Optimization of Pre-Forging of the Aircraft Wheel Hub by FEM

Yan Yan Dai; Shi Qiang Lu; Ke Lu Wang; Shu Zhe Shang Guan

doi:10.4028/www.scientific.net/AMR.652-654.2029

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 652-654Optimization of Pre-Forging of the Aircraft Wheel...

Optimization of Pre-Forging of the Aircraft Wheel Hub by FEM

Abstract:

Optimization and design for shape and size of pre-forging with numerical simulation have some advantages compared with the conventional methods. The optimization object is the pre-forgings of an aircraft wheel hub. A commercially available software DEFORM 3D is used for the finite element method (FEM) simulation of the forging process of the aircraft wheel hub. The pre-forgings with three different shapes and sizes were used for numerical simulation. The effects of shape and size of the pre-forging on mould filling, forging load, effective strain and effective stress were analyzed. Finally, the suitable shape and size of the pre-forging were obtained based on the numerical simulation results.

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Periodical:

Advanced Materials Research (Volumes 652-654)

Pages:

2029-2033

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.652-654.2029

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Online since:

January 2013

Authors:

Yan Yan Dai, Shi Qiang Lu, Ke Lu Wang, Shu Zhe Shang Guan

Keywords:

Aircraft Wheel Hub, Finite Element Method (FEM), Pre-Forging, Titanium Alloy TB6

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