飞机结构腐蚀维修数据库的设计与实现

在已有的腐蚀资料及相关研究的基础上,设计了飞机结构腐蚀维修数据库系统,该数据库系统包括飞机结构腐蚀维修设计所需要的各类知识,并收集了大量现实可用数据,建立了飞机腐蚀维修培训的数据基础。

腐蚀条件下新型胶体密封剂对典型飞机结构材料疲劳性能影响

针对飞机结构密封防水问题,研制了一种新型胶体密封剂。采用加速模拟环境方法,考核验证了这种胶体密封防水新技术的腐蚀防护性及其对典型飞机结构材料疲劳性能的影响。试验结果表明,与常规环境下原始疲劳寿命相比,随加速腐蚀周期增加,典型飞机结构材料疲劳寿命大幅度降低,而涂敷新型胶体密封剂后其疲劳寿命没有明显变化。新型胶体密封剂具有良好的密封防水、防腐功能,能够有效地抑制或减缓水分、腐蚀性介质的侵入,明显提高了典型飞机结构材料的抗环境腐蚀品质,适用于解决飞机结构密封防水问题。

民用飞机典型腐蚀环境区域的聚类及差异性研究

收集百余架某系列民航飞机近十年的腐蚀损伤数据,及其过夜停放的16个基地机场的气象环境指标数据,利用动态聚类分析方法,对基地机场的腐蚀环境区域进行了划分,得到对该系列飞机的腐蚀行为影响规律具有相似性的4类腐蚀环境区域。其次应用方差分析方法,对在不同类型机场环境区域的腐蚀频率进行了差异性研究。结果表明,不同机场环境区域的飞机结构腐蚀频率有显著的差异。研究成果对编制民用机场环境谱和进行腐蚀加速试验选取参数有重要的参考价值。

Application of supersonic particle deposition to enhance the structural integrity of aircraft structures

Aircraft metal components and structures are susceptible to environmental degradation throughout their original design life and in many cases their extended lives.This paper summarizes the results of an experimental program to evaluate the ability of Supersonic Particle Deposition(SPD),also known as cold spray,to extend the limit of validity(LOV)of aircraft structural components and to restore the structural integrity of corroded panels.In this study the potential for the SPD to seal the mechanically fastened joints and for this seal to remain intact even in the presence of multi-site damage(MSD)has been evaluated.By sealing the joint the onset of corrosion damage in the joint can be significantly retarded,possibly even eliminated,thereby dramatically extending the LOV of mechanically fastened joints.The study also shows that SPD can dramatically increase the damage tolerance of badly corroded wing skins.