The Strength Analysis of the Diagonal Stay of Aircraft Landing Gear Based on ANSYS

DOI

10.2991/emeit.2012.176How to use a DOI?

Keywords

Simulation, ANSYS, Aircraft landing gear, Diagonal stay, Stress

Abstract

As the landing gear structure is complicated, it is difficult to draw accurate stress and strain distribution through the theoretical calculation. This paper carries on modeling and force analysis to the buffer mechanism of aircraft landing gear, transforms the stress problem dynamic system into static stress problem according to D'Alembert principle and analyzes the diagonal stay of landing gear, and at the same time, analyzes the strength of an aircraft main landing gear by using computer simulation technology and finite element analysis technology, which provides effective basis for damage prediction and practical maintenance.

Copyright

© 2012, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Ying XING
PY  - 2012/09
DA  - 2012/09
TI  - The Strength Analysis of the Diagonal Stay of Aircraft Landing Gear Based on ANSYS
BT  - Proceedings of the 2nd International Conference on Electronic & Mechanical Engineering and Information Technology (EMEIT 2012)
PB  - Atlantis Press
SP  - 822
EP  - 826
SN  - 1951-6851
UR  - https://doi.org/10.2991/emeit.2012.176
DO  - 10.2991/emeit.2012.176
ID  - XING2012/09
ER  -