Multi-Extremum Adaptive Fuzzy Network Method for Dynamic Reliability Estimation Method of Vectoring Exhaust Nozzle

Author:

Zhang Chunyi1,Yuan Zheshan2,Li Huan3,Wen Jiongran3ORCID,Zheng Shengkai1,Fei Chengwei3ORCID

Affiliation:

1. College of Mechanical and Electrical Engineering, Guangdong University of Science and Technology, Dongguan 523668, China

2. Weihai Guangtai Airport Equipment Co., Ltd., Weihai 264203, China

3. Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, China

Abstract

To enhance the accuracy and efficiency of reliability analysis for an aero-engine vectoring exhaust nozzle (VEN), a multi-extremum adaptive fuzzy network (MEAFN) method is developed by absorbing an adaptive neuro-fuzzy inference system (ANFIS) into the multi-extremum surrogate model (MESM) method. In the proposed method, the MERSM is used to establish the surrogate models of many output responses for the multi-objective integrated reliability analysis of the VEN. The ANFIS method is regarded as the basis function of the MESM method and adopted to improve the modeling precision of the MESM by introducing the membership degree into the input parameters and weights to improve the approximation capability of the neural network model to the high nonlinear reliability analysis of the VEN. The mathematical model of the MEAFN method and reliability analysis thoughts of the VEN is provided in this study. Then, the proposed MEAFN method is applied to conduct the dynamic reliability analysis of the expansion sheet and the triangular connecting rod in the VEN by considering the aerodynamic loads, operation temperature, and material parameters as the random input variables and the stresses and deformations as the output responses, compared with the Monte Carlo method and the extremum response surface method. From the comparison of the methods, it is indicated that the MEAFN method is promising to improve computational efficiency while maintaining accuracy. The efforts of this study provide guidance for the optimization design of the VEN and enrich the reliability theory of the flexible mechanism.

Funder

National Natural Science Foundation of China

Guangdong Province Key Construction Discipline Research Ability Enhancement Project

Research Project of the Guangdong University of Science and Technology

Publisher

MDPI AG

Subject

Aerospace Engineering

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