动态尾涡间隔缩短技术在民航中的应用
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  • 英文篇名:Application of dynamic wake vortex separation reduction technology in civil aviation
  • 作者:张天俊 ; 王洪 ; 陈世浩
  • 英文作者:ZHANG Tianjun;WANG Hong;CHEN Shihao;School of Electronic Engineering,University of Electronic Science and Technology of China;Rockwell Collins CETC Avionics Co.,LTD;
  • 关键词:尾涡 ; 尾涡间隔 ; 动态尾涡间隔缩短 ; 尾涡咨询系统
  • 英文关键词:wake vortex;;wake vortex spacing;;dynamic wake vortex separation reduction;;wake vortex advisory system
  • 中文刊名:XXYD
  • 英文刊名:Journal of Terahertz Science and Electronic Information Technology
  • 机构:电子科技大学电子工程学院;中电科柯林斯航空电子有限公司;
  • 出版日期:2018-12-28
  • 出版单位:太赫兹科学与电子信息学报
  • 年:2018
  • 期:v.16
  • 语种:中文;
  • 页:XXYD201806013
  • 页数:5
  • CN:06
  • ISSN:51-1746/TN
  • 分类号:76-80
摘要
尾涡是一种空气漩涡,是固定翼飞机机翼产生升力的副产品,它会影响其他飞机的飞行安全。特别是在飞机起飞降落阶段,飞机遭遇尾涡可能带来灾难性的后果。本文从尾涡的雷达探测、行为预测、尾涡安全系统应用三个方面,梳理了国内外研究尾涡雷达系统的现状。重点介绍了几种动态尾涡间隔缩短技术,展望了关于尾涡的拓展应用的前景与方向。
        Wake vortex is a kind of turbulence. When a wing of the fixed wing aircraft is generating lift, the wake vortex is formed from the wingtip. Wake vortex is hazardous to other aircrafts especially during the take-off phase. The detection, prediction and safety system application are studied. Some types of the dynamic wake vortex separation system are introduced as well.
引文
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