DocumentCode
2341287
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
Volume
2
fYear
2011
fDate
22-23 Oct. 2011
Firstpage
118
Lastpage
121
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;
fLanguage
English
Publisher
ieee
Conference_Titel
System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011 International Conference on
Conference_Location
Guiyang
Print_ISBN
978-1-4577-0247-1
Type
conf
DOI
10.1109/ICSSEM.2011.6081253
Filename
6081253
Link To Document