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Aero-engine service life prediction method based on improved LSTM

An aero-engine and life prediction technology, applied in the field of aero-engine, can solve the problem of high complexity of feature extraction model, achieve the effect of strong generalization ability and feasibility, reduce complexity, and improve the effect of life prediction

Pending Publication Date: 2022-04-08
CIVIL AVIATION UNIV OF CHINA
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Problems solved by technology

Kernel principal component analysis (KPCA) can be used to remove information redundancy between features and construct a reduced feature matrix. The complexity of the algorithm is closely related to the dimension of the data. Since the monitoring data collected by the engine sensor It has the characteristics of high dimensionality, multi-parameters, and large scale, resulting in high complexity of the feature extraction model

Method used

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  • Aero-engine service life prediction method based on improved LSTM
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  • Aero-engine service life prediction method based on improved LSTM

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Embodiment

[0073] Refer to attached Figure 1-6 As shown, an aero-engine life prediction method based on improved LSTM includes the following steps:

[0074] Step 1: Process the raw sensor data acquired by the sensor and construct a training sample. The training sample includes a training set and a test set. The specific steps include:

[0075] Step 1.1: Normalize and standardize the raw sensor data acquired by the sensor. The specific method is to use the Min-Max model for normalization, as shown in formula (1), and convert the normalized data to the mean value is 0 and a distribution with a standard deviation of 1;

[0076]

[0077] Data standardization, as shown in formula (2):

[0078]

[0079] In formula (1), (2), x' i,j (t) represents the dimensionless sample, x i,j (t) represents the original sample, max(x :,j ) represents the maximum value of the same dimension sample, min(x :,j ) represents the minimum value of the same dimension; represents the sample mean; s repr...

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Abstract

The invention belongs to the technical field of aero-engines, and particularly relates to an aero-engine service life prediction method based on improved LSTM. Comprising the steps of 1, processing original sensor data acquired by a sensor, and constructing a training sample which comprises a training set and a test set; step 2, on the basis of constructing the training sample in the step 1, constructing an LSTM structure model as an engine residual life prediction model; and 3, inputting the test set in the step 1 into the LSTM structure model constructed in the step 2 to obtain a predicted RUL value, and evaluating the obtained predicted RUL value by adopting RMSE and Score evaluation indexes. According to the aero-engine life prediction method based on SDAE and LSTM, the advantage of unsupervised feature extraction of a deep encoder is utilized, effective feature extraction is performed on an engine sensor signal, low efficiency of manual feature extraction and prediction uncertainty caused by the low efficiency are avoided, and the prediction accuracy is improved. And the residual life of the engine is predicted by using the advantage of processing the time sequence data by the LSTM model.

Description

technical field [0001] The invention belongs to the technical field of aero-engines, in particular to an aero-engine life prediction method based on improved LSTM. Background technique [0002] Aeroengine is an important part of the normal flight of the aircraft. Due to the complex and changeable operating conditions of the engine and the relatively harsh operating environment, once it fails, it will pose a huge threat to flight safety and the safety of passengers. The remaining life prediction of aero-engines is based on condition monitoring data, such as fan, compressor inlet and outlet temperature, pressure, speed and other historical data, and features are extracted to build a life prediction model and provide technical support for preventive maintenance, which has a wide range of application values. [0003] In recent years, data-driven methods have gradually become the mainstream technology in the field of remaining life prediction. There are two types of commonly used...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/27G06N3/04G06N3/08G06F119/04
Inventor 郭晓静贠玉晶殷宇萱赵小源
Owner CIVIL AVIATION UNIV OF CHINA
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