|
| Improvement of Aircraft Structure Surface Coating System |
| Received:April 25, 2013 Revised:September 01, 2013 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2013.05.022 |
| KeyWord:aircraft structure anti-corrosion nano-composite coating interlayer adhesion accelerated simulation environment |
| Author | Institution |
| FANG Zhen-qian |
Beijing Aeronautical Technology Research Center，Beijing，China;Unit93756of PLA，Tianjin，China |
| CHEN Qun-zhi |
Beijing Aeronautical Technology Research Center，Beijing，China |
| DONG Bing |
Unit93756of PLA，Tianjin，China |
| HUANG Xue-jun |
Unit93756of PLA，Tianjin，China |
|
| Hits: |
| Download times: |
| Abstract: |
| According to the urgent issue of surface coating system with worse anticorrosion properties in several types of aircraft, the simulative components of typical aircraft skin butt joint structures were designed and painted with manufacture coating system, overhaul coating system and nano-composite coating system. The interlayer adhesion of coating system was characterized using bend test method. The corrosion protection performance of nano-composite coating was comparatively assessed and validated using laboratory accelerated simulation environment test method. The experimental results showed that the interlayer adhesion, the corrosion protection and anti-ultraviolet ageing performance of nano-composite coating system are obviously better than that of manufacture and overhaul coating system. Nano-composite coating can distinctly improve the anti-corrosion quality of aircraft skin structures in corrosive medium. |
| Close |