文章摘要
孙宁国,李良春.空投着陆缓冲气囊研究现状[J].包装工程,2017,38(11):97-101.
SUN Ning-guo,LI Liang-chun.Research Status of Landing Airbag for Airdrop[J].Packaging Engineering,2017,38(11):97-101.
空投着陆缓冲气囊研究现状
Research Status of Landing Airbag for Airdrop
投稿时间:2016-11-28  修订日期:2017-06-10
DOI:
中文关键词: 气囊  缓冲  空投  研究现状
英文关键词: airbag  cushion  airdrop  research status
基金项目:
作者单位
孙宁国 军械工程学院石家庄 050000 
李良春 军械技术研究所石家庄 050000 
摘要点击次数:
全文下载次数:
中文摘要:
      目的 总结当前着陆缓冲气囊的国内外研究现状。方法 介绍不同缓冲气囊的工作原理与优缺点,总结解析与有限元2种气囊性能的计算方法与性能参数优化方法的研究现状,以及气囊技术研究的发展方向。结果 分析了各类缓冲气囊与性能参数计算方法的优缺点,总结了气囊技术待解决的问题。结论 提高缓冲气囊的气压主动控制技术与着陆姿态控制技术可进一步提高气囊性能。
英文摘要:
      The work aims to summarize the current research status of the landing airbag. Firstly, the working principle, advantages and disadvantages of different cushioning airbags were introduced. Then, the calculation methods and performance parameter optimization methods of the two kinds of airbags in finite element analysis, as well as the development of airbag technology was summarized. As a result, the advantages and disadvantages of all kinds of cushion airbag and performance parameter calculation methods were analyzed, and the problems to be solved by airbag technology were summarized. In conclusion, improving pressure active control technology and landing attitude control technology can further improve airbag performance.
查看全文   查看/发表评论  下载PDF阅读器
关闭

关于我们 | 联系我们 | 投诉建议 | 隐私保护 | 用户协议

您是第21349643位访问者    渝ICP备15012534号-2

版权所有:《包装工程》编辑部 2014 All Rights Reserved

邮编:400039 电话:023-68795652 Email: designartj@126.com

    

渝公网安备 50010702501716号