飞机迎风面蒙皮涂层高动态雨蚀损伤评价和机理OA
Evaluation and Mechanism of Highly Dynamic Rain Corrosion Damage to Aircraft Windward Side Skin Coatings
目的 飞机在雨中高速飞行时,机体迎风面蒙皮涂层受到雨滴冲击作用而产生损伤,出现表面开裂、剥离等典型损伤,会降低结构的安全性和功能性,因此需要对蒙皮涂层的雨蚀损伤机理进行深入研究.方法 利用一级轻气炮搭建的单射流试验平台和水切割装置改装的多射流试验平台模拟雨滴冲击.针对以碳纤维T300编制材料为基体,表面涂有3 种同等厚度的聚氨酯涂层材料,在不同试验条件下对材料进行雨蚀试验研究.结果 在 617 m/s冲击速度条件下,以 0°、15°、30°的冲击角度以及在 15°冲击角度,430、490 和555 m/s的冲击速度下对三种涂层材料进行单射流试验;对三种涂层材料在 350、370和420 m/s的冲击速度下,进行 1 000 次冲击的多喷射流试验.结果表明:随着冲击角度和速度的变化,三种涂层材料的损伤趋势是一致的;典型损伤形貌相同,即当水锤压力低于涂层材料的屈服强度极限时,损伤区域由环形损伤包围中央未损伤区域构成;当水锤压力超过材料的屈服强度极限时,水锤压力结合侧向射流会造成 1~2 倍液滴直径的损伤区域.多射流与单射流的试验结果具有相似性.结论 通过对比单射流与多射流试验下涂层材料的典型损伤形貌可知,材料的雨蚀损伤机理与自身的力学性能关系密切.根据三种涂层材料在不同试验参数下的损伤结果,材料1性能最佳,在多种试验条件下均有良好的表现,能够满足飞机在不同环境下的飞行需求.
When an aircraft flies at high speed in the rain,the skin coating on the windward side of the fuselage is damaged by the impact of raindrops.In order to ensure the safety of flight,the rain erosion damage mechanism of the skin coating is studied in depth.To simulate the raindrop impact,a single-jet test platform constructed by a first-class light-air gun and a multi-jet test platform modified by a water-cutting device were utilized.Rain erosion tests were conducted on the materials under different experimental conditions,where the substrate is made of carbon fiber T300 woven fabric,and its surface is coated with three types of polyurethane coating materials of equal thickness.Single-jet flow tests were performed on three coating materials at an impact velocity of 617 m/s and impact angles of 0°,15°,and 30° as well as on three coating materials at impact velocities of 430,490,and 555 m/s and an impact angle of 15°.Multi-jet flow tests were performed on three coating materials at impact velocities of 350,370,and 420 m/s with 1 000 impacts.The results showed that,with the change of impact angle and velocity,the damage trend of the three coating materials was consistent and the typical damage morphology was the same.For example,when the water hammer pressure was lower than the yield strength limit of the coating material,the damage area consisted of a ring-shaped region encircling the central uninjured area,and when the water hammer pressure was higher than the yield strength limit of the material,the combination of the water hammer pressure with the lateral jet would cause a damage area 1-2 times the diameter of the liquid droplet.Under the impact of a single jet,the damage profile of the coating material was not symmetrical,and the damage profile in the transverse direction was larger than that in the longitudinal direction.This occurred because the jet was affected by gravity during flight,which produced a downward drop,resulting in hindered lateral jet propagation in the vertical direction.Under the impact of multiple jets,the damage critical velocities of materials 1 and 2 were in the range of 320-350 m/s and the damage critical velocity of material 3 was slightly lower than 320 m/s.Different materials produced distinct erosion pit shapes under the impact of multiple jets.These shapes affected further erosion differently:flat-bottomed pits promoted erosion,while sharp-bottomed pits mitigated it.There was a similarity between the test results for single and multiple jets.Comparing the typical damage morphology of the coating materials under single-jet and multi-jet tests,it was found that the rain-etching damage mechanism of the materials was closely related to their own mechanical properties,but not to the impact mode.Based on the damage results of the three coating materials under different test parameters of single and multiple jets,material 1 performs best under different rain field impacts simulated by the test and can adapt to the aircraft under different flight conditions.
沙明工;Tkhabisimov Aleksandr;李玉龙;陈建军;惠志强;李雨桐;孙莹;李明;魏政;Babaytsev Arseny;Fedotenkov Gregory;Mednikov Aleksei
西北工业大学 民航学院,西安 710072西北工业大学太仓长三角研究院,江苏 苏州 215400国立研究大学莫斯科动能学院,莫斯科 111250 俄罗斯西北工业大学 民航学院,西安 710072西北工业大学太仓长三角研究院,江苏 苏州 215400杭州萧山技师学院,杭州 310000西北工业大学 民航学院,西安 710072西北工业大学 民航学院,西安 710072莫斯科航空学院国立研究大学,莫斯科 125993 俄罗斯航空综合环境航空科技重点实验室,北京 100028中国航空综合技术研究所,北京 100028中航工业集团公司济南特种结构研究所,济南,250104
矿业与冶金
液固冲击雨蚀损伤水射流冲击动力学复合材料涂层
liquid-solid impactrain erosion damagewater jetsimpact dynamicscompositescoatings
《表面技术》 2026 (2)
1-14,14
国家自然科学基金资助项目(12261131505,U2241274)俄罗斯科学基金(23-49-00133)航空科学基金项目(20240002053002)陕西省自然科学基础研究计划(2025JC-YBMS-005)陕西省重点研发计划项目(2024GX-YBXM-037)太仓市基础研究项目(TC2024JC10)The National Natural Science Foundation of China(12261131505,U2241274)Russian Science Fund(23-49-00133)Aeronautical Science Foundation of China(20240002053002)Natural Science Basic Research Program of Shaanxi(2025JC-YBMS-005)Key Research and Development Program of Shaanxi(2024GX-YBXM-037)Basic Research Programs of Taicang(TC2024JC10).
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