An aerial electromechanical equipment residual life prediction method, device, medium and product fusing multi-source sensor data
By constructing an improved neural network model that integrates multi-source sensor data, the problem of accuracy in predicting the remaining life of aviation electromechanical equipment was solved, achieving more efficient prediction results.
CN118898039BActive Publication Date: 2026-06-26BEIHANG UNIV
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIHANG UNIV
- Filing Date
- 2024-07-08
- Publication Date
- 2026-06-26
Smart Images

Figure CN118898039B_ABST
Abstract
The application discloses an aviation electromechanical equipment residual life prediction method and device fusing multi-source sensor data, a medium and a product, and relates to the technical field of intelligent information. The method comprises the following steps: inputting the preprocessed multi-source sensor data of the aviation electromechanical equipment into an aviation electromechanical equipment residual life prediction model to obtain an aviation electromechanical equipment residual life prediction value; the aviation electromechanical equipment residual life prediction model is obtained by training a neural network model using a training set; the training set comprises a plurality of preprocessed training samples and corresponding aviation electromechanical equipment residual life values, and the training sample is historical multi-source sensor data; wherein the aviation electromechanical equipment residual life prediction model comprises an improved mixed bidirectional long short-term memory network submodel, a residual network submodel, a multi-head attention mechanism network submodel, a first full connection layer, a second full connection layer and a first activation function layer connected in sequence. The application improves the accuracy of aviation electromechanical equipment residual life prediction.
Need to check novelty before this filing date? Find Prior Art
Citation Information
Patent Citations
CN115510740A
CN116663386A