Composite material electrical lap joint model impedance analysis method, device, equipment and medium
By establishing a composite material simulation lap joint model, analyzing the factors affecting impedance, and optimizing fastener stress and lap joint area, the problems of long cycle and high cost in evaluating the lap joint performance of composite materials for aircraft were solved, and efficient lap joint performance testing was achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- COMMERCIAL AIRCRAFT CORP OF CHINA LTD
- Filing Date
- 2022-08-04
- Publication Date
- 2026-05-26
AI Technical Summary
In the existing technology, the evaluation of the bonding performance of composite material aircraft relies on experimental measurement, which results in long testing cycles and high costs, and cannot determine the bonding performance under a single condition.
By establishing a composite material simulation lap model, the impedance influencing factors are determined based on the initial electrical parameter distribution. The fastener stress and lap area of the simulation lap model are adjusted to analyze the impedance influence and optimize the lap performance.
It shortens the testing cycle for overlap performance, improves testing efficiency, reduces testing costs, and can accurately evaluate overlap performance under single conditions.
Smart Images

Figure CN117556583B_ABST