星载红外探测器组件寿命试验研究及系统设计

洪津; 王征云; 胡亚东; 张元贞; 孙晓兵

doi:10.3788/OPE.20182605.1148

您当前的位置：

首页 >

文章列表页 >

星载红外探测器组件寿命试验研究及系统设计

微纳技术与精密机械 | 更新时间：2020-08-13

- 星载红外探测器组件寿命试验研究及系统设计
- Research of life test and design of system for satellite-borne infrared detector assembly
- 光学精密工程 2018年26卷第5期页码：1148-1155
- 作者机构：
  
  1.中国科学院安徽光学精密机械研究所, 安徽合肥 230031
  2.中国科学技术大学, 安徽合肥 230026
- 作者简介：
  
  [ "洪津(1969-), 男, 浙江杭州人, 研究员, 博士生导师, 1987年于浙江大学获得学士学位, 2008年于中科院安徽光机所评为研究员, 主要研究光谱偏振遥感技术和航天遥感工程技术等。E-mail:hongjin@aiofm.ac.cn" ]
  [ "王征云(1991-), 男, 江苏淮安人, 硕士研究生, 2015年于合肥工业大学获得学士学位, 主要研究方向为光电获取技术。E-mail:fisher_wzymail@163.com" ]
- 基金信息：
  
  国家国防科工局高分专项（民用部分）资助项目(32-Y20A22-9001-15/17);中国科学院重点资助项目(KGFZD-125-13-006)
- DOI：10.3788/OPE.20182605.1148
  中图分类号： TP273
- 收稿日期：2017-10-11，
  
  录用日期：2017-11-6，
  
  纸质出版日期：2018-05-25
- 稿件说明：
移动端阅览
洪津, 王征云, 胡亚东, 等. 星载红外探测器组件寿命试验研究及系统设计[J]. 光学精密工程, 2018,26(5):1148-1155.

Jin HONG, Zheng-yun WANG, Ya-dong HU, et al. Research of life test and design of system for satellite-borne infrared detector assembly[J]. Optics and precision engineering, 2018, 26(5): 1148-1155.
洪津, 王征云, 胡亚东, 等. 星载红外探测器组件寿命试验研究及系统设计[J]. 光学精密工程, 2018,26(5):1148-1155. DOI： 10.3788/OPE.20182605.1148.

Jin HONG, Zheng-yun WANG, Ya-dong HU, et al. Research of life test and design of system for satellite-borne infrared detector assembly[J]. Optics and precision engineering, 2018, 26(5): 1148-1155. DOI： 10.3788/OPE.20182605.1148.

摘要

探测器是航天有效载荷中完成光电转换的核心部件，且一旦发射升空，几乎不可能对其进行维护、修理和更换。采用经过筛选的无寿命数据的商业红外探测器存在风险，热电制冷器（TEC）的使用寿命是探测器组件寿命的薄弱环节，其可靠性对探测器的正常使用具有重要影响。因此，对红外探测器组件的寿命试验研究至关重要。首先分析了某航天载荷红外探测器的工作模式及TEC的失效机理，制定了恒定应力结合定数截尾的加速寿命试验方案降低时间成本；然后，从硬件和软件的两个部分详细地阐述了红外探测器寿命试验系统的搭建，并展示了设备实物图和红外探测器温度循环效果图；最后，运行寿命试验系统，试验时间累积约170 d，红外探测器温度循环累积约30 000次。试验结果指出：两种型号星载红外探测器经过寿命试验后G12180相对光谱响应率最大变化1.45%，G12183相对光谱响应率最大变化4.44%，G12180组件热电制冷器制冷驱动电流最大增加了4.30%，G12183组件热电制冷器制冷驱动电流最大增加了7.50%，探测器组件的使用寿命和性能变化满足航天载荷需求。

Abstract

The detector is the core component of the photoelectric conversion in the satellite-borne

and once launched

it is almost impossible for the maintenance

repair and replacement. Using The screened commercial infrared detector without life data has the risk. The service life of the thermoelectric cooler(TEC) is the weak link of the life of detector assembly

and its reliability has an important influence on the normal use of the detector. Therefore

it is important to study the life test of the infrared detector assembly. Firstly

the working mode of the satellite-borne infrared detector and the failure mechanism of TEC were analyzed. The accelerated life test method with constant stress combined with fixed number truncation was developed to reduce the time cost.Secondly

the hardware and software of the infrared detector life test system was described in detail

demonstrated the equipment and temperature cycle of the infrared detector; Finally

the life test system was operated

the test time accumulated for about 170 days

and the temperature cycle of the infrared detector accumulated about 30 000 times. The test result indicated that the maximum changes of the relative photosensitivity of G12180 and G12183 were 1.45% and 4.44%

respectively. The maximus increments of the cooling current of G12180 and G12183 component TEC were 4.30% and 7.50%

respectively. It can be seen that the life and performance changes of the detector assembly meet the aerospace load requirements.

关键词

Keywords

references

张卫峰, 张若岚, 赵鲁生, 等. InGaAs短波红外探测器研究进展[J].红外技术, 2012, 34(6):361-365.

ZHANG W F, ZHANG R L, ZHAO L SH, et al .. Development progress of InGaAs short-wave infrared focal plane arrays[J]. Infrared Technology , 2012, 34(6):361-365. (in Chinese)

PERALTAR J, NARDELL C, CAIRNS B, et al . . Aerosol polarimetry sensor for the glory mission[C]. Proceedings Volume 6786, MIPPR 2007: Automatic Target Recognition and Image Analysis; and Multispectral Image Acquisition, SPIE, 2007: 67865L.

