天线罩表面金属纳米涂层红外隐身性能分析

Yongwoo Lee, Injoong Chang, Juyeong Nam, H. Bae, H. Cho
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摘要

飞机红外隐身技术是利用内部散热片、低发射率材料或超材料,通过控制飞机表面温度和发射率来降低红外信号的技术。然而,在飞机的一个部分,这种技术的使用是有限的,那就是天线罩。特别是天线罩对于特定的射频要有透射率,因此发射率控制面等常见的隐身技术不能应用于天线罩表面。在本研究中,我们开发了一种适用于雷达罩表面的红外隐身金属纳米涂层。我们设计了狭缝型模式,用于x波段的频率选择传输,并控制金属纳米涂层的厚度,用于控制长波红外发射率。结果表明,雷达罩红外隐身表面的x波段透过率为93.2%,红外发射率随纳米涂层厚度的变化范围为0.17 ~ 0.57。通过数值模拟分析了雷达罩的红外特征,与聚氨酯表面相比,雷达罩的对比辐射强度降低了97.57%。
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Analysis on Infrared Stealth Performance of Metal Nano-coating on Radome Surface
Infrared stealth technology used in aircraft is applied to reduce the infrared signal by controlling surface temperature and emissivity using internal heat sink, low emissivity material or metamaterial. However, there is one part of the aircraft where the use of this technology is limited, and that is the radome. Especially, radome should have transmittance for the specific radio frequency, therefore, common stealth technology such as emissivity control surfaces cannot be applied to radome surface. In this study, we developed metal nano-coating for infrared stealth which is applicable to radome surface. We designed slot-type pattern for frequency selective transmission in X-band, and also controlled thickness of metal nano-coating for long wavelength infrared emissivity control. As a result, our infrared stealth surface for radome has 93.2 % transmittance in X-band and various infrared emissivities from 0.17 to 0.57 according to nano-coatings thickness. Also, we analyzed infrared signature of radome through numerical simulation, and finally reduced contrast radiant intensity by 97.57 % compared to polyurethane surface.
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