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Supersonic air inlet flow state monitoring method based on distinguishing feature learning

A supersonic inlet and flow state technology, applied in neural learning methods, instruments, biological neural network models, etc., to achieve good performance

Pending Publication Date: 2021-12-24
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Therefore, in the previous research process, the dynamic characteristics in the actual test data and the influence of factors such as noise and interference will be ignored.

Method used

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  • Supersonic air inlet flow state monitoring method based on distinguishing feature learning
  • Supersonic air inlet flow state monitoring method based on distinguishing feature learning
  • Supersonic air inlet flow state monitoring method based on distinguishing feature learning

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Embodiment

[0202] This embodiment uses the experimental data of a class of binary external pressure supersonic inlet to verify the effectiveness of the proposed DDL-CNN / TDL-CNN network. All experiments are performed on a laptop configured with IntelR CoreTM, i7-7700HQ CPU, 2.80GHz main frequency, 8G memory, Windows 10 system and MATLAB 2020b version.

[0203] In order to prove the effectiveness of the DDL-CNN / TDL-CNN network, this embodiment compares it with a traditional CNN. The network architectures used by these comparison methods are the same, the only difference is their loss function. The loss function of traditional CNN is cross-entropy loss, while DDL-CNN / TDL-CNN considers both cross-entropy loss and the learning of discriminative features.

[0204] In the specific implementation process, firstly, the dynamic pressure signal collected by each sensor is segmented by using a fixed-time sliding window to obtain samples under different flow states with a duration of 50 ms. Then, a...

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Abstract

The invention provides a method for monitoring the flow state of a supersonic air inlet channel, which adopts a method of combining a time-frequency analysis technology and deep learning to monitor the flow state of the supersonic air inlet channel from a dynamic sensor signal. The method comprises the following steps: performing preliminary signal processing on a dynamic sensor signal by using continuous wavelet transform, converting the dynamic sensor signal into a time-frequency spectrogram, and then inputting the time-frequency spectrogram into a convolutional neural network (CNN) for classification. In order to reduce the classification error, the invention provides a DDL-CNN / TDL-CNN (Doublet / Triplet ConvolutionalNeural Network combined with Discriminative Learning) which simultaneously considers the loss of the cross entropy and the learning of the discriminative features. The proposed method encourages the convolution module to project the time-frequency spectrogram to a feature space, so that different flow states in the space become more separable. Experimental results show that compared with a traditional CNN, the DDL-CNN / TDL-CNN has better performance on multiple indexes.

Description

technical field [0001] The invention belongs to the technical field of monitoring the flow state of a supersonic inlet, and in particular relates to a method for monitoring the flow state of a supersonic inlet. Background technique [0002] As one of the key components of the air-breathing supersonic propulsion system, the supersonic inlet has a direct impact on the performance of the whole system. For example, supersonic inlet surge is an extremely unstable flow state, usually accompanied by severe and periodic shock wave oscillations, which will seriously deteriorate the thrust characteristics of the entire propulsion system, and is always facing the risk of flameout . Not only that, but the periodic thermal load generated by the shock wave oscillation will also make the controllability of the whole system deteriorate sharply, and may even directly lead to the destruction of the overall structure, posing a threat to the safety of the aircraft and personnel. From the pers...

Claims

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Application Information

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IPC IPC(8): G06F30/27G06F30/28G06K9/62G06N3/04G06N3/08G06F113/08G06F119/14
CPCG06F30/27G06F30/28G06N3/084G06F2113/08G06F2119/14G06N3/044G06N3/045G06F18/2411G06F18/2415
Inventor 赵永平吴奂谭慧俊
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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