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Research on redundancy design of a certain aircraft hydraulic system based on goal-oriented methodology

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Abstract

Aircraft hydraulic system is one of the key flight control subsystems to control aircraft flight attitude and flight trajectory. The reliability and safety of aircraft hydraulic system are the priorities of aircraft reliability design. Redundancy design is highly effective to improve the system’s reliability and safety. This paper studies the redundancy design method of the aircraft hydraulic system based on goal-oriented (GO) methodology, putting forward a GO analysis and design method, and constructing the GO chart of aircraft hydraulic system with multi-component redundancy parameter. Meantime, the system reliability model with redundancy parameter is obtained, and the related theory of high reliability aircraft hydraulic system design is enriched. The results show that the redundancy design and analysis method of aircraft hydraulic system based on GO methodology is effective and novel, which can accurately and quickly obtain the best redundancy design scheme of the system.

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Acknowledgements

This work was supported by the National Natural Science Foundation of China (Grant No. 52177042), the Hebei Provincial Key Research and Development Program (Grant No. 21312102D), the Hebei Key Project of Science and Technology Research for Universities (Grant No. ZD2022162), the Fundamental Research Funds for the Central Universities (Grant No. 2022MS095), and the Top Youth Talent Support Program of Hebei Province ([2018]-27).

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Authors and Affiliations

  1. Department of Mechanical Engineering, North China Electric Power University, 689# Hua-Dian Road, Lian-Chi District, Baoding, 071003, China

    Hai-Peng Wang, Xiao-Long Wang & Yu-Ling He

  2. School of Mechanical Engineering, Dalian University of Technology, 2# Ling-Gong Road, High-Tech District, Dalian, 116024, China

    Fu-Hai Duan & Jun Ma

  3. Hebei Key Laboratory of Electric Machinery Health Maintenance Failure Prevention, North China Electric Power University, 689# Hua-Dian Road, Lian-Chi District, Baoding, 071003, China

    Hai-Peng Wang, Xiao-Long Wang & Yu-Ling He

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  1. Hai-Peng Wang
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  2. Fu-Hai Duan
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Correspondence to Yu-Ling He.

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Wang, HP., Duan, FH., Ma, J. et al. Research on redundancy design of a certain aircraft hydraulic system based on goal-oriented methodology. Int J Syst Assur Eng Manag 14, 343–352 (2023). https://doi.org/10.1007/s13198-022-01800-4

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  • DOI: https://doi.org/10.1007/s13198-022-01800-4

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