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Aero-engine residual life prediction method based on data enhancement

An aero-engine and life prediction technology, which is applied in electrical digital data processing, computer-aided design, instruments, etc., can solve the problems of not being able to meet the needs of deep learning model training data, not being able to mine and comprehensively consider, and poor generalization performance. Achieve the effect of improving prediction accuracy, reducing over-fitting phenomenon, and improving calculation speed

Pending Publication Date: 2022-05-27
BEIJING UNIV OF TECH
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AI Technical Summary

Problems solved by technology

Most of the existing deep learning models are based on a single model, which cannot mine and comprehensively consider various features, and the generalization performance is poor.
In addition, in terms of degradation data, there are few existing performance degradation data sets, which cannot meet the needs of deep learning models for a large amount of training data, making the accuracy of existing deep learning life prediction models low

Method used

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  • Aero-engine residual life prediction method based on data enhancement
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  • Aero-engine residual life prediction method based on data enhancement

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Embodiment Construction

[0033] A method for predicting the remaining life of an aero-engine based on data enhancement of the present invention will be further described below with reference to the accompanying drawings.

[0034] The invention adopts the turbofan engine degradation simulation data set disclosed by NASA, and invents a data enhancement method and a multi-path feature fusion prediction model to predict the remaining life of the aero-engine.

[0035] Step 1: Data Prediction Processing

[0036] The adopted CMAPSS dataset is used for data enhancement and data normalization.

[0037] The specific operations of data enhancement are as follows: figure 1 shown, figure 1 (a) is the complete training trajectory of an engine RUL, and each moment in the trajectory contains multi-dimensional data. In the augmentation algorithm, partial training trajectories are generated from the full training trajectories. like figure 1 Use as shown in (b) of figure 1 The full training trajectory in (a) of (a...

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Abstract

The invention discloses an aero-engine residual life prediction method based on data enhancement, and provides a multi-path feature fusion network model and a data enhancement algorithm. Firstly, the number of samples of a data set is increased through a data enhancement mode, so that the prediction accuracy is improved; secondly, a multi-path feature fusion prediction model is constructed, and two different paths are selected to extract features: the first path inputs data into a convolutional neural network (CNN) and a gating cycle unit (GRU), and spatial features and time sequence features are extracted respectively; and the second path directly inputs the data into a long short-term memory (LSTM) network to obtain time sequence characteristics. And finally, fusing the output features of the two paths, and inputting the fused output features into a full-connection layer for RUL prediction. Compared with an existing network model, the residual life prediction precision of the equipment can be effectively improved, and the method has practical application value.

Description

technical field [0001] The invention relates to a method for predicting the remaining life of an aero-engine, in particular to a method for predicting the remaining life of an aero-engine based on data enhancement and a multi-path feature fusion model. Background technique [0002] Turbofan engine, as the "heart" of various aircraft systems in the aviation field, its performance changes can directly affect the safe operation of the aircraft. However, due to the daily work of aviation turbofan engines in the environment of high temperature, high pressure and high vibration speed, accidents and failures are prone to occur with the increase of working time. Therefore, it is of great significance to predict the remaining life (RUL) of aviation turbofan engines and change the regular maintenance to active maintenance for reducing flight safety accidents and saving equipment maintenance costs. [0003] At present, the remaining life prediction methods can be roughly divided into ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06F119/02G06F119/04
CPCG06F30/27G06F2119/02G06F2119/04Y02T90/00
Inventor 赵德群赵嘉宇张雅栋
Owner BEIJING UNIV OF TECH
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