Abstract: The present disclosure provides an optimized designing method for a laminate preform of a ceramic matrix composite e. With overall consideration of a strength requirement of a component, a geometric shape and properties of the laminate preform, the method includes: optimizing, based on a corresponding mechanical formula, a fiber volume fraction of each laminate constituting the preform and a fiber direction in the laminate, and selecting a preferred microscopic structure for each laminate, thereby taking full advantage of material performance. The method is applicable for optimized design of various components of the ceramic matrix composite.

Abstract: A structural integration design method for a ceramic matrix composite bolt preform is provided, which includes: preform modeling; structure modeling; deformation and failure calculation. The method builds different small composites inside the bolt according to actual mesostructures of the ceramic matrix composites, which can realize structurally macroscopic failures caused by mesoscopic failures inside the small composites. The screw threads that are built by the method can reflect a failure form of thread teeth, and the influence of complex stress conditions of the screw threads on the failure form of the screw fracture is also considered, which improves the prediction accuracy of the strength of the ceramic matrix composite bolt. The method builds a structure integrated model, which has a certain structure, for a ceramic matrix composite preform according to the actual size and shape of the structure.