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Modeling and analysis of nonlinear dynamics of axisymmetric vector nozzle based on deep neural network

Published online by Cambridge University Press:  11 November 2024

X. Wang*
Affiliation:
School of Mechanical Engineering and Automation, Northeastern University, Shenyang, China Key Laboratory of Vibration and Control of Aero-Propulsion System, Ministry of Education, Northeastern University, Shenyang, PR China AECC Shenyang Engine Research Institute, Shenyang, China
H. Hu
Affiliation:
School of Mechanical Engineering and Automation, Northeastern University, Shenyang, China
Z. Chen
Affiliation:
School of Mechanical Engineering and Automation, Northeastern University, Shenyang, China
H. Wang
Affiliation:
School of Mechanical Engineering and Automation, Northeastern University, Shenyang, China
L. Ye
Affiliation:
AECC Shenyang Engine Research Institute, Shenyang, China
G. Ye
Affiliation:
AECC Shenyang Engine Research Institute, Shenyang, China
*
Corresponding author: X. Wang; Email: wangxy@me.neu.edu.cn

Abstract

The axisymmetric nozzle mechanism is the core part for thrust vectoring of aero engine, which contains complex rigid-flexible coupled multibody system with joints clearance and significantly reduces the efficiency in modeling and calculation, therefore the kinematics and dynamics analysis of axisymmetric vectoring nozzle mechanism based on deep neural network is proposed. The deep neural network model of the axisymmetric vector nozzle is established according to the limited training data from the physical dynamic model and then used to predict the kinematics and dynamics response of the axisymmetric vector nozzle. This study analyses the effects of joint clearance on the kinematics and dynamics of the axisymmetric vector nozzle mechanism by a data-driven model. It is found that the angular acceleration of the expanding blade and the driving force are mostly affected by joint clearance followed by the angle, angular velocity and position of the expanding blade. Larger joint clearance results in more pronounced fluctuations of the dynamic response of the mechanism, which is due to the greater relative velocity and contact force between the bushing and the pin. Since axisymmetric vector nozzles are highly complex nonlinear systems, traditional numerical methods of dynamics are extremely time-consuming. Our work indicates that the data-driven approach greatly reduces the computational cost while maintaining accuracy, and can be used for rapid evaluation and iterative computation of complex multibody dynamics of engine nozzle mechanism.

Type
Research Article
Copyright
© The Author(s), 2024. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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Footnotes

*

These two authors contributed equally to this work.

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