The invention provides a finite
element modeling method for a flight
simulation rotary table frame, and relates to the technical field of flight
simulation rotary table
simulation, and the method comprises the steps: S1, rotary table frame
feature recognition and parameterization setting, S2, mixed offset shell unit modeling of the rotary table frame, S3, multi-rule equivalent modeling of a shell unit of a thin-wall structure and a reinforcing rib, and S4,
model integration and application. According to the method, differentiated bias rules and multi-rule equivalence are set for the cylinder
assembly, the
thin wall and the reinforcing ribs respectively, the configurability of model precision and efficiency is achieved, various rules from
high fidelity to high efficiency are adopted according to the
design stage and the analysis target, under mechanical equivalence, the
model complexity and the calculation task requirement are optimally matched, and the design efficiency is improved. And the geometric characteristics of the reinforcing ribs are subjected to relevance setting according to
neutral plane normal offset parameters and a thin-wall
reference plane, so that equivalent simplification of bending resistance and
torsional rigidity of the reinforcing rib-thin-wall composite section is realized, an efficient simulation foundation is provided for a turntable frame, and the design efficiency of simulation driving is remarkably improved.