成膜防腐化合物对铆接接头疲劳影响的实验研究

Eugene Gavrylov
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摘要

本文的主题是成膜防腐蚀化合物对航空铆接疲劳寿命的影响。这项工作的目标是开发一种方法,用于评估应用防腐蚀化合物所造成的负面影响。这项工作的任务如下:分析飞机腐蚀问题;批判性审查有关应用防腐蚀化合物保护航空铆接接头免受腐蚀可能造成的负面影响的现有出版物,其中将疲劳寿命缩短视为防腐蚀化合物渗入铆接接头缝隙的结果;开发具有当代运输机典型设计特征的疲劳试验试样;对经过防腐蚀化合物处理和未经过处理的铆接试样进行疲劳试验;调查防腐蚀化合物渗入铆接接头缝隙的情况。这项研究的主要方法是对铆接试样进行疲劳加载,加载载荷接近飞机服役时遇到的载荷。主要结果是实验证明了使用防腐蚀化合物可能会产生负面影响。所观察到的影响可以用接合处摩擦力的变化以及接合元件之间力的相应重新分布来解释。研究发现,影响摩擦力的一个因素是防腐蚀化合物的粘度。实验证明,可以通过优化保护程序来防止负面影响。结论。本文的研究结果表明,使用防腐蚀化合物可能会产生负面影响。考虑到这些材料的多样性及其物理和化学特性,显然有必要对保护化合物进行合理选择,并对处理技术进行优化。已开展的研究揭示了预防性化合物对铆接接头疲劳寿命的负面影响,并为预防这种影响开辟了道路。所述研究程序是探索防腐蚀化合物负面影响的复杂方法的组成部分。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Експериментальне дослідження впливу плівкоутворюючих антикорозійних сполук на втому заклепкових з’єднань
The subject matter of this article is the influence of film-forming corrosion preventive compounds on aviation riveted joints fatigue life. The goal of this work is to develop a method for the assessment of negative side effects caused by the application of corrosion preventive compounds. Tasks of the work are as follows: analysis of the aircraft corrosion problem; critical review of existing publications concerning possible negative side effects caused by the application of corrosion preventive compounds  for protection of aviation riveted joints against corrosion, where reduction of the fatigue life is considered as a result of the preventive compounds penetration into the gaps of riveted joints; development of the specimen for fatigue tests, with features of contemporary transport aircraft typical design; fatigue tests of the riveted specimens treated with preventive compounds and without treatment; investigation of the preventive compounds penetration into the gap of riveted joint. The main method of this research is fatigue loading of the riveted specimens at loads close to those the aircraft encounters in service. The main result is the experimentally proven possibility of negative side effects of corrosion preventive compound application. The observed effect is explained by the change in friction in joints and the corresponding redistributions of the forces between the joint elements. It was found that a factor influencing friction force is the viscosity of the preventive compounds. The possibility of preventing negative side effects by optimizing the protective procedure has been experimentally proven. Conclusions. The results presented in the paper show the probability of the negative side effects of corrosion preventive compound application. Considering the variety of these materials and their physical and chemical characteristics, the necessity   of the grounded selection of the protective compounds is evident as well as the optimization of the treatment technology. Conducted research has revealed an example of the negative influence of preventive compounds on riveted joints fatigue life and has opened the way for this effect prevention. The described research procedure is a component of the complex method for exploring corrosion preventive compounds’ negative side effects.
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