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
           
AuthorInstitution
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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