scholarly journals Development of fault diagnosis platform for liquid rocket engine based on experimental data

2021 ◽  
Vol 2093 (1) ◽  
pp. 012022
Author(s):  
Shoujin Chang ◽  
Yong He ◽  
Haitao Hu ◽  
Jiaxin Chai ◽  
Minghe Hu ◽  
...  

Abstract Aiming at the defects of difficult to establish fault diagnosis models caused by the small scale of liquid rocket engine test data, imbalanced categories and high fault coupling, the fault diagnosis platform with 10 fault diagnosis models are developed for fault diagnosis, covering K-nearest neighbor (KNN) model, optimized KNN model, logistic regression (LR) model, optimized LR model, support vector machine model, K-means model, decision tree model, neural network model, random forest model and light-GBM model. The prediction accuracies of these models are validated based on the experimental data. Among these models, the light-GBM model provide the best prediction accuracies, and 5 models have the prediction accuracy larger than 98%.

2015 ◽  
Vol 19 (3) ◽  
pp. 73-82 ◽  
Author(s):  
Taewoan Kim ◽  
Wanchan Kim ◽  
Sunjin Kim ◽  
Yeoungmin Han ◽  
Youngsung Ko

2011 ◽  
Vol 383-390 ◽  
pp. 7729-7733
Author(s):  
Na Zhao ◽  
Yong Gang Yu ◽  
Yu Qiang Wang

The mathematical and physical model of the liquid propellant spray in straight nozzle was proposed for studying the performance characteristics of the small-scale liquid rocket engine. With the Fluent software, the numerical simulation was carried out. Sauter mean diameter (SMD) of the HAN-based liquid propellant (LP1846) in the engine combustor changing with spray pressure, nozzle diameter and the liquid surface tension were analyzed. The results indicate that: in the spray pressure region of 1.8MPa~3.0MPa, at a fixed spray pressure, the smaller is the nozzle diameter, the smaller is the droplets’ SMD and the relationship between the SMD and the nozzle diameter is approximately linearity; for the same nozzle diameter and spray pressure, the larger is the surface tension, the larger is the liquid droplets’ SMD.


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