期刊文献+

大型双曲蜂窝夹层结构短舱成型工艺研究 被引量:3

Investigation on the manufacturing process of large-scale nacelleswith double curved honeycomb sandwich structure
下载PDF
导出
摘要 大型双曲蜂窝夹层结构是复合材料制件中一种较复杂的结构形式,它具有尺寸大、型面复杂等特点,但是其力学承载特性好、整体重量轻、抗变形能力强,应用较广。本文以大型双曲蜂窝夹层结构短舱制件为研究对象,详细论述了其结构特点以及加工工艺方法,重点解决了蜂窝芯易收缩、难固定,装配区要求高等技术难点,通过实验方案验证及实验数据分析,综合比对实验结论以及工程差异性,最终得到了一套行之有效的成型方法。 The large hyperbolic honeycomb sandwich structure is a kind of complex structure form in composite materials,it has the charecteristics of large size and complex profile.But its mechanical bearing performance is good,light weight,and has strong resistance to deformation.Sandwich nacelles are studied,the structure characteristics and processing technology are discussed in detail.The honeycomb core is easy to shrink and hard to fix,and the assembly area requires high technical difficulties.The experimental scheme,experimental data,and engineering differences are analyzed and compared.Finally,a set of effective forming methods were obtained.
作者 王莹 肖光明 贺韡 WANG Ying;XIAO Guang-ming;HE Wei(AVIC XI'an Aircraft Industry Group Company Ltd.,Xi'an 710089,China;The First Military Representative Office of Air Force Armament Department in Xi'an,Xi'an 710089,China)
出处 《复合材料科学与工程》 CAS 北大核心 2021年第7期99-104,共6页 Composites Science and Engineering
关键词 双曲 蜂窝夹层结构 短舱 复合材料 hyperbolic honeycomb structure nacelles composites
  • 相关文献

参考文献2

二级参考文献14

  • 1万里冰,武湛君,张博明,王殿富.光纤布拉格光栅监测复合材料固化[J].复合材料学报,2004,21(3):1-5. 被引量:26
  • 2沈真.复合材料结构设计手册[M].北京:航空工业出版社,2001.
  • 3Fernlund G,Rahman N,Courdji R,et al.Experimental andnumerical study of the effect of cure cycle,tool surface,aspectratio,and the lay-up on the dimensional stability of autoclave-processed composite parts Q].Composites Part A,2002,33(3):341-351.
  • 4Johnston A,Vaziri R,Poursartip A.A plane strain model forprocess-induced deformation of laminated composite structures[J].J Compos Mat,2001,35(16):1435-1469.
  • 5Radford D W,Rennick T S.Separating sources ofmanufacturing distortion in laminated composites [ J].JReinforced Plast Compos,2000,19(8):621-641.
  • 6Potter K D,Campbell M,Langer C,et al.The generation ofgeometrical deformations due to tool part interaction in themanufacture of composite components [J].Composites PartA,2005,36(2):301-308.
  • 7Satish K B,Lloyd V S.A linear finite element model topredict processing-induced distortion in FRP laminates [J].Composites Part A,2005,36(12):1666-1674.
  • 8Twigg G,Poursartip A,Fernlund G.An experimental method forquantifying tool-part shear interaction during composites processing[J].Compos Sci Technol,2003,63(13):1985-2002.
  • 9Twigg G,Poursartip A,Fernlund G.Tool-part interaction incomposites processing I:Experimental investigation and analyticalmodel [J].Composites Part A,2004,35(1):121-133.
  • 10Hughes William J.Metallic materials properties developmentand standardization [ M].Columbus:Federal AviationAdministration,2010:440-451.

共引文献35

同被引文献28

引证文献3

二级引证文献1

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