期刊文献+

X-Cor夹层结构的平压性能试验 被引量:2

Experimental on Compressive Behavior of X-Cor Sandwich
下载PDF
导出
摘要 通过对不同的z-pin角度、面板厚度、去除泡沫处理的X-Cor夹层结构试样进行平压性能试验和分析比较,得到其破坏模式及不同设计参数对性能的影响。试验结果表明:X-Cor夹层结构中z-pin和泡沫存在协同增强效应;增大z-pin端部约束和减少z-pin的植入角度能提高平压性能;但z-pin角度为0°的夹层结构平压性能对植入角的角偏差缺陷更敏感,缺陷的存在影响承力性能。 Comparison tests of compressive properties were carried out on different z-pin angle, face skin thickness ,with and without foam, which could be acquired the failure modes of X-Cor sandwich and the effect of different design parameters on compressive properties. Experimental results show that the combination of z-pins and foam core lead to a synergistic strengthening. Increasing restriction of z-pin' s end and decreasing the angle between z-pin and face sheet can enhace the compressive properties. But the compressive properties of z-pin angle with 0° are more to sensitive to angle deviation error, and it directly affects behavior of perfect mechanicals properties.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2012年第3期78-81,共4页 Aerospace Materials & Technology
关键词 X-COR夹层结构 平压性能 对比试验 角偏差缺陷 X-Cor sandwich, Compressive property, Comparison test,Angle deviation error
  • 相关文献

参考文献11

  • 1窦润龙,胡培.复合材料泡沫夹层结构在民机中的应用[J].民用飞机设计与研究,2004(3):42-45. 被引量:18
  • 2Majumdar P, Srinivasagupta D, Mahfuz H, et al. Effect of processing conditions and material properties on the debond frac- ture toughness of foam-core sandwich composites : experimental op- timization [ J ]. Composites Part A,2003,34 ( 11 ) : 1097-1104.
  • 3Zabihpoor M, Adibnazari S. Mechanisms of fatigue dam- age in foam core sandwich composites with unsymmetrical carbon/ glass face sheets[ J]. Journal of Reinforced Plastics and Compos- ites ,2007,26 ( 17 ) : 1831 - 1842.
  • 4Carstensen T C, Kunkel E, Magee C. X-CorTM advanced sandwich core material [ C ] //Falcone A, International SAMPE Technical Conference Series, CA: Society of Advancement Material and Process Engineering,2001:452-466.
  • 5Carti6 D D, Fleck N A. The effect of pin reinforcement upon the through-thickness compressive strength of foam-cored sandwich panels [ J]. Composites Science and Technology, 2003, 63:2401-2409.
  • 6Andrea I Marasco, Carti6 D D, Partridge I. K, et al. Me- chanical properties balance in novel z-pinned sandwich panels: out-of-plane properties [ J ]. Composites : Part A,2006,37 (2) : 295 -302.
  • 7Andrea I Marasco. Analysis and evaluation of mechani- structures :X-Cor and K- cal performance of reinforced sandwich TM CorTM [ D ]. Cranfield University,2005.
  • 8田旭,肖军,李勇.X-cor夹层结构试制与性能研究[J].飞机设计,2004,24(1):22-25. 被引量:30
  • 9李廉锟.结构力学[M].北京:高等教育出版社,1996.82-14.
  • 10刘鸿文.材料力学[M].北京:高等教育出版社,2007.

二级参考文献8

  • 1[1]Carstensen T,Cournoyer D,Edward K,et al.X-corTMadvanced sandwich core material.In:Falcone A ed.Advancing Affordable Materials Technology,33rd Internation SAMPE Technical Conference November 5-8,2001.452-466.
  • 2[2]O' Brien K T,Paris I L.Exploratory investigation of failure mechanisms in transition regions between solid laminates and X -cor (R○)truss sandwich(网上下载PDF文献).
  • 3[4]Vaidya U K,Nelson S,Sinn B,et al.Processing and high strain rate impact response of multi-functional sandwich composites.Composite Structure,2001(52):429-440.
  • 4[6]沃丁柱,