Aircraft Landing Gear of a Dynamic Research and Computer Simulation

Shen Shou Li; Xiao Ming Liu; Zhong Gan Zhu; Fang Yang

doi:10.4028/www.scientific.net/AMR.383-390.2426

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 383-390Aircraft Landing Gear of a Dynamic Research and...

Aircraft Landing Gear of a Dynamic Research and Computer Simulation

Abstract:

by the MSC Adams / Aircraft software features, setting pillar-type landing gear as the prototype, and using ADAMS software modules prior to the establishment of a certain type of aircraft landing gear model, then calculate the air buffer spring force oil, damping force and the structural constraints force curve based on dynamics model, At the end of paper we will analyze the model drop-test results. The results proved that we used this method was feasible.

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Manufacturing Science and Technology, ICMST2011

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Periodical:

Advanced Materials Research (Volumes 383-390)

Pages:

2426-2429

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.383-390.2426

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Online since:

November 2011

Authors:

Shen Shou Li, Xiao Ming Liu, Zhong Gan Zhu, Fang Yang

Keywords:

ADAMS/Aircraft, Buffer, Landing Gear, Simulation

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References

[1] Zheng Jian-Rong. ADAMS-virtual prototype technology and improve the introduction [M]. beijing: mechanical industry press, 2002. 205 ~ 229.

Google Scholar

[2] Wan Xiao-peng, Hou chi, Zhao Mei-ying. Development of Auto-Modeling Program Based on ADAMS Marcos for Aircraft Landing gear Dynamic Loads Simulation Analysis. 2009 Second International Conference on Intelligent Computation Technology and Automation, (2009).

DOI: 10.1109/icicta.2009.242

Google Scholar

[3] The plane design manual total plane design manual. 14, take-off landing system design. Beijing: aviation industry press, (2002).

Google Scholar

[4] Zhi Chao-you, Gao Ya-kui, Li Xia. A Distributed System for Aircraft Hydraulic System Simulation Test Based on LXI. IEEE AUTOTESTCON 2008. Salt Lake City, UT, 8-11 September (2008).

DOI: 10.1109/autest.2008.4662609

Google Scholar

[5] Nicholas, Joseph L. Advanced dynamic simulations for determination of Landing gear loads, Annual Forum Proceedings-AHS International, Vol. 2007, P1028-1036, EI: 20073410771455.

Google Scholar

[6] ADAMS USER'S MANUAL, SC. Software Corporation, (2005).

Google Scholar

[7] Aerospace industry science and technology commission. Aircraft landing gear strength design guidelines [M]. Chengdu, sichuan science and technology press, 1989. 646 ~ 654.

Google Scholar

[8] Yang Chun-Sheng, Huang Dan. Based on the Matlab aircraft landing gear dynamic simulation analysis, aviation 2006. 07 computer technology.

Google Scholar

[9] Liu hui, semi-active control technology of landing gear shock absorption system, PhD thesis, Nanjing University of Aeronautics and Astronautics, Nanjing, China, December. (2007).

DOI: 10.7498/aps.60.010506

Google Scholar