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Technical Requirement for Corrosion Protection of Aircraft Electrical Bonding Devices |
Received:July 18, 2024 Revised:October 21, 2024 |
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DOI:10.7643/issn.1672-9242.2025.02.005 |
KeyWord:electricalbonding device corrosion protection bonding line corrosion inspection corrosion surface treatment bonding resistance |
Author | Institution |
WANG Xibin |
School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai , China |
YU Dazhao |
School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai , China |
WANG Lin |
School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai , China |
HU Jialin |
School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai , China |
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Abstract: |
The work aims to put forward technical requirements for corrosion protection of aircraft electrical bonding devicesbased on the research of relevant standard manuals at home and abroadso as to solve the problem of corrosion affecting equipment quality and flight safety of aircraft electrical bonding devices in China. Firstly, from the principles and requirements of selection, the selection requirements for anti-corrosion of electricalbonding devices were proposed; Secondly, from the aspects of corrosion inspection, corrosion surface washing, and corrosion product cleaning, the requirements for corrosion surface treatment of the electricalbonding device were putforward; Finally, the requirements for anti-corrosion installation of electricalbonding devices were put forward from the aspects of anti-corrosion installation, bonding resistance measurement, and anti-corrosion treatment after installation. This study can provide technical guidance and implementation basis for corrosion protection in the field inspection, technical repair, and maintenance of aircraft electrical bonding devices. |
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