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

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

CN114297910APending Publication Date: 2022-04-08CIVIL AVIATION UNIV OF CHINA

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

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Experimental program
Comparison scheme
Effect test

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...

Claims

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Application Information

Patent Timeline
08 Apr 2022
Publication
CN114297910A
IPC
G06F30/27; G06N3/04; G06N3/08; G06F119/04
Inventors
郭晓静; 贠玉晶