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涡环旋转伞系统减速导旋效率研究
  • ISSN号:0258-1825
  • 期刊名称:《空气动力学学报》
  • 时间:0
  • 分类:V211.73[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术]
  • 作者机构:[1]南京理工大学机械工程学院,智能弹药技术国防重点学科实验室,江苏南京210094, [2]哈尔滨建成集团有限公司,黑龙江哈尔滨150030, [3]中国兵器工业第203研究所,陕西西安710065
  • 相关基金:国家自然科学基金(11372136);国家自然科学基金一青年科学项目(11102088);江苏省研究生培养创新计划项目(CXL1312-0210)
中文摘要:

为了解涡环旋转伞的减速导旋特性,提高旋转伞系统的减速导旋效率,以满足某些载物工作状态对转速、落速的苛刻需求,设计一种由涡环旋转伞和圆形减速伞构成的组合伞系统。制作单伞系统和组合伞系统的试验模型,分别进行伞塔试验。基于伞塔试验的高速摄影和图像处理技术,提取伞物系统的弹道数据点,结合弹道模型,用最小二乘法拟合时间弹道数据,得到单伞系统和组合伞系统的极限速度和阻力特征。基于姿态存储测量法,获得伞物系统的转速变化规律。对单伞系统和组合伞系统的弹道规律及减速导旋效率等数据进行对比分析,提出可有效提高旋转伞系统转速落速比的方法。结果表明:对高速录像进行图像处理可简单快速有效地提取伞物系统的极限速度和阻力特征;单具涡环旋转伞可提供更大扭矩,使载物旋转加速度更大,其导旋效率高;组合伞可提供更大阻力,使载物极限落速更低,其减速效率高;且合伞系统的转速落速比更大,整体性能优于单伞系统。

英文摘要:

To understand the decelerating and spinning characteristics of vortex ring parachute,increase the decelerating and spinning efficiency of rotating parachute system,and satisfy the harsh demand of limiting falling speed and rotating speed for some payloads at specific working state,a compound parachute system composed of a circle drag parachute and a vortex ring parachute was designed.The test models of single parachute system and compound parachute system were made out?and then two tower tests were carried out separately.Based on high speed photography of parachute tower test and image processing technology,the trajectory data points of the parachute-payload system were extracted.Combining with the trajectory model,the time and trajectory data was fitted by least square method,the limiting falling speed and the resistance characteristics of the system were obtained.Using attitude memory-measuring technology,the rotating speed changing law of parachute-payload system was gained.The trajectory laws and the decelerating and spinning efficiency of the vortex ring parachute and thecompound parachute system were analyzed contrastively,and then the method to increase theratio of rotating speed and limiting falling speed availably was proposed.The results show that through processing the pictures shot by high-speed camera,the limiting falling characteristics of the parachute-payload system can be extracted quickly and efficiently.The single vortex ring parachute could provide bigger torque so that the rotating accelerating of the payload is higher,which means that the spinning efficiency is better.The compound parachute could bigger resistance so that the limiting falling speed of the payload is lower,which means that the decelerating efficiency is better.The radio of rotating speed and falling speed of compound parachute system is bigger than that of single parachute system,which means that the whole performance of compound parachute system is better.

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期刊信息
  • 《空气动力学学报》
  • 中国科技核心期刊
  • 主管单位:中国空气动力研究与发展中心
  • 主办单位:中国空气动力学会
  • 主编:邓小刚
  • 地址:四川省绵阳市二环路南段6号13-11信箱
  • 邮编:621000
  • 邮箱:kqdlxxb@aas.cardc.com
  • 电话:0816-2463287
  • 国际标准刊号:ISSN:0258-1825
  • 国内统一刊号:ISSN:51-1192/TK
  • 邮发代号:62-27
  • 获奖情况:
  • 1997年获中国科协评比的“全国优秀科技期刊二等奖”,1997年获中宣部、国家新闻出版局、国家科委“第二...
  • 国内外数据库收录:
  • 荷兰文摘与引文数据库,日本日本科学技术振兴机构数据库,中国中国科技核心期刊,中国北大核心期刊(2004版),中国北大核心期刊(2008版),中国北大核心期刊(2011版),中国北大核心期刊(2014版),中国北大核心期刊(2000版)
  • 被引量:6089