Optimal Design of Composite Material Maintenance Structure for Aircraft Based on ANSYS Workbench-Reference-Cited by-同舟云学术

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

Published:2021-01 Issue: Volume:871 Page:216-221
ISSN:1662-9795
Container-title:Key Engineering Materials
language:
Short-container-title:KEM

Author:

Dai Jing Tao¹,Zhao Pei Zhong¹,Su Hong Bo¹,Liu Hao Dong¹,Wang Yu Bo¹,Dong Shi Kang¹

Affiliation:

1. Naval Aviation University Qingdao branch

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.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://www.scientific.net/KEM.871.216.pdf

Reference6 articles.

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