Aero-engine residual life prediction method based on transfer learning
An aero-engine and life prediction technology, which is applied in neural learning methods, computer-aided design, biological neural network models, etc., can solve problems such as difficult to obtain degradation data, low prediction accuracy, and poor engineering usability, so as to achieve improved accuracy and high Prediction accuracy and the effect of improving prediction accuracy
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[0066] The flow chart of the method for predicting the remaining life of an aero-engine based on transfer learning proposed by the present invention, such as figure 1 shown. The specific steps of the method for predicting the remaining life of an aero-engine based on transfer learning are as follows:
[0067] Step 1. Sensitive parameter analysis S1: Sensitivity analysis is carried out for all the state monitoring parameters of the aero-engine, so as to obtain several monitoring parameter sets X={x 1 , x 2 ,...,x n}
[0068] Step 2, data preprocessing S2: smoothing and normalizing preprocessing are performed on the selected aero-engine performance degradation characteristic parameter sequence, and c preprocessed parameter data X={x 1 , x 2 ,...x c}, c is the number of engine operating cycles, where X c ={x c1 , x c2 ,...,x cn}
[0069] Step 3. Calculation of the similarity distance based on the dynamic time warping algorithm S3: Carrying out the transferability measu...
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