The Strength Analysis of Aircraft Landing Gear Strut Based on ANSYS

Fei Chen; Yong Lv; Zhi Wei Xing

doi:10.4028/www.scientific.net/AMR.490-495.2686

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 490-495The Strength Analysis of Aircraft Landing Gear...

The Strength Analysis of Aircraft Landing Gear Strut Based on ANSYS

Abstract:

Because the landing gear structure is complicated, it is difficult to draw accurate stress and strain distribution through the theoretical calculation. In this paper, based on the modeling and stress analysis of the buffer mechanism of aircraft landing gear, by converting the stress of a dynamic system into a static stress, the force of the landing gear struts are calculated. This paper analyzes the strength of the aircraft main landing gear by using computer simulation technology and finite element analysis, it provides an effective basis for maintenance and the damage prediction

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Periodical:

Advanced Materials Research (Volumes 490-495)

Pages:

2686-2690

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.490-495.2686

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Cite this paper

Online since:

March 2012

Authors:

Fei Chen, Yong Lv, Zhi Wei Xing

Keywords:

Aircraft Landing Gear, ANSYS, Side Strut, Simulation, Stress

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References

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