Multistage comprehensive fuzzy evaluation method for health state of reusable aircraft structure

CN120654151APending Publication Date: 2025-09-16HARBIN INST OF TECH
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202510744899.6
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-06-05
Publication Date
2025-09-16

Smart Images

  • Figure CN120654151A_ABST
    Figure CN120654151A_ABST
Patent Text Reader

Abstract

The invention relates to a reusable aircraft structure health state multi-stage comprehensive fuzzy evaluation method. The invention relates to the technical field of reusable aircraft structure health state evaluation, and the method comprises the steps: converting spacecraft evaluation indexes into elements, and forming a factor set; forming a comment set according to various results made by the evaluation target; through structural health monitoring, a membership function is determined, and a multi-level evaluation model and a single-factor evaluation matrix are constructed; and determining an evaluation result, and taking the finally obtained membership degree as a comprehensive index for representing the health degree of the structure. According to the method, a quantitative mapping relation between material microscopic damage and structure macroscopic attenuation is established, and the defect of independent evaluation of cross-scale damage in a traditional method is overcome.
Need to check novelty before this filing date? Find Prior Art