTIMAL DESIGN OF PLATE-WEB BEAM STRUCTURE AGAINST FATIGUE BUCKLING BASED ON PARETO GENERAL ALGORITHM

In virtue of Detail Fatigue Rating method(DFR), an optimization design method of aircraft plate-web beam structure against fatigue buckling is proposed based on genetic algorithm. After finite element analysis and experimental verification, an optimized model of structure life on fatigue buckling is...

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Bibliographic Details
Main Authors: SU ShaoPu, XU GuangTao, DONG DengKe, CHEN An
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2018-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2018.06.016
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Summary:In virtue of Detail Fatigue Rating method(DFR), an optimization design method of aircraft plate-web beam structure against fatigue buckling is proposed based on genetic algorithm. After finite element analysis and experimental verification, an optimized model of structure life on fatigue buckling is built by engineering method, and the structure design solution in the condition of minimum mass is achieved with maximum fatigue life. The theoretical results illustrated that the life can excessively increase than that of the original beam. This technology will provide the design strategy of reducing aircraft mass and cost production for general aircraft structure.
ISSN:1001-9669