激光驱动飞片飞行特征研究进展
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摘要
激光驱动飞片是高效的冲击加载方法,作为激光起爆炸药的一种方式,具有本质安全性。激光驱动飞片起爆炸药的可靠度与飞片的飞行特性密切相关,飞片的飞行速度和表观形貌(平面度和完整性)是成功起爆的两个重要参数。因此,从飞片的飞行特性的表征手段与影响因素两方面出发,综述了激光驱动飞片技术的研究进展。针对单层飞片,介绍了观测、表征和接收方法,分析讨论了飞片性能影响因素作用规律的近年研究成果,梳理归纳了现有研究中存在的不足,指出了今后的发展方向,包括激光驱动飞片飞行过程的系统物理模型和激光驱动飞片的平面度和完整性定量参数。
Laser?driven flyer is an efficient shock loading method,which has essential safety as a method of initiating explosives by laser. The reliability of initiating explosives by laser?driven flyer is closely related to the flight characteristics of flyer. The flying velocity and apparent morphology(planarity and integrity) of flyer are two important parameters for a successful initiation.Therefore,in this paper,the research progresses of laser?driven flyer technique were reviewed from two aspects of characterization means and influencing factors of flight properties of flyer. Focusing on laser?driven single layer foils,the methods of observation,characterization and reception were introduced. The research findings for the function law of influencing factors of flight performance in recent years were analyzed and discussed. The deficiencies existing in current researches were hackled and summarized and the future development directions,including the systematic physical model of flight process of laser?driven flyer and quantitative parameters of planarity and integrity of laser?driven flyer,were pointed out.
Laser?driven flyer is an efficient shock loading method,which has essential safety as a method of initiating explosives by laser. The reliability of initiating explosives by laser?driven flyer is closely related to the flight characteristics of flyer. The flying velocity and apparent morphology(planarity and integrity) of flyer are two important parameters for a successful initiation.Therefore,in this paper,the research progresses of laser?driven flyer technique were reviewed from two aspects of characterization means and influencing factors of flight properties of flyer. Focusing on laser?driven single layer foils,the methods of observation,characterization and reception were introduced. The research findings for the function law of influencing factors of flight performance in recent years were analyzed and discussed. The deficiencies existing in current researches were hackled and summarized and the future development directions,including the systematic physical model of flight process of laser?driven flyer and quantitative parameters of planarity and integrity of laser?driven flyer,were pointed out.
引文
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[7]Walker F E,Wasley R J.Critical energy for shock initiation of heterogeneous explosives[J].Explosive Stoffe,1969,17(1):9-13.
[8]濮赞泉.破片撞击起爆战斗部影响因素及判据研究[D].南京:南京理工大学,2016.PU Zan-quan.Influence factors and criteria of warhead shock initiation by fragments[D].Nanjing:Nanjing University of Science and Technology,2016.
[9]吴立志,沈瑞琪,徐娇,等.激光驱动飞片技术的研究进展[J].兵工学报,2010(31):219-228.WU Li-zhi,SHEN Rui-qi,XU Jiao,et al.Research advance in laser-driven flyer technology[J].Acta Armamentaria,2010(31):219-228.
[10]税敏,储根柏,席涛,等.神光Ⅲ原型装置激光驱动高速飞片实验研究进展[J].物理学报,2017,66(6):064703(1-9).SHUI Min,CHU Gen-bai,XI Tao,et al.Experimental progress of laser-driven flyers at the SG-Ⅲprototype laser facility[J].Acta Phys Sin,2017,66(6):064703(1-9).
[11]Watson S,Field J E.Integrity of thin,laser-driven flyer plates[J].Journal of Applied Physics,2000,88(7):3859-3864.
[12]Bowden M D,Drake R C.The initiation of high surface area Pentaerythritol Tetranitrate using fiber-coupled laser-driven flyer plates[C]//Optical Technologies for Arming,Safing,Fuzing,and Firing III,San Diego,CA,2007,6662:66620D(1-12).
[13]Mattel T,Shaw-Stewart J,Schneider C W,et al.Laser induced forward transfer aluminum layers:Process investigation by time resolved imaging[J].Applied Surface Science,2012,258:9352-9354.
[14]Liu C Y,Mao X L,Greif R,et al.Time Resolved Shadowgraph Images of Silicon during Laser Ablation Shockwaves and Particle Generation[C]//8th International Conference on Laser Ablation,2007,59:338-342.
