Finite Element Simulation and Experimental Study of Advanced Reinforced Structures
Received:December 29, 2020  Revised:February 06, 2021
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DOI:10.7643/issn.1672-9242.2021.04.009
KeyWord:advanced reinforcement structure  finite element simulation analysis  research and testing  stress level
                 
AuthorInstitution
WEI Li-jun Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
ZHAO Lian-hong Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
ZHANG Hong-fei Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
JIN Tao Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
LIU Yuan-hai Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
WANG Hao-wei Structure Corrosion Protection and Control of Aviation Science and Technology Key Laboratory, China Special Aircraft Research Institute, Jingmen , China
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Abstract:
      This paper aims to study the stress distribution characteristics of advanced reinforced structures under load. The finite element simulation analysis of advanced reinforced structures is carried out to simulate the stress and strain distribution of advanced reinforced structure under uniaxial load, at the same time, advanced reinforcement structural mechanics tests are carried out under uniform loading up to 20 kN at a speed of 0.02 mm/s. The stress and strain levels of advanced reinforced composite structures and metal matrix structures are obtained by strain detection. The finite element and test results are compared and analyzed. The results show that the simulation results of advanced reinforced structure are in good agreement with the test results. Advanced reinforcement structure can reduce the stress level of metal matrix structure results. According to the structure characteristics and load distribution characteristics of aircraft in high stress zone, the reasonable layout of advanced reinforcement structure can improve the fatigue and damage tolerance of this area.
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