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.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.