Optimal Design of Composite Material Maintenance Structure for Aircraft Based on ANSYS Workbench

Jing Tao Dai; Pei Zhong Zhao; Hong Bo Su; Hao Dong Liu; Yu Bo Wang; Shi Kang Dong

doi:10.4028/www.scientific.net/KEM.871.216

Paper Titles

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Research and Prospect of Diamond/Aluminum Matrix Composites
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Optimal Design of Composite Material Maintenance Structure for Aircraft Based on ANSYS Workbench
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HomeKey Engineering MaterialsKey Engineering Materials Vol. 871Optimal Design of Composite Material Maintenance...

Optimal Design of Composite Material Maintenance Structure for Aircraft Based on ANSYS Workbench

Abstract:

Composite material is widely used to maintain damaged structures of aircraft. The 3D finite element model of composite cement maintenance for aircraft is established by finite element method software ANSYS Workbench. The structural characteristics and usage status of the composite cement maintenance model is analyzed, and then the optimal structural parameters of the composite patch are obtained, including the length, width and thickness. The results show that the composite cement maintenance method could effectively restore the rigidity, and improve the strength of the structure. Furthermore, the optimal design for composite patch ensures safety of aircraft, economics of maintenance, and operability of repair methods.

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Periodical:

Key Engineering Materials (Volume 871)

Pages:

216-221

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.871.216

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Online since:

January 2021

Authors:

Jing Tao Dai*, Pei Zhong Zhao, Hong Bo Su, Hao Dong Liu, Yu Bo Wang, Shi Kang Dong

Keywords:

Aircraft, Composite Materials, Finite Element

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* - Corresponding Author

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