期刊文献+

大面阵红外探测器与低温冷平台集成后的应变测试研究 被引量:4

Test Study of Strain after Integration of Large Scale Infrared Detector Chip into Cryogenic Cold Platformat at Low Temperature
下载PDF
导出
摘要 大面阵红外探测器是红外遥感仪器的核心元件。该类探测器大多由小规模面阵探测器拼接组成,与杜瓦低温冷平台集成后形成杜瓦组件。探测器在杜瓦低温冷平台上安装集成后的应力状态是影响芯片性能和寿命的关键因素。测试了低温时探测器在自由状态下和被安装在杜瓦组件内应变片的热输出,再利用两者的差值表征了探测器与杜瓦低温冷平台集成后的额外应变。以2000×512探测器组件为例,进行了测试验证分析,结果表明该方法可行。 Large area array infrared detectors are the core components in infrared remote sensing in-struments. Most of them are composed of spliced small-scale area array detectors and are integrated onDewar cold platforms to form Dewar assemblies. The stress state of a detector after being integrated onthe Dewar cold platform is a key factor affecting the performance and lifetime of the chip. The thermaloutput of a strain gage when the detector is both in the free state and in the Dewar is tested at low tem-perature. The difference between the two values is used to characterize the extra strain after the detectoris integrated with the Dewar cold platform. Taking a 2000x512 detector assembly as an example, thetest verification and analysis are carried out. The result shows that this method is feasible.
出处 《红外》 CAS 2017年第8期23-26,共4页 Infrared
关键词 探测器 应变 应变片 detector strain strain gage
  • 相关文献

参考文献2

二级参考文献41

  • 1张苹苹.航空产品加速寿命试验研究及应用[J].北京航空航天大学学报,1995,21(4):124-129. 被引量:21
  • 2汤英文,朱龙源,游达,许金通,刘诗嘉,庄春泉,李向阳,龚海梅.表面二次阳极氧化对HgCdTe光导器件性能的影响[J].半导体光电,2007,28(1):72-75. 被引量:2
  • 3Glaister D S, Donabedian M, Curran D G T, et al. An Overview of the Performance and Maturity of Long Life Cryocoolers for Space Applications [C]. Cryocoolers, 1999, 10: 1-31.
  • 4Radebaugh R. Development of Pulse Tube Refrig- erators as an Efficient and Reliable Cryocooler [C]. Proceedings of Institute of Refrigeration, 2000: 11- 29.
  • 5Radebaugh R. Pulse Tube Cryocoolers for Cooling Infrared Sensorsv [C]. SPIE, 2000, 4130: 363-379.
  • 6Tward E, Chan C K, Jaco C, et al. Miniature Space Pulse Tube Cryocoolers [J]. Cryogenics, 1999, 39(8): 717-720.
  • 7Raab J, Tward E. Northrop Grumman Aerospace Systems Cryocooler Overview [J]. Cryogenics, 2010, 50(9): 572-581.
  • 8Wang G P, Cai J H, Li N, et al. Development of a 0.5W/50K Pulse Tube Cryocooler for an Infrared Detector [C]. Cryocoolers, 2007, 14: 83-88.
  • 9Trollier T, Tanchon J, Buquet J, et al. Design of a Large Heat Lift 40 to 80 K Pulse Tube Cryocooler for Space Applications [C]. Cryocoolers, 2007, 14: 75-82.
  • 10Wilson K B, Fralick C C, Gedeon D R, et al. Sun- power's CPT60 Pulse Tube Cryocooler [C]. Cry- ocoolers, 2007, 14: 123-132.

共引文献34

同被引文献22

引证文献4

二级引证文献13

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部