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Method and device for predicting residual service life of aero-engine through time-frequency domain analysis

An aero-engine and life prediction technology, which is applied in neural learning methods, computer components, computer-aided design, etc., can solve the problems of not analyzing and considering the correlation of multiple input features, CNN ignoring the timing of data, etc., to achieve long-term degradation Trends, reasonable forecast results, and the effect of improving forecast accuracy

Pending Publication Date: 2022-05-13
UNIV OF SCI & TECH BEIJING
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AI Technical Summary

Problems solved by technology

[0006] Aiming at the problem that CNN ignores the timing of data in the prior art, and the RNN network does not analyze and consider the correlation between multiple input features, the present invention proposes a time-frequency domain analysis method for predicting the remaining service life of an aero-engine and device

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  • Method and device for predicting residual service life of aero-engine through time-frequency domain analysis
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  • Method and device for predicting residual service life of aero-engine through time-frequency domain analysis

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[0064] In order to make the technical problems, technical solutions and advantages to be solved by the present invention clearer, the following will describe in detail with reference to the drawings and specific embodiments.

[0065] An embodiment of the present invention provides a time-frequency domain analysis method for predicting the remaining service life of an aeroengine, and the method can be implemented by an electronic device, and the electronic device can be a terminal or a server. like figure 1 The flow chart of the method for analyzing the remaining service life of an aero-engine in the time-frequency domain is shown, and the processing flow of the method may include the following steps:

[0066] S101: Preprocessing the raw data of the aeroengine sensor;

[0067] S102: For the preprocessed original data, use continuous wavelet transform to obtain corresponding time-frequency domain data;

[0068] S103: Construct a sliding window and an input of a prediction mode...

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Abstract

The invention provides a time-frequency domain analysis aero-engine remaining service life prediction model method and device, and relates to the technical field of aero-engine service life prediction and health management. Comprising the following steps: preprocessing aero-engine sensor data, carrying out continuous wavelet transform to obtain time-frequency domain characteristics, and constructing network input from three dimensions of time, a sensor and the time-frequency domain characteristics; and establishing and training a 3DConLSTM neural network to obtain an output result, namely prediction of the remaining service life. According to the method, continuous wavelet transform is introduced, and historical data of the aero-engine are analyzed in a time domain and a time-frequency domain respectively. The characteristics of the LSTM network are adopted, three gating units control inflow of information, and the long-term degradation trend of time sequence data is reserved; according to the method, dot product operation in a traditional LSTM network is changed into convolution operation, features among three-dimensional inputs are effectively extracted, time sequence and spatiality of data are considered, the residual service life prediction result is more accurate, and the residual service life prediction precision is improved.

Description

technical field [0001] The invention relates to the technical field of aero-engine life prediction and health management, in particular to a time-frequency domain analysis method and device for predicting the remaining service life of an aero-engine. Background technique [0002] RUL (Remaining Useful Life) prediction can predict the time from the operating state of the equipment at a specific moment to the fault state. Existing RUL methods mainly include three categories: physical model-based methods, data-driven methods and hybrid methods. First, physical model-based methods develop physical failure models by studying the internal interpretation mechanisms of equipment. These methods are developed on the basis of physical system knowledge, and the accuracy is limited when the system is complex. Second, data-based methods can be based on historical sensor The data learns potential degradation trends. Third, hybrid methods try to integrate the above two methods, but sometim...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06K9/00G06N3/04G06N3/08G06F119/04
CPCG06F30/27G06N3/08G06F2119/04G06N3/048G06N3/044G06F2218/06
Inventor 胡艳艳辛英杰
Owner UNIV OF SCI & TECH BEIJING
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