The application provides a force-bearing casing support plate and mounting edge
axial distance design method, and relates to the technical field of an aero-engine. The method comprises the following steps: S1, determining the maximum load of the force-bearing casing mounting edge according to a set engine design method; S2, equivalent the force and moment of the maximum load acting on the casing mounting edge to a maximum
resultant force F 合 ; S3, taking the material
yield limit as the maximum
stress limit value of the force-bearing support plate root
rounding position, calculating the minimum
axial distance l min of the force-bearing casing support plate and the mounting edge according to the maximum
resultant force F 合 of the force-bearing casing mounting edge; S4, taking the minimum rigidity of the casing mounting edge as the minimum rigidity of the casing mounting edge according to the maximum
resultant force F 合 , calculating the maximum
axial distance l max of the force-bearing casing support plate and the mounting edge according to the minimum rigidity. The application can guarantee that the maximum
stress level and the minimum deformation of the casing meet the design requirements, and realize the optimal solution of the strength life and the rigidity.