A Detection and Repair Method for Aircraft Structure Damaged by Elcetric Shock Burn
Pages 159 - 165
Abstract
There is a need for a civil aircraft structure damaged by electric shock burn to find a simple damage detection and repair method. The current research are all about the aircraft structure damaged by fire burn and few research about the aircraft structure damaged by electric shock burn. Therefore, the present article adopts a hardness detection method to determine the hardness influence range of electric short burn for 7075-T6 aluminum alloy. Then conduct static and fatigue tests for the damaged material to research the static and fatigue property variation rules for the damaged material by electric short burn. Finally, combined with the hardness detection results and static and fatigue test analysis results, the present article proposes an aircraft structure damaged by electric shock burn detection and repair method.
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Index Terms
- A Detection and Repair Method for Aircraft Structure Damaged by Elcetric Shock Burn
Index terms have been assigned to the content through auto-classification.
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Published In
December 2020
687 pages
ISBN:9781450388665
DOI:10.1145/3452940
Copyright © 2020 ACM.
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Association for Computing Machinery
New York, NY, United States
Publication History
Published: 17 May 2021
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ICITEE2020
ICITEE2020: The 3rd International Conference on Information Technologies and Electrical Engineering
December 3 - 5, 2020
Hunan, Changde City, China
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