Multistage comprehensive fuzzy evaluation method for health state of reusable aircraft structure
CN120654151APending Publication Date: 2025-09-16HARBIN INST OF TECH
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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
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Figure CN120654151A_ABST
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.
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