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- W2393331886 abstract "In the research of optimization modeling about aircraft engine vibration performance,engine mounting system is an important subsystem in the vibration system of the aircraft,and its performance directly affects the overall performance of the aircraft. To solve the aero-engine problem about too big vibration displacement,the overall system performance optimization was carried out,hyperelastic constitutive theory of rubber materials and finite element modeling techniques of rubber isolator were analyzed and discussed,and the static characteristics of a single rubber component were analyzed using Ansys,which verified the credibility of the results of the simulation compared with the experimental results. Then,the impact of axial pre-compression on the overall stiffness of the isolator and the displacement amplitude was focused on,and the displacement amplitude,the engine vibration transfer rate and the fatigue properties of rubber materials were studied,which identified that choosing the best axial compression of the vibration isolator can provide the basis for the optimization of the whole performance of the suspension system." @default.
- W2393331886 created "2016-06-24" @default.
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- W2393331886 date "2014-01-01" @default.
- W2393331886 modified "2023-09-27" @default.
- W2393331886 title "Simulation of Static Characteristics of Aero-Engine Rubber Mount" @default.
- W2393331886 hasPublicationYear "2014" @default.
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