汪方斌, 洪津, 孙晓兵, 等.航空多角度偏振辐射计信噪比估算与测量[J].光学精密工程, 2015, 23(2):387-394.

WANG F B, HONG J, SUN X B, et al .. Estimation and measurement of signal-to-noise ratio for aviation multi-angular polarimetric radiometer[J]. Opt. Precision Eng ., 2015, 23(2):387-394. (in Chinese)

胡亚东, 胡巧云, 孙斌, 等.暗电流对短波红外偏振测量精度的影响[J].红外与激光工程, 2015, 44(8):2375-2381.

HU Y D, HU Q Y, SUN B, et al .. Impact of dark current on SWIR polarimetry accuracy[J]. Infrared and Laser Engineering , 2015, 44(8):2375-2381. (in Chinese)

ONATB M, HUANG W, MASAUN N, et al . . Ultra-low dark current InGaAs technology for focal plane arrays for low-light level visible-shortwave infrared imaging[C]. Proceedings Volume 6542, Infrared Technology and Applications XXXⅢ, SPIE, 2007, 6542: 65420L.

黄岳巍, 崔瑞祯, 巩马理, 等.基于TEC的大功率LD恒温控制系统的研究[J].红外与激光工程, 2006, 35(2):143-147.

HUANG Y W, CUI R ZH, GONG M L, et al .. TEC based thermostat system for high-power semiconductor laser[J]. Infrared and Laser Engineering , 2006, 35(2):143-147. (in Chinese)

SHAN J D, WU G, TIAN X J. Study on large time-delay constant temperature control system based on TEC[J]. The Journal of China Universities of Posts and Telecommunications , 2010, 17(S2):32-35.

ZANG H Q, LI Q. The automatic temperature system with fuzzy self-adaptive PID control in semiconductor laser[C]. Proceedings of the IEEE International Conference on Automation and Logistics , IEEE, 2009: 1691-1694.

田小建, 尚祖国, 高博, 等. 980 nm高稳定度激光泵浦源控制系统[J].光学精密工程, 2015, 23(4):982-987.

TIAN X J, SHANG Z G, GAO B, et al .. Control system for 980 nm high stability laser pump source[J]. Opt. Precision Eng ., 2015, 23(4):983-987. (in Chinese)

张泉, 黄书华, 赵欣, 等.机载成像光谱仪CCD制冷系统设计与实现[J].光子学报, 2017, 46(3):0311004.

ZHANG Q, HUANG SH H, ZHAO X, et al .. The design and implementation of CCD refrigeration system of imaging spectrometer[J]. Acta Photonica Sinica , 2017, 46(3):0311004. (in Chinese)

任仁, 吴礼刚, 王小坤, 等.碲镉汞红外探测器高低温循环特性研究[J].激光与红外, 2007, 37(S):941-943.

REN R, WU L G, WANG X K, et al .. Study on the thermal cycle characteristic of HgCdTe detector[J]. Laser & Infrared , 2007, 37(S):941-943. (in Chinese)

朱宪亮, 张海燕, 龚海梅.航天InGaAs短波红外探测器步进应力加速寿命试验研究[J].半导体光电, 2014, 35(6):1008-1012.

ZHU X L, ZHANG H Y, Gong Hai-mei. Study on step-stress accelerated life test for space InGaAs shortwave infrared device[J]. Semiconductor Optoelectronics , 2014, 35(6):1008-1012. (in Chinese)

李久祥.整机加速贮存寿命试验研究[J].质量与可靠性, 2004, (4):14-17.

LI J X. Study on accelerated storage life test of complete machine[J]. Quality and Reliability , 2004, (4):14-17. (in Chinese)

朱宪亮. 红外探测器组件可靠性试验研究[D]. 上海: 中国科学院上海技术物理研究所, 2014.

ZHU X L. Study on reliability test of infrared detector assembly [D]. Shanghai: Shanghai Institute of Technical Physics of the Chinese Academy of Sciences, 2014. (in Chinese)

MURRAYS F, HESHMAT H. Accelerated testing of space mechanisms[R]. NASA CR-198437. Latham, NY: NASA.

YANG SH H, LIU X G, WU Y N. The lifetime prediction model of stirling cryocooler for infrared detector assembly[C]. Proceedings Volume 8907, International Symposium on Photoelectronic Detection and Imaging 2013: Infrared Imaging and Applications , SPIE, 2013: 89075L.

张勇波, 傅惠民, 王治华.恒定应力无失效加速寿命试验可靠性分析方法[J].航空动力学报, 2013, 28(3):520-524.

ZHANG Y B, FU H M, WANG ZH H. Method for reliability analysis on constant-stress zero-failure accelerated life test[J]. Journal of Aerospace Power , 2013, 28(3):520-524. (in Chinese)

LIN K S, CHEN Y X, XU D. Reliability assessment model considering heterogeneous population in a multiple stresses accelerated test[J] . Reliability Engineering & System Safety , 2017, 165:134-143.

浏览量

491

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

TEA CO₂长波红外激光对红外凝视成像系统探测器组件的损伤效应

红外探测器星上大范围高分辨率测温系统

特气室温红外探测器的噪声分析

碳纳米管压阻微悬臂梁红外热探测器的研究

关于红外探测器与红外焦平面阵列探测器性能参数描述方法的商榷