[15]刘寿先,温伟峰,袁树云,等.分幅面成像任意反射面速度干涉仪诊断激光驱动飞片全场速度[J].光学学报,2013,33(9):0912007(1-7).LIU Shou-xian WEN Wei-feng,YUAN Shu-yun,et al.Full field velocity measurement of laser-driven fllyer using framing-imaging velocity interferometer system for any reflector[J].Acta Optica Sinica,2013,33(9):0912007(1-7).
[16]Celliers P M,Erskine D J,Sorce C M,et al.A high-resolution two-dimensional imaging velocimeter[J].Review of Scientific Instrument,2010,81(3):035101.
[17]Banishev A A,Shaw W L,Bassett W P,et al.High-speed laser-launched flyer impacts studied with ultrafast photography and velocimetry[J].Journal of Dynamic Behavior Materials,2016(2):194-206.
[18]Yeager J D,Bowden P R,Guildenbecher D R,et al.Characterization of hypervelocity metal fragments for explosive initiation[J].Journal of Applied Physics,2017,122:035901(1-9).
[19]Willey T M,Champley K,Hodgin R,et al.X-ray imaging and3D reconstruction of in-flight exploding foil initiator flyers[J].Journal of Applied Physics,2016,119:235901(1-4).
[20]Curtis A D,Banishev A A,Shaw W L,et al.Laser-driven flyer plates for shock compression science:Launch and target impact probed by photon Doppler velocimetry[J].Review of Scientific Instrument.2014,85(4):043908(1-12).
[21]Rességuier T D,Signor L,Dragon A,et al.Experimental investigation of liquid spall in laser shock-loaded tin[J].Journal of Applied Physics,2007,101(1):013506(1-7).
[22]郭俊峰,曾庆轩,李明愉,等.飞片材料对微装药驱动飞片形貌的影响[J].高压物理学报,2017,31(3):315-320.GUO Jun-feng,ZENG Qing-xuan,LI Ming-yu,et al.Influnce of flyer material on morphology of flyer driven by micro charge[J].Chinese Journal of High Pressure Physics,2017,31(3):315-320.
[23]Signor L,Rességuier T D,Dragon A,et al.Investigation of fragments size resulting from dynamic fragmentation in melted state of laser shock-loaded tin[J].International Journal of Impact Engineering,2010,37(8):887-900.
[24]Lescoute E,Rességuier T D,Chevalier J M,et al.Soft recovery technique to investigate dynamic fragmentation of laser shock-loaded metals[J].Applied Physics Letters,2009,95(21):211905(1-3).
[25]Cottet F,Romain J P.Formation and decay of laser-generated shock waves[J].Physics Review A,1982,25(1):576-579.
[26]Watson S,Field J E.Measurement of the ablated thickness of films in the launch of laser-driven flyer plates[J].Journal of Physics D:Applied Physics,2000,33(2):170-174.
[27]Stein C,Roybal R,Tlomak P,et al.A review of hypervelocity debris testing at the Air Force Research Laboratory[J].Space Debris,2004,2(4):331-356.
[28]Jr Farnsworth A V,Trott W M,Setchell R E.A computational study of laser driven flyer plates[C]//AIP Conference Proceedings,2001,CP620:1355-1358.
[29]牛锦超,龚自正,曹燕,等.8 km/s激光驱动飞片发射技术实验研究[J].爆炸与冲击,2014,34(2):129-136.NIU Jin-chao,GONG Zi-zheng,CAO Yan,et al.Experimental research on laser-driven flyer plates up to 8 km/s[J].Explosion and Shock Waves,2014,34(2):129-136.
[30]高瑀含.高斯光束整形技术研究[D].长春:长春理工大学,2012.GAO Yu-han.Research of Gaussian beam shaping[D].Changchun:Changchun University of Science and Technology,2012.
[31]Brown K E,Shaw W L,Zheng X,et al.Simplified laser-driven flyer plates for shock compression science[J].Review of Scientific Instruments,2012,83:103901(1-12).
[32]Fujiwara H,Brown K E,and Dlott D D.High-energy flat-top beams for laser launching[J].Applied Opitcs,2010,49(19):3723-3731.
[33]董洪建,童靖宇,黄本诚.真空环境下空间碎片超高速撞击试验研究[J].真空科学与技术学报,2004,24(2):109-112.DONG Hong-jian,TONG Jing-yu,HUANG Ben-cheng.Impact simulation of hypervelocity space debris in vacuum environment[J].Vacuum Science and Technology(China),2004,24(2):109-112.
[34]Gurney R W.The initial velocites of fragments from bombs,shell,grenades[R].Ballistic Research Laboratory Report No.405,1943.
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