首页> 外文会议>International Conference on Mechanics and Mechatronics >Numerical simulation study on the coating damage of aluminum alloy lap joints surface
【24h】

Numerical simulation study on the coating damage of aluminum alloy lap joints surface

机译:铝合金搭接接头表面涂层损伤的数值模拟研究

获取原文

摘要

Galvanic corrosion will happen when the top coating of aluminum alloy joint-structures which abound in the aircraft damages. The corrosion type of aircraft materials is atmospheric corrosion that is the electrochemical corrosion under the thin layer electrolyte. The electrochemical properties of the materials covered with the 0.5mm thick film by self-made electrochemical measurement device have been researched in this paper. The potential distribution and corrosion rate of lap joints after the coating damaged have been calculated by BEASY. The simulation results show that the closer to the bolts,the greater the current density of aluminum alloy, the faster the corrosion rate; the corrosion rate is closely related to the coating damage area, the smaller the damage area,the bigger the corrosion rate in the region of coating damage.
机译:当飞机损坏中取比的铝合金接头结构的顶部涂层时,将发生电流腐蚀。腐蚀类型的飞机材料是大气腐蚀,是薄层电解质下的电化学腐蚀。本文研究了通过自制造电化学测量装置覆盖着0.5mm厚膜的材料的电化学性质。通过Beasy计算涂层损坏后LAP关节的电位分布和腐蚀速率。仿真结果表明,螺栓越靠近铝合金的电流密度越大,腐蚀速率越快;腐蚀速率与涂层损伤区域密切相关,损伤区域越小,涂层损坏区域中的腐蚀速率越大。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号