期刊文献+

Permittivity of composites used for Luneburg lens antennas by drilling holes based on 3-D printing technique

Permittivity of composites used for Luneburg lens antennas by drilling holes based on 3-D printing technique
下载PDF
导出
摘要 Due to the attractive performances such as the ability of beam focus,broadband,multi-beam scanning and other features,Luneburg lens antennas are applied in multi-beam antenna,which overcomes the problem of gain loss produced by multi-beam parabolic antenna.Based on 3-D printing technique,Luneburg lens antennas by drilling holes are studied.Permittivity and loss tangent of the equivalent lens materials can be influenced by original materials,hole shapes,hole directions,and porosity.After tests,polystyrene with waxes may be the most appropriate materials for Luneburg lens with high strength.Permittivity with the shape of triangle is the lowest due to the homogeneity.Relative permittivities with the direction at a range of 15°-45°are lower while loss tangent at a range of 0°-30°.Radial directional holes are more appropriate for Luneburg lens.The relative permittivity is decreased with the increment of porosity.After calculations,the forecasts calculated by Looyenga and A-BG theory are more precise.Finally,Luneburg lens with two layers is fabricated by 3-D printing. Due to the attractive performances such as the ability of beam focus, broadband, multi-beam scanning and other features, Luneburg lens antennas are applied in multi-beam antenna, which overcomes the problem of gain loss produced by multi-beam parabolic antenna. Based on 3-D printing technique, Luneburg lens antennas by drilling holes are studied. Permittivity and loss tangent of the equivalent lens materials can be influenced by original materials, hole shapes, hole directions, and porosity. After tests, polystyrene with waxes may be the most appropriate materials for Luneburg lens with high strength. Permittivity with the shape of triangle is the lowest due to the homogeneity. Relative permittivities with the direction at a range of 15°-45° are lower while loss tangent at a range of 0°-30°. Radial directional holes are more appropriate for Luneburg lens. The relative permittivity is decreased with the increment of porosity. After calculations, the forecasts calculated by Looyenga and A-BG theory are more precise. Finally, Luneburg lens with two layers is fabricated by 3-D printing.
出处 《太赫兹科学与电子信息学报》 2017年第4期646-651,共6页 Journal of Terahertz Science and Electronic Information Technology
基金 supported by the Science and Technology Programme of Shijiazhuang under Grant 151130081A
关键词 Luneburg lens by DRILLING HOLES 3-D PRINTING TECHNIQUE PERMITTIVITY Luneburg lens by drilling holes 3-D printing technique permittivity
  • 相关文献

参考文献1

二级参考文献27

  • 1Kirby P L,Pukala D,Manohara H. Characterization of micromachined silicon rectangular waveguide at 400 GHz[J].{H}IEEE MICROWAVE AND WIRELESS COMPONENTS LETTERS,2006,(06):366-368.
  • 2Fitch M,Osiander R. Terahertz waves for communications and sensing[J].John Hopkins APL Technical Digest,2004,(04):348-355.
  • 3Liu X,Kizer S,Barnet C. Retrieving atmospheric temperature and moisture profiles from NPP CRIS ATMS sensors using CriMSS EDR algorithm[A].Munich:[s.n.],2012.
  • 4Grankov A G,Mil'shin A A,Shelobanova N K. Comparison of data measured in the North Atlantic region by the MTVZA radiometer of a meteor-3M satellite and by the SSM/I radiometer of the F-13(DMSP series)satellite[J].{H}JOURNAL OF COMMUNICATIONS TECHNOLOGY AND ELECTRONICS,2006,(02):158-163.
  • 5Zabolotny V F,Yakopov G V,Mingaliev M G. High sensitive 0.13-0.38 THz TES array radiometer for the big telescope azimuthal of Special Astrophysical Observatory of Russian Academy of Sciences[A].IRMMW-THz.Cardiff:[s.n.],2007.117-118.
  • 6Edward K,Cheng-H Joseph L,Vince L R. The Advanced Technology Microwave Sounder(ATMS):A New Operational Sensor Series[A].Munich:[s.n.],2012.
  • 7Gorobets N N,Chernyavsky G M,Cherny I V. Advanced antenna of microwave imager/sounder for spacecraft “METERO-M”[A].Barcelona:[s.n.],2010.
  • 8Mahaffy P,Webster C R,Conrad P G. The sample analysis at Mars investigation and instrument suite[R].Goddard Space Flight Center,Jet Propulsion Laboratory.GSFC.JA.5567.2011,GSFC.JA.6685,SPRINGER:[s.n.],2012.
  • 9Gulkis S,Frerking M,Crovisier J. MIRO:Microwave Instrument for Rosetta Orbiter[J].{H}Space Science Reviews,2007,(1-4):561-597.
  • 10刘豪,梁巍.美国国防高级研究计划局F6项目发展研究[J].航天器工程,2010,19(2):92-98. 被引量:29

共引文献23

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