Research on the Chassis of Aircraft Recovery Trailer Based on ANSYS

Zhi Hua Xu; Qi Chao Du; Zhen Yu Hong

doi:10.4028/www.scientific.net/AMM.670-671.819

Paper Titles

Research on Time-Domain Dynamic Response of Tension Leg Platform in Regular Wave
p.801

Determination of Settling Velocity of Suspended Sediment in Estuary
p.805

Analysis on the Selection of Tooth Number for Closed Differential Planetary Gear Transmission Mechanism and Software Development
p.809

Optimization Design of Rapid-Cooling Mixer of By-Pass System of Cement Production Based on CFD
p.814

Research on the Chassis of Aircraft Recovery Trailer Based on ANSYS
p.819

Numerical Study on the Ballistic Impact on Lightweight Composite Armour
p.824

Structure Design of Manipulator for Pot Seedling Transplanter and Simulation Analysis
p.829

Study on Flexible Spin-Up Maneuver with Variable Cross-Section Based on Positional FEM
p.834

Numerical Investigation on Resistance Reducing Effect by Mass Injection through Porous Wall
p.838

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 670-671Research on the Chassis of Aircraft Recovery...

Research on the Chassis of Aircraft Recovery Trailer Based on ANSYS

Abstract:

The traditional method of finite element that fixing constraint between suspension and chassis for the damaged aircraft recovery trailer chassis usually ignored the buffer function of suspension leading to too much stress, So aiming at that problem The constraint of trailer is fixed by the method of balance frame system. Based on FE-software ANSYS the FE module of trailer chassis and balance frame system is set up and their node is coupled by the force analysis of aircraft with half of fuel in damaged. It's result that the maximum stress is less than permissible stress.The result show that the method of balance frame system is more practical by computer simulation.

You might also be interested in these eBooks

Applied Mechanics, Materials and Manufacturing IV

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 670-671)

Pages:

819-823

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.670-671.819

Citation:

Cite this paper

Online since:

October 2014

Authors:

Zhi Hua Xu, Qi Chao Du, Zhen Yu Hong*

Keywords:

Aircraft Recovery Trailer, ANSYS, Chassis

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Jingqi Li. Aircraft rescue vehicle: China, 1511759[P], 2004-7-14.

Google Scholar

[2] Rongtian Li, Suguang Yang. Aircraft rescue trailer: China, 202046441U[P], 2011-11-23.

Google Scholar

[3] Jinghong Zhang, Yongzhi Yu. Research of combined connecting devices with aircraft resuce trailer based on ADAMS and ANSYS[J]. Journal of Machine Design, 2012, 06: 19-22. In Chinese.

Google Scholar

[4] Xianbin Du, Weichun Zhang. Finite Element Analysis and Topology Optimization of Mine Semi-trailer Frame [J]. Coal Mine Machinery, 2013, 01: 113-114. In Chinese.

Google Scholar

[5] Dongjie Zhao, Chunjiang Bao，Lipeng Zhang．Analysis and Optimization of Agricultural Vehicle Frame Structure [J]. Machine Design and Research, 2010, 26(2): 48-50. In Chinese.

Google Scholar

[6] Xingmin Liu. Three column-hydraulic module assembled trailer's loading problem study and Lightweight design [D]. Wuhan: Wuhan University of Technology, 2011. In Chinese.

Google Scholar

[7] Xinmin Wang，Yiqiang Li，Hongwei Xu．ANSYS Structural analysis unit and application. China Communications Press[M], 2011, 5: 27-30. In Chinese.

Google Scholar