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6R两自由度空间扑翼机构设计与分析

曹金秋 金晓宏 朱建阳

曹金秋, 金晓宏, 朱建阳. 6R两自由度空间扑翼机构设计与分析[J]. 机械科学与技术, 2018, 37(2): 206-210. doi: 10.13433/j.cnki.1003-8728.2018.0207
引用本文: 曹金秋, 金晓宏, 朱建阳. 6R两自由度空间扑翼机构设计与分析[J]. 机械科学与技术, 2018, 37(2): 206-210. doi: 10.13433/j.cnki.1003-8728.2018.0207
Cao Jinqiu, Jin Xiaohong, Zhu Jianyang. Design and Analysis of 6R Spatial Flapping-wing Mechanism with Two Degrees of Freedom[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(2): 206-210. doi: 10.13433/j.cnki.1003-8728.2018.0207
Citation: Cao Jinqiu, Jin Xiaohong, Zhu Jianyang. Design and Analysis of 6R Spatial Flapping-wing Mechanism with Two Degrees of Freedom[J]. Mechanical Science and Technology for Aerospace Engineering, 2018, 37(2): 206-210. doi: 10.13433/j.cnki.1003-8728.2018.0207

6R两自由度空间扑翼机构设计与分析

doi: 10.13433/j.cnki.1003-8728.2018.0207
基金项目: 

国家自然科学基金项目(51505347)资助

详细信息
    作者简介:

    曹金秋(1992-),硕士研究生,研究方向为微型扑翼飞行器扑翼机构设计及样机研制,caojinqiu23@163.com

    通讯作者:

    朱建阳,讲师,博士,zhujianyang02@163.com

Design and Analysis of 6R Spatial Flapping-wing Mechanism with Two Degrees of Freedom

  • 摘要: 对现有空间连杆机构进行分析改进,提出了一种6R对称布置的具有两自由度的空间扑翼机构。首先,通过对6R空间扑翼机构理论计算和仿真分析,得到了不同杆长对翼尖"8"字形轨迹的影响规律。然后,提出通过调整扑翼平均上反角来提高飞行平稳性的方法。最后,采用Adams对本文设计的机构进行仿真分析,结果表明所设计的空间扑翼机构传动流畅平稳,并满足扑动角和扭转角相位相差90°。
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出版历程
  • 收稿日期:  2016-11-14
  • 刊出日期:  2018-02-25

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