期刊文献+

腿式着陆器缓冲材料缓冲特性及其表征方法研究 被引量:17

Study on Cushion Properties and Its Characterization Methods of Legged Lander's Cushion Materials
下载PDF
导出
摘要 为了研究适合腿式着陆器用缓冲器的缓冲材料,对8种不同规格的薄壁铝管,3种不同规格的铝蜂窝及4种不同规格的泡沫铝在准静态及冲击载荷作用下的压缩特性进行了试验研究,并得出了其相应的应力/能量-应变曲线图。通过对缓冲材料的应力-应变曲线图及压缩特性进行系统的研究分析,得到了5类缓冲材料缓冲特性的表征方法,这些表征方法可以全面地对不同缓冲材料的缓冲特性进行评价,以便指导腿式着陆器用缓冲器的设计。最后结合所提出的缓冲材料缓冲特性的表征方法,对所试验的薄壁铝管、铝蜂窝及泡沫铝这3类不同的缓冲材料的缓冲特性进行了总结,并得到了粗孔的名义压缩强度为0.14~0.15MPa的泡沫铝为在所试验的缓冲材料中,是最理想的腿式着陆器用缓冲材料。 In order to investigate the cushion materials suitable for shock absorber of legged Lander, experimental investigations were carried out to study quasi-static and dynamics compressive behavior of eight different specification thin- walled aluminum tubes, three different specification aluminum honeycombs and four different specification aluminum foams, whose stress/energy-strain curves were also given. Five kinds of characterization methods of cushion properties on cushion materials obtained through systematical analysis of the stress-strain curves and compressive behavior of the cushion materials. These methods can be used to evaluate the cushion properties comprehensively, and guide design legged Lander's shock absorber. At last, based upon the characterization methods of cushion properties on cushion materials, the cushion properties of thin-walled aluminum tube, aluminum honeycomb and aluminum foam were summarized, the coarse-hole aluminum foam with nominal stress strength 0.14 -0.15MPa is the best selection for legged Lander's cushion material of these samples.
出处 《宇航学报》 EI CAS CSCD 北大核心 2009年第2期786-794,共9页 Journal of Astronautics
基金 国家自然科学基金(50775048) 高等学校学科创新引智计划(B07018)
关键词 着陆器 薄壁铝管 铝蜂窝 泡沫铝 缓冲特性 表征方法 Lander Thin-walled aluminum tube Aluminum honeycomb Aluminum foam Cushion properties Characterization method
  • 相关文献

参考文献8

  • 1Taylor Inc. Investigation of the application of airbag to provide soft landing[ C ]. AIAA, 2001 : 2001 - 2045.
  • 2Sperling F B. The surveyor shock absorber [ C ]. AIAA N50 - 17368, 1964.
  • 3刘志全,黄传平.月球探测器软着陆机构发展综述[J].中国空间科学技术,2006,26(1):33-39. 被引量:36
  • 4Milton Beilock. Surveyor Lander Mission Capability[ R]. NASA N64 - 228969, 1964.
  • 5Thornton P H, Magee C L. The interplay of geometric and materials variables in energy absorption [ J]. J. Eng. Mat. Tech. , 1977, 99:114-120.
  • 6风仪.泡沫铝的动态力学性能及物理性能研究[D].中国科学院博士论文,2002.
  • 7Gibson L J, Ashby M F. Cellular Solid: Structure and Properties, 2nd ed[ M]. Cambridge University Press, 1997.
  • 8Mihz J, Gruenbaum G. Evaluation of cushion properties of plastic foams compressive measurements [ J ]. Polymer Engineering and Science, 1981, 21 : 1010 - 1024.

二级参考文献7

  • 1Taylor Inc. Investigation of The Application of Airbag to Provide Softlanding. AIAA 2001 2045, 2001.
  • 2Sperling F B. The Surveyor Shock Absorber. AIAA N50-17368, 1964.
  • 3Milton Beilock. Surveyor Lander Mission Capability, NASA N64-28969, 1964.
  • 4Lavochkin. The Lunokhod unmanned lunar-17 surface rover. NASA 1976-081A, 1976.
  • 5Nelson M Inc. The progression of EuroMoon 2000. NASA1996-78, 1996.
  • 6Finzi A E, Vasile M. Optimal Trajectory Attitude Manoeuvres for apollo Missions. IAF-98-A410, 1998.
  • 7邓宗全,王少纯,胡明,高海波,邱雪松.微小型航天着陆器技术初探[J].导弹与航天运载技术,2003(2):1-6. 被引量:11

共引文献35

同被引文献412

引证文献17

二级引证文献125

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