期刊文献+

可充气聚焦器的展开过程及聚焦性能仿真

Simulation for Deployment Process and Concentrating Performance of Inflatable Concentrator
在线阅读 下载PDF
导出
摘要 为了研究可充气聚焦器的展开过程及展开后的性能,以一个开口面积为20 m2,焦距为8 m的旋转抛物面型太阳能聚焦器为例建立了充气结构模型,采用控制体积法对一次和三次折叠的未充气状态的支撑杆及反射部件的展开过程进行了仿真计算。基于充气反射面展开后的几何模型,采用蒙特卡罗光线跟踪法,数值模拟了其对光线的聚焦性能。结果表明展开后的反射面聚焦效率约为理想设计曲面的57%,褶皱是其聚焦性能不高的主要原因。分析展开后结构的聚焦效率可以作为评价可充气展开结构展开性能优劣的一种新方法。 To study the deployment process and deployed characteristics of the inflatable concentrator, a paraboloidal dish concentrator, whose aperture and focal length are 20 m2 and 8 m respectively, is built and taken as an example. The deployment of the one-fold and three-fold inflatable support truss and reflecting part is simulated with the control volume method. Based on the geometrical model of a deployed reflecting surface, the concentrating characteristics on the receiving plane are performed with the Monte Carlo ray tracing method. The results show that the concentrating efficiency of the deployed structure is 57% of the designed one, and the low concentrating efficiency is mainly caused by the wrinkling of the reflecting surface. Analysis of unfolded structure's concentrating efficiency can be as a new method to evaluate the deployment performance of deployable structure.
出处 《南京理工大学学报》 EI CAS CSCD 北大核心 2012年第1期73-78,共6页 Journal of Nanjing University of Science and Technology
基金 江苏高校优势学科建设工程资助项目
关键词 可充气聚焦器 展开 蒙特卡罗光线跟踪法 褶皱 数值模拟 inflatable concentrators deployment Monte Carlo ray tracing method wrinkling numerical simulation
作者简介 王磊磊(1982-),男,博士生,主要研究方向:太阳能利用,E—mail:wll-youth@163.com; 通讯作者:黄护林(1968-),男,博士,教授,主要研究方向:太阳能利用,磁流体流动与传热,E-mail:hlhuang@nuaa.edu.cn。
  • 相关文献

参考文献17

  • 1刘明治,高桂芳.空间可展开天线结构研究进展[J].宇航学报,2003,24(1):82-87. 被引量:70
  • 2Salama M,Kuo C P,Lou M.Simulation of deploymentdynamics of inflatable structures[J].AIAA Journal,2000,38(12):2277-2283.
  • 3Freeland R E,Billyeu G D.In-step inflatable antennaexperiment[A].IAF Proceedings of the 43rd Congressof the International Astronautical Federation[C].Washington D C:IAF,1992:1-12.
  • 4Pappa R S,Giersch L R,Quagliaroli J M.Photogrammetryof a 5m inflatable space antenna with consumer digitalcameras[R].Technical Memorandum/TM-2000-210627.Washington:NASA,2000:1-11.
  • 5Naboulsi S.Investigation of geometric imperfection ininflatable aerospace structures[J].Journal of AerospaceEngineering,2004,17(3):98-105.
  • 6Tang T N.Edge effects in pressurized membranes[J].Journal of Engineering Mechanics,2002,128(10):1100-1104.
  • 7Richard C,Eric S.Design and flight qualification of therigidizable inflatable get-away-special experiment[J].Journal of Spacecraft and Rockets,2010,47(4):659-669.
  • 8Raymond L,David T.Computational investigation offlow over inflatable airfoils at multiple reynoldsnumbers[A].49th AIAA Aerospace Sciences Meetingincluding the New Horizons Forum and Aerospace Ex-position[C].Orlando,Florida:AIAA,2011:4-7.
  • 9徐彦,关富玲,管瑜.充气可展天线精度分析和形面调整[J].空间科学学报,2006,26(4):292-297. 被引量:13
  • 10徐彦,关富玲,马燕红.充气可展开天线的反射面设计及精度测量[J].浙江大学学报(工学版),2007,41(11):1921-1926. 被引量:16

二级参考文献54

  • 1向阳,沈世钊,赵臣.张拉式薄膜结构的弹性模型风洞实验研究[J].空间结构,1998,4(3):31-36. 被引量:11
  • 2向阳,沈世钊.薄膜结构的实用裁剪设计方法[J].空间结构,1999,5(2):46-50. 被引量:13
  • 3杜星文,王长国,万志敏.空间薄膜结构的褶皱研究进展[J].力学进展,2006,36(2):187-199. 被引量:15
  • 4宋昌永 沈世钊.薄膜结构形状确定分析.第六届空间结构学术会议论文集[M].广州:-,1992.572-579.
  • 5郭璐 蓝天.膜结构的初始形状判定与静力分析及其模型试验研究.第七届空间结构学术会议论文集[M].文登:-,1994..
  • 6李中立 吴健生 等.膜结构成形受荷与裁剪分析.第八届空间结构会议论文集[M].开封:-,1997.229-304.
  • 7蓝天.膜结构的发展及其在中国的应用前景.第八届空间结构学术会议论文集[M].开封:-,1997.291-298.
  • 8刘明治.スパン展开构造物の质量分布及び形状分析[J].日本宇宙科学研究,所名取研第七回ゼミナ-,1995,12.
  • 9陈艳.[D].西安电子科技大学,1994.
  • 10[3]CLIFF E W,RON C S.A hybrid inflatable dish antenna system for spacecraft[C]∥Proceedings of the 42th AIAA/ASME/ASCE/AHS/ASC SDM Conference.Seattle:AIAA,2001:1-9.

共引文献145

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