Simulation Analysis and Fault Simulation of Aircraft Landing Gear Retraction Hydraulic System based on Model

Qichao Duan, Shentianyu Zhou, Fangyi Wan, Yudong Qiang, Yipeng Zong

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

3 Scopus citations

Abstract

In this paper, the AMEsim software is used as the simulation platform to study the retraction hydraulic system of aircraft landing gear. The composition and working principle of the aircraft landing gear retraction hydraulic system are introduced. Then, the retraction hydraulic system model of the aircraft landing gear is established by using the hydraulic library, hydraulic component library, and mechanical library provided by the AMEsim software, and the simulation analysis method is used. By changing the parameters of the hydraulic pump, oil filter, retractable actuator, electromagnetic directional valve and other modules, the failure of the corresponding module is simulated and its influence is analyzed.

Original languageEnglish
Title of host publication2022 Global Reliability and Prognostics and Health Management Conference, PHM-Yantai 2022
EditorsWei Guo, Steven Li
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781665496315
DOIs
StatePublished - 2022
Event2022 Global Reliability and Prognostics and Health Management Conference, PHM-Yantai 2022 - Yantai, China
Duration: 13 Oct 202216 Oct 2022

Publication series

Name2022 Global Reliability and Prognostics and Health Management Conference, PHM-Yantai 2022

Conference

Conference2022 Global Reliability and Prognostics and Health Management Conference, PHM-Yantai 2022
Country/TerritoryChina
CityYantai
Period13/10/2216/10/22

Keywords

  • AMEsim
  • failure
  • retraction hydraulic system of aircraft landing gear
  • simulation

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