Title :
Dynamic analysis of aircraft arresting gear based on finite element method
Author :
Lihua, Liang ; Chen, Wan ; Panpan, Xun
Author_Institution :
Coll. of Autom., Harbin Eng. Univ., Harbin, China
Abstract :
Aircraft arresting system is important auxiliary equipment on the aircraft carrier, in order to confirm the arresting force and working status of aircraft arresting gear, the mathematical models of the arresting system was established according to kink-wave impact in the cable and the theory of multi-dynamic. According to the simulation results, the finite element model is availability to analyze the dynamic behavior of the arresting gear. The simulation results provide some standpoints to the research and design of arresting gear.
Keywords :
aerospace components; aerospace safety; aircraft; cables (mechanical); finite element analysis; gears; aircraft arresting gears; aircraft carriers; arresting force; auxiliary equipments; cables; finite element method; kink wave impacts; mutidynamic theory; Aircraft; Atmospheric modeling; Force; arresting gear; cable; dynamic analysis; finite element;
Conference_Titel :
System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011 International Conference on
Conference_Location :
Guiyang
Print_ISBN :
978-1-4577-0247-1
DOI :
10.1109/ICSSEM.2011.6081253
