浅析飞机隐身技术的发展趋势
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- 英文论文题名：Analysis on Development Trend of Aircraft Stealth Technology
- 论文作者：吕召燕 ; 胡海阳 ; 薛会民 ; 王美琦
- 英文论文作者：Lv Zhaoyan ; Hu Haiyang ; Xue Huimin ; Wang Meiqi ; AVIC Shenyang Aircraft Design and Research Institute
- 年：2016
- 作者机构：中航工业沈阳飞机设计研究所;
- 论文关键词：隐身技术 ; 结构形式 ; 衍生 ; 多学科
- 英文论文关键词：stealth technology ; structural type ; derive ; multidisciplinary subject
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（下册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：V218
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：4
- 文件大小：321k
- 原文格式：O
- 会议级别：全国
摘要
隐身技术水平是未来战斗机综合性能的重要指标。通过分析飞机隐身技术的现状,结合先进的吸波剂、结构形式和结构材料的发展,指出未来飞机隐身技术的发展不仅是先进隐身材料、结构材料的发展,也是新的结构形式以及这种新的结构形式所衍生出的隐身、结构等新的技术问题的发展。未来的飞机隐身设计应该是结构、材料、航电和隐身等多学科协同设计研究的产物。
Stealth technology level is an important index for the future fighter's comprehensive property.Based on the analysis of the present situation on the stealth technology,and the development of advanced absorbers,structural types and structural materials,the view that the development of the future fighter's stealth technology is not only about advanced stealth materials and structural materials,but also about new structural types and new technical problems about stealth and structure derive from the new structural types is proposed.The stealth design of the future fighter should be a product of collaborative design and research with multidisciplinary subject intersected by structure,material,avionics,stealth and so on.
Stealth technology level is an important index for the future fighter's comprehensive property.Based on the analysis of the present situation on the stealth technology,and the development of advanced absorbers,structural types and structural materials,the view that the development of the future fighter's stealth technology is not only about advanced stealth materials and structural materials,but also about new structural types and new technical problems about stealth and structure derive from the new structural types is proposed.The stealth design of the future fighter should be a product of collaborative design and research with multidisciplinary subject intersected by structure,material,avionics,stealth and so on.
引文
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[2]薛晓春.隐身与反隐身技术的发展研究[J].现代防御技术,2004,32(2),60-65.
[3]桑建华.飞行器隐身技术[M].北京:航空工业出版社.2015.1-32.
[4]姬金祖,武哲,刘战合.s弯形进气道隐身设计中弯度参数研究[J].西安电子科技大学学报,2009,36(4),746-750.
[5]石磊,郭荣伟.蛇形进气道的电磁散射特性[J].航空学报,2007,28(6),1296-1301.
[6]刘顺华,刘军民,董星龙,等.电磁波屏蔽及吸波材料[M].北京:化学工业出版社,2013,185-230.
[7]宋荟荟,周万城,罗发,等.超材料吸波体研究进展与展望[J].材料导报,2015,29(9),43-46.
[8]Landy N I,Sajuyigbe S,Mock J J,et al.Perfect Netamaterial Absorber[J].Physical Review Letters,2008:207402.
[9]杨欢欢,曹祥玉,高军,等.利用超材料吸波体减缩缝隙天线雷达散射截面[J].西安电子科技大学学报,2013,40(5),130-134.
[10]李文强,曹祥玉,高军,等.基于超材料吸波体的低散射截面波导缝隙阵列天线[J].物理学报,2015,64(9),094102.
[11]Geim A K,Novoselov K S.The Rise of Grapheme[J].Nature Materials,2007,6(3),183-191.
[12]Geim A K.Graphene:Status and Prospects[J].Science,2009,324(5934):1530-1534.
[13]Brumfiel G.Graphene Gels Ready for the Big Time[J].Nature,2009,458(7237):390-391.
[14]Novoselov K S,Geim A K,Morozov S V,et al.Electric Field Effect in Alomically Thin Carbon Films[J].Science,2004,306(5696):666-669.
[15]Balandin A A,Ghosh S,Bao W Z,el al.Superior Thermal Conductivity of Single-Layer Grapheme[J].Nano Letters,2008,8(3):902-907.
[16]Lee C,Wei X D,Kysar J W,et al.Measurement of the Elastic Properties and Intrinsic Strength of Monolayer Grapheme[J].Science,2008,321(5887):385-388.
[17]Novoselov K S,Geim A K,Morozov S V,et al.TwoDimensional Gas of Massless Dirac Fermions in Grapheme[J].Nature,2005,438(7065):197-200.
[18]Qin F,Brosseau C.A Review and Analysis of Microwave Absorption in Polymer Composites Filled with Carbonaceous Particles[J].Journal of Applied Physics,2012,111(6):061301.
[19]Basavaraja C,Kim W J,Kim Y D,et al.Synthesis of Polyaniline-Gold/grapheme Oxide Composite and Microwave Absorption Characteristics of the Composite Film[J].Materials Letters,2011,65(19):3120-3123.
[20]孙聪,张澎.先进战斗机对机载射频孔径系统隐身的需求及解决方案[J].航空学报,2008,29(6),1472-1481.
[21]Lars J,Patrik P.Conformal Array Antenna Theory and Design[M].Now Jersey:John wiley&Sons Inc,2006.
[22]何庆强,王秉中,何海丹.智能蒙皮天线的体系构架与关键技术[J].电讯技术,2014,54(8),1039-1045.
[23]Sinmazcelik T,Avcu E,Bora M O,et al.A Review;Fibre Metal Laminates.Background,Bonding Types and Applied Test Methods[J].Materials and Design,2011,32(7):3671-3685.
[24]Hayato N,Tatsuro K,Katsuhiko O.Damage Characterization of Titanium/GFRP Hybrid Laminates Subjected to Low-Velocity Impact[J].Composites Part A,2011,42(7):772-781.
[25]马玉娥,胡海威,熊晓枫.低速冲击下FMLs、铝板和复合材料的损伤对比[J].2014,35(7),1902-1911.
[26]Chai G B,Manikandan P.Low Velocity Impact Response of Fibre-Metal Laminates—A Review[J].Composite Structures,2014,107:363-381.