红外与激光工程, 2016, 45 (2): 0204001, 网络出版: 2016-04-05
红外窗口气动热辐射效应评估方法
Evaluation method for aero-thermo-radiation effect of IR window
摘要
气动热辐射效应导致红外探测制导系统的性能降低甚至失效,而红外窗口是气动热辐射效应评估的关键因素。通过分析红外辐射在红外窗口中的传输特性,提出一种红外窗口气动热辐射效应评估方法,基于等温状态试验,评估了某超音速飞行器红外探测系统蓝宝石红外窗口在中波3.7~4.8 μm波段的气动热辐射效应。研究结果显示,红外窗口暴露于大气环境后,蓝宝石窗口导致的气动热辐射效应迅速上升,表现为红外窗口透过率下降约10%,仍然在0.9以上,而自辐射迅速增强约458倍,相当于约125 ℃黑体,在探测器获取总辐射中的比例大于78%。在对地探测应用中,对于厚度小于20 mm的蓝宝石红外窗口,窗口温度在100~350 ℃范围内,随着厚度增加,透过率下降,自辐射增强,总辐射也增强,自辐射在总辐射中的比例增加,易造成探测器饱和,对探测系统影响较大。
Abstract
The windows of IR detection systems becomes the main factor of the aero-thermo-radiation effect, which reduces the performance of these IR systems, or even makes these systems fail. By analyzing thermal radiation propagating in IR windows, a participating medium, an evaluation method for aero-thermo-radiation effect of the non-isothermal IR windows was proposed, based on the experimental results of the isothermal state, include self-radiation and transmittance. Aim to an MWIR detection system of a hypersonic vehicle, aero-thermo-radiation effect of a sapphire IR window was evaluated in 3.7-4.8 μm. The results indicate that, as the sapphire IR window is exposed in high-temperature and high-speed airflow, the aero-thermo-radiation effect of the window intensifies as temperature rises rapidly, the transmittance drops about 10%, still bigger than 0.9, otherwise the self-radiation enhances 458 times approximately, equal to that of blackbody about 125 ℃. For sapphire windows in 100-350 ℃, which thickness are smaller than 20 mm, as thickness increases, the transmittance decreases, self-radiation increases, and total radiation behind sapphire windows is increased, of which the ratio of self-radiation increases. So, self-radiation would drive detector into saturation easily, of which the influence on the MWIR detection system is bigger than that of transmittance.
王亚辉, 王强, 张伯川, 郑文娟, 刘彦, 徐力. 红外窗口气动热辐射效应评估方法[J]. 红外与激光工程, 2016, 45(2): 0204001. Wang Yahui, Wang Qiang, Zhang Bochuan, Zheng Wenjuan, Liu Yan, Xu Li. Evaluation method for aero-thermo-radiation effect of IR window[J]. Infrared and Laser Engineering, 2016, 45(2): 0204001.