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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

Inactive Publication Date: 2020-01-17
SHANDONG CHAOYUE DATA CONTROL ELECTRONICS CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the structure of the aero-engine is very complex, there are many parts, and the environmental conditions are complex and changeable. Many parts work in harsh environments such as high temperature, high pressure, high-speed rotation, and strong vibration, and are subjected to high loads and thermal shocks, so they are prone to failure. The failure of the engine is related to the safe flight of the aircraft, and failure prediction is usually required

Method used

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  • Method for predicting failure of aero-engine

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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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Abstract

An embodiment of the invention discloses a method for predicting a failure of an aero-engine, which comprises the following steps: collecting parameter data in an engine recording system to obtain anengine vibration signal, and determining a training data set and test data based on the parameter data; constructing an LSTM neural network model by using a python platform, and determining a signal margin spectrum according to the training data set and the LSTM (Long Short Term Memory) neural network; constructing a BP neural network model by using the python platform, training a BP (Backward Propagation) neural network by using a marginal spectrum characteristic training set, and acquiring and storing parameters of the BP neural network after convergence of training; and predicting a failureof the aero-engine according to the trained BP neural network model. Through adoption of the method of the invention, the failure of the aero-engine can be predicted.

Description

technical field [0001] The invention relates to the field of aero-engines, in particular to an aero-engine failure prediction method. Background technique [0002] The aero-engine is the most important part of the aircraft, and its reliability and safety are extremely important. However, the structure of the aero-engine is very complex, there are many parts, and the environmental conditions are complex and changeable. Many parts work in harsh environments such as high temperature, high pressure, high-speed rotation, and strong vibration, and are subjected to high loads and thermal shocks, so they are prone to failure. Engine failure is related to the safe flight of the aircraft, and failure prediction is usually required. [0003] How to predict the failure of aero-engine is a problem that needs to be solved at present. Contents of the invention [0004] An embodiment of the present invention provides an aeroengine failure prediction method capable of predicting aeroengi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/14G01M15/12G01H17/00G06N3/04G06N3/08
CPCG01M15/14G01M15/12G01H17/00G06N3/084G06N3/044G06N3/045
Inventor 黄刚艾腾腾许政
Owner SHANDONG CHAOYUE DATA CONTROL ELECTRONICS CO LTD
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