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Abstract
Based on the computing platform of the finite element method commercial software ABAQUS, the mechanical property of the simulation training cabin in a helicopter rescue simulation system was researched by the finite element analysis. This paper studied the dynamic properties of the cabin skeleton under the dynamic load of the six-DOF platform. Moreover, the stress and displacement distribution and variation law of the stimulation cabin were obtained from the stimulation. Results show that the cabin structure design is reasonable and provide a theory basis for the simulation cabin mechanism design optimization and manufacture. For other similar structure design, the study has certain reference value.
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