真空 ›› 2020, Vol. 57 ›› Issue (5): 38-44.doi: 10.13385/j.cnki.vacuum.2020.05.09
王琎, 王春勇, 付朝晖
WANG Jin, WANG Chun-yong, FU Zhao-hui
摘要： 在探月工程的基础上继续开展深空探测是未来的发展趋势,后续的深空探测活动必然会有地外天体的采样与返回,其中样品密封技术为保证深空探测样品的原样返回提供了技术保障。本文针对我国深空探测样品钎焊密封的使用需求,调研了国外深空探测采样返回任务中钎焊密封技术的发展现状,主要介绍了双层钎焊密封容器和单层钎焊密封容器两种具体的密封容器形式,同时简要介绍了目前国内钎焊密封的技术现状。最后结合我国小行星、火星等任务的应用需要,提出了适合我国深空探测样品钎焊密封的工作建议。
中图分类号:
| [1] 欧阳自远. 我国月球探测的总体科学目标与发展战略[J]. 地球科学进展, 2004, 19(3): 351-358. [2] 李丹明, 吴启鹏, 王琎, 等. 月球样品地面转移过程中防污染措施研究[J]. 真空与低温, 2015, 21(5): 287-290. [3] 付朝晖, 许旻, 杜永刚. 极高真空环境下软金属刀口密封研究[J]. 真空科学与技术学报, 2014, 34(3): 13-18. [4] Thackara J I. Method for making a hermetically sealed package comprising at least one optical fiber feedthrough: U. S. Patent 6, 216, 939[P].2001-4-17. [5] FEBKELL D. ASSKJNOBS: U. S. Patent 1, 834, 581[P].1931-12-1. [6] 俞敏. 月球样品密封结构的泄露分析与地面试验[D]. 杭州: 浙江大学, 2014. [7] 俞勇祥. 感应加热技术的应用与发展[J]. 今日科技, 1999, 9: 002. [8] 许艺峰, 张德禹, 徐学军, 等. 液体火箭发动机推力室钎焊过程热固耦合分析[J]. 焊接学报, 2011, 32(10): 93-96. [9] 韩玉昆, 梁智. 毛细管板结构电子束钎焊温度场研究[J]. 航空制造技术, 2005, (5): 81-85. [10] 李琢. 飞机安装式导管高频感应钎焊技术研究及应用[D]. 哈尔滨: 哈尔滨工业大学, 2014. [11] Yoseph B C, Mircea B, Bao X Q, et al.Synchronous Separation, Seaming, Sealing and Sterilization(S4)using Brazing for Sample Containerization and Planetary Protection[C]. Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2017, 2017, 10168: 1-7. [12] Bao X Q, Mircea B, Stewart S, et al.Heating and thermal control of brazing technique to break contamination path for potential Mars sample return[C]. Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace Systems 2017. [13] Bao X Q, Mircea B, Yoseph B C.Thermal analysis of brazing seal and sterilizing technique to break contamination chain for Mars sample return[C]. San Diego, Sensors and Smart Structures Technologies for Civil, Mechanical, and Aerospace 2015, 9435: 1-6. [14] Rummel J D, Conley C.Preparing for the human exploration of Mars: health care and planetary protection requirements and practices[C]. International Astronautical Congress, 2012. [15] Gershman R, Adams M, Dillman R, et al.Planetary Protection Technology for Mars Sample Return[C]//IEEE Aerospace Conference, 2005, 34(11): 2328-2337. [16] Anonymous. Separation and Sealing of a Sample Container Using Brazing[J]. NASA Tech Briefs, 2007, 31(8): 42-44. [17] Yoseph B C, Wu J, AyoolaK O. Simultaneous Separation, Seaming and Sealing using Brazing(S3B)for Sample Containerization and Planetary Protection[C]. Smart Structures and Materials 2005, 67(6), 717-723. [18] Mattingly R, May L.Mars Sample Return as a Campaign[C], IEEE Aerospace Conference, 2011, 1805: 1-13. [19] Backes P, Lindemann R, Collins C, et al.An Integrated Coring and Caching Concept[C], IEEE Aerospace Conference, 2010, 1675: 1-7. [20] Backes P, Aldrich J, Zarzhitsky D, et al.Demonstration of Autonomous Coring and Caching for a Mars Sample Return Campaign Concept[C], IEEE Aerospace Conference, 2012, 1-11. [21] Collins C, Younse P, Backes P.Planetary Sample Caching System Design Options[C]. AIAA SPACE 2009 Conference & Exposition, 2009, 6506. [22] Backes P, Younse P, Cicco M P, et al.Experimental Results of Rover-Based Coring and Caching[C]. Aerospace IEEE Conference, 2011, 1808: 1-14. [23] Backes P, Onstott T, Yoseph B C.Planetary Sample Sealing for Caching[C]. Aerospace conference, 2009, 1676: 1-10. [24] Younse P, Alwis T, Backes P, et al.Sample Sealing Approaches for Mars Sample Return Caching[C]. 2012. [25] Backes P, Younse P, Ganino A.A Minimum Scale Architecture for Rover-Based Sample Acquisition and Caching[C]//, 2013: 1-10. 10. 1109 /AERO. 2013. 6497399. [26] Allton J H, Dardano C B.How Successful were the lunar sampling tools: Implications for sampling Mars[R]. Houston, TX.77358, In Lunar and Planetary Inst. , Workshop on Mars. |
| [1] | 纪 明, 孙 亮, 杨敏勃. 一种用于对月球样品自动密封锁紧的设计[J]. 真空, 2018, 55(6): 24-27. |
|