Optimal Design of a Hydraulic Suspension Mechanism of Aircraft Recovery Vehicle

Zhen Yu Hong; Peng Fei Zhang; Zhi Hua Xu

doi:10.4028/www.scientific.net/AMM.670-671.886

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 670-671Optimal Design of a Hydraulic Suspension Mechanism...

Optimal Design of a Hydraulic Suspension Mechanism of Aircraft Recovery Vehicle

Abstract:

Through theoretical analysis of a suspension mechanism used for aircraft recovery vehicle, the mapping relationship between the hydraulic cylinder axial force and scale parameters of the suspension mechanism was built. With coordinate values of each hinge joint of the suspension mechanism in the initial position as design variables, the minimum hydraulic cylinder axial force was taken as evaluating index with reasonable constraints and optimal design of the hydraulic suspension mechanism was studied. The influence law of scale parameters to the axial force was discussed and coordinate alternation method was applied to find the optimal solution. The effectiveness of the method was indicated by an example.

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Periodical:

Applied Mechanics and Materials (Volumes 670-671)

Pages:

886-891

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.670-671.886

Citation:

Cite this paper

Online since:

October 2014

Authors:

Zhen Yu Hong, Peng Fei Zhang*, Zhi Hua Xu

Keywords:

Aircraft Recovery Vehicle, Hydraulic Suspension Mechanism, Optimal Design

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* - Corresponding Author

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