Dynamic Response Analysis of the Hydraulic Pipe under Jets of the Aircraft Tire Burst

Run Lian Jiang; Yao Hua Wang; Cheng Fei Fan; Mian Jun Duan

doi:10.4028/www.scientific.net/AMR.798-799.341

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 798-799Dynamic Response Analysis of the Hydraulic Pipe...

Dynamic Response Analysis of the Hydraulic Pipe under Jets of the Aircraft Tire Burst

Abstract:

The finite element model of an aircraft hydraulic pipe was established in this paper. Based on LS-Dyna software equivalent static pressure and peak pressure surface loads on the tire burst test (main landing gear retracted state, and did not consider the impact of tire debris) jets were applied to the hydraulic pipe. Both stress and strain contours of hydraulic pipe were obtained under dynamic loading. Plastic strain occurred under both loads on the hydraulic pipe, and the peak pulse loads were more severe than equivalent static loads, the maximum strain reached 0.41172 under the peak pulse loads. However, in both cases the pipe is not broken.

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Periodical:

Advanced Materials Research (Volumes 798-799)

Pages:

341-344

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.798-799.341

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Online since:

September 2013

Authors:

Run Lian Jiang, Yao Hua Wang, Cheng Fei Fan, Mian Jun Duan

Keywords:

Aircraft Tire, Burst, Dynamic Response, Hydraulic Pipe, Jet Flow

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References

[1] Information on http: /www. easa. europa. eu.

Google Scholar

[2] L.Y. Gu and J.W. He: Aircraft Design, Vol. 29 (2009) No . 2, p.29. (In Chinese).

Google Scholar

[3] T. He,J. Yang and X. Jin: ANSYS 10. 0/LS-DYNA Nonlinear Finite Element Analysis Instances Tutorial (China Machine Press, BeiJing 2007) (In Chinese).

Google Scholar

[4] Y. H. Pao and A.N. Ceranoglu : Journal of Applied Mechanics, Vol. 5(1978) No . 5, p.114.

Google Scholar

[5] D.L. Preston and D.C. Wallace: Solid State Commun, Vol. 81(1992) No. 3, p.277.

Google Scholar

[6] Information on http: /www. suppliersonline. com.

Google Scholar