从实验室规模到相关环境的多功能航空涂料的发展与技术表征

L. Mazzola, G. Bruno, B. Galasso, Quaranta, F. Albano, A. Auletta, Cori
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引用次数: 5

摘要

关键飞机表面的冰附着是一个严重的潜在危险,有引发事故的风险。冻结的污染物会造成粗糙和不平整的表面,这会扰乱平稳的空气流动,大大降低机翼产生升力和增加阻力的能力。在结冰减缓系统中,被动式防冰涂层对减少冰的成核和生长、减少主动除冰系统的功耗以及燃料消耗提出了挑战。本文介绍了新型多功能涂层的先进性能和效果,该涂层具有憎冰性和美观性。特别是基于原子力显微镜和激光扫描显微镜测量的高级形态学表征以及随后的功率谱密度分析进行了评估表面粗糙度。为了确定飞行条件下的润湿性、表面自由能和附着功,进行了接触角测量。此外,还对新型多功能涂层和传统涂装涂层进行了单水滴冲击的动力学分析,以展示其在冲击过程中的不同物理行为。实验还表明,该新型多功能涂料与商用涂装涂料一样,符合航空规范,克服了环境试验。最后,利用3D打印技术设计和开发了两个NACA对称翼型。在一种情况下,表面涂有商业涂层,在另一种情况下涂有新型多功能涂层。两种翼型都在结冰风洞中进行了不同条件下的测试,以评估新型多功能涂层相对于商用涂层在减少增冰方面的有效性。测试表明,使用新的多功能涂层可以减少50%的增冰。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development and Technological Characterization of Multi-functional Aeronautical Coating From Lab-Scale to the Relevant Environment
Ice adhesion on critical aircraft surfaces is a serious potential hazard that runs the risk of causing accidents. Frozen contaminants cause rough and uneven surfaces which will disturb smooth air flow and greatly degrade the ability of the wing to generate lift and increasing drag. Amongst icing mitigation systems, passive anti-icing coatings represent a challenge to reduce the ice nucleation and growth, reducing the power consumption of the active de-icing systems and consequently the fuel consumption. In this work the advanced properties and effectiveness of the new multifunctional coating with ice-phobic and aesthetical properties are described. In particular advanced morphological characterizations based on Atomic Force Microscopy and Laser Scanning Microscopy measurements as well as subsequent Power Spectral Density analysis were performed to evaluate the surface roughness. Contact angle measurements were executed in order to determine the wettability and surface free energy as well as work of adhesion in flight conditions. In addition, dynamic analysis of the impact of single water droplets on the new multifunctional coating and the classical livery coating were performed in order to demonstrate the different physical behavior during the impingement. It was also demonstrated that the new multifunctional coating overcome the environmental test similarly to the commercial livery coating in accordance with the aeronautical specification. Finally, two NACA symmetric airfoils were design and developed using 3D printing technology. The surfaces were coated with a commercial coating in one case and with the new multifunctional coating in the other case. Both airfoils were tested in the Icing Wind Tunnel at different conditions in order to evaluate the effectiveness, in terms of reduction of accreted ice, of the new multifunctional coating respect to the commercial one. Tests demonstrated the reduction of accreted ice of 50% using the new multifunctional coating.
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