Fatigue Life Simulation on Forestay Bar of Aircraft Landing Gear

Xiang Feng Li; Jin Dong Chen; Dun Wen Zuo

doi:10.4028/www.scientific.net/KEM.431-432.29

Paper Titles

Numerical Simulation of the Prestressed Laser Welding of 7075－T7451 Aluminum Alloy Sheet
p.13

Preparation and Evaluation of Hydrophilic Fixed Abrasive Pad
p.17

Simulation of Gas Flow Field in HFCVD System for CVD Diamond Growth
p.21

Experimental Research on Cutting of Silicon with Fixed Diamond Wire Saw
p.25

Fatigue Life Simulation on Forestay Bar of Aircraft Landing Gear
p.29

Effect of Anisotropy on Chemical Mechanical Polishing of LBO Crystal
p.33

Research on High-Speed Preparation of Micro-Nanocrystalline Diamond Film
p.37

Rapid Parameter Optimization of High Speed Milling Aluminum Alloy Thin-Walled Workpiece
p.41

Modeling and Analyzing the Temperature Field of the Swing Substrate in Miniature EACVD System
p.45

HomeKey Engineering MaterialsKey Engineering Materials Vols. 431-432Fatigue Life Simulation on Forestay Bar of...

Fatigue Life Simulation on Forestay Bar of Aircraft Landing Gear

Abstract:

Firstly, taking the stability of the forestay bar as the restraint, the section area of the forestay bar was optimized from 1800 mm2 to 1178 mm2, with reduced weight of 16.1%. Secondly, the equivalent load of the forestay bar was obtained by using dynamics simulation software. Finally, the stress field and the fatigue life of the forestay bar were simulated. The results show that stress of the forestay bar with 929MPa can meet the requirement for its material strength, and fatigue life of 51200 times also satisfies the request of the nose landing gear. That is, material property of the forestay bar is utilized more than before, and its weight decreased successfully.

You might also be interested in these eBooks

Machining and Advanced Manufacturing Technology X

View Preview

Info:

Periodical:

Key Engineering Materials (Volumes 431-432)

Pages:

29-32

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.431-432.29

Citation:

Cite this paper

Online since:

March 2010

Authors:

Xiang Feng Li, Jin Dong Chen, Dun Wen Zuo

Keywords:

Fatigue Life, Forestay Bar, Landing Gear, Size Optimization

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] X.F. Wang and Y.J. Wang: Science Technology and Engineering Vol. 8 (12) (2008), pp.3243-3245. (In Chinese).

Google Scholar

[2] Y.C. Liu: Finite Elements in Analysis and Design, Vol. (44) (2008), pp.139-147.

Google Scholar

[3] C. Ren, X.P. Wan and M.Y. Zhao: Science Technology and Engineering, Vol. 8 (7) (2008), pp.1727-1731. (In Chinese).

Google Scholar

[4] Q. Ji: Research on Fatigue Reliability Analysis Method of Aircraft Landing Gear (M.E. Nanjing University of Aeronautics and Astronautics, 2007). (In Chinese).

Google Scholar

[5] H.T. Wang and J.T. Xing: Journal of System Simulation, Vol. 20 (22) (2008), pp.6261-6264.

Google Scholar