Method for predicting failure of aero-engine
An aero-engine and fault prediction technology, which is applied in the field of aero-engines, can solve the problems of aero-engines with complex structures, prone to failures, and complex and changeable environmental conditions
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Embodiment 1
[0057] Such as figure 1 As shown, the embodiment of the present invention provides an aeroengine failure prediction method, including:
[0058] 101. Collect parameter data in the engine recording system to obtain engine vibration signals, and determine a training data set based on the parameter data;
[0059] Among them, the training data set is used to train the model;
[0060] 102. Use the python platform to construct an LSTM neural network model, and determine the signal marginal spectrum according to the training data set and the LSTM neural network;
[0061] 103. Use the python platform to construct a BP neural network model, use the marginal spectral feature training set to train the BP neural network, obtain and store the BP neural network parameters after training convergence;
[0062] 104. Predict the failure of the aeroengine according to the trained BP neural network model.
[0063] Optionally in one embodiment, after the collection of the parameter data in the e...
Embodiment 2
[0103] The embodiment of the present invention provides an aeroengine failure prediction method, which uses the long-short-term memory cyclic neural network algorithm to train a prediction model suitable for the engine vibration signal of the test data set through the training data set, and can predict the future short-term aircraft engine failure prediction method. State signal data, feed the predicted data into the input of the Hilbert-Huang Transform (HHT) algorithm, and decompose it into a series of IMF components according to the inherent fluctuation mode of the signal by using the empirical mode decomposition method (EMD), Carry out Hilbert transform (HHT) on the IMF component, analyze and extract the signal based on the energy change characteristics of the marginal spectrum; use the extracted fault characteristic parameters as the training input of the BP neural network, and use a large number of measured fault signals for diagnostic testing to realize Engine Failure Pre...
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