The load-bearing sealing frame of an aircraft was designed using CAD/CAE integrated design technology: CAD model and CAE model were established; various main parameters required for stiffness and strength analysis of the load-bearing sealing frame were determined according to the use environment and design requirements of the load-bearing sealing frame; CAE system software was used to calculate the stiffness and strength of the load-bearing sealing frame, and the calculation results were analyzed. Keywords: fuselage load-bearing frame; computer-aided design; finite element analysis
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