张勇,王晨光,卞贵学,王安东.沿海机场某型飞机典型结构件自然曝晒试验研究[J].装备环境工程,2016,13(2):92-97. ZHANG Yong,WANG Chen-guang,BIAN Gui-xue,WANG An-dong.Performance of Typical Structures of A Type of Aircraft after Natural Exposure in a Coastal Airport[J].Equipment Environmental Engineering,2016,13(2):92-97.
沿海机场某型飞机典型结构件自然曝晒试验研究
Performance of Typical Structures of A Type of Aircraft after Natural Exposure in a Coastal Airport
投稿时间:2015-10-27  修订日期:2016-04-15
DOI:10.7643/issn.1672-9242.2016.02.017
中文关键词:  飞机  结构件  自然曝晒
英文关键词:aircraft  structures  natural exposure
基金项目:
作者单位
张勇 海军航空工程学院 青岛校区,山东 青岛,266041 
王晨光 海军航空工程学院 研究生管理大队,山东 烟台,264001 
卞贵学 海军航空工程学院 青岛校区,山东 青岛,266041 
王安东 海军航空工程学院 研究生管理大队,山东 烟台,264001 
AuthorInstitution
ZHANG Yong Qingdao Branch of Naval Aeronautical Engineering Academy, Qingdao 266041, China 
WANG Chen-guang Graduate Students Brigade of Naval Aeronautical Engineering University, Yantai 264001, China 
BIAN Gui-xue Qingdao Branch of Naval Aeronautical Engineering Academy, Qingdao 266041, China 
WANG An-dong Graduate Students Brigade of Naval Aeronautical Engineering University, Yantai 264001, China 
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中文摘要:
      目的 研究某型飞机典型结构件的腐蚀机理。方法 在海南陵水机场进行自然曝晒试验, 采用表面宏观形貌记录和微观形貌表征法、 腐蚀产物物相分析等手段对基体及上覆防护体系的腐蚀、 老化性能进行评估, 进而得出该型飞机不同部位的防护性能变化规律。结果 其中试件边缘、与螺栓直接接触的部位和试件连接处涂层老化、 脱落最为严重, 涂层脱落后裸露的基体也会出现较为严重的腐蚀现象; 而一般远离螺栓、 边缘和断口的区域则涂层老化、 脱落均匀, 腐蚀程度较轻。结论 相同环境谱作用下, 受力壁板连接关键部位不同部位发生腐蚀的类型、 机理不同。
英文摘要:
      Objective To study the corrosion mechanism of typical structures of a type of aircraft. Methods Natural exposure test of typical aircraft structures were carried out in Lingshui coastal airport. The surface morphology and the composition of corrosion products were obtained by means of SEM and XRD, which were used to evaluate the corrosion and aging performance of substrate and its overlying corrosion protection system, and to obtain the changing law of the protection performance at different parts of the aircraft. Results Different parts showed different mechanism and types of corrosion even in the same environment. The coating of the specimen, which directly contacted with the edge and bolt parts, and the specimen joint showed most serious aging and falling off phenomenon, leading to serious corrosion in the exposed substrate, while the corrosion degree of other parts was lighter, with even aging and falling off of the coating. Conclusion Under the action of the same environmental spectrum, the corrosion types and mechanisms at different parts of the critical connecting structures of the force-bearing panel.
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