王希彬,郁大照,王琳,胡家林.飞机电搭接装置腐蚀防护技术要求[J].装备环境工程,2025,22(2):40-45. WANG Xibin,YU Dazhao,WANG Lin,HU Jialin.Technical Requirement for Corrosion Protection of Aircraft Electrical Bonding Devices[J].Equipment Environmental Engineering,2025,22(2):40-45.
飞机电搭接装置腐蚀防护技术要求
Technical Requirement for Corrosion Protection of Aircraft Electrical Bonding Devices
投稿时间:2024-07-18  修订日期:2024-10-21
DOI:10.7643/issn.1672-9242.2025.02.005
中文关键词:  电搭接装置  腐蚀防护  搭接线  腐蚀检查  腐蚀表面处理  搭接电阻中图分类号:TG174 文献标志码:A 文章编号:1672-9242(2025)02-0040-06
英文关键词:electricalbonding device  corrosion protection  bonding line  corrosion inspection  corrosion surface treatment  bonding resistance
基金项目:
作者单位
王希彬 海军航空大学 航空基础学院,山东 烟台 264001 
郁大照 海军航空大学 航空基础学院,山东 烟台 264001 
王琳 海军航空大学 航空基础学院,山东 烟台 264001 
胡家林 海军航空大学 航空基础学院,山东 烟台 264001 
AuthorInstitution
WANG Xibin School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai 264001, China 
YU Dazhao School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai 264001, China 
WANG Lin School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai 264001, China 
HU Jialin School of Basic Science for Aviation, Naval Aviation University, Shandong Yantai 264001, China 
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中文摘要:
      为解决我国飞机电搭接装置腐蚀影响装备质量和飞行安全的问题,在国内外相关标准手册研究基础上,提出了飞机电搭接装置腐蚀防护技术要求。首先,从选用原则和要求方面,提出了电搭接装置防腐蚀选型要求;其次,从腐蚀检查、腐蚀表面清洗和腐蚀产物清理等方面,提出了电搭接装置腐蚀表面处理要求;最后,从防腐蚀安装、搭接电阻测量和安装后的防腐蚀处理方面,提出了电搭接装置防腐蚀安装要求。该研究可为飞机电搭接装置外场检查、技术修理和维护使用中的腐蚀防护提供技术指导和实施依据。
英文摘要:
      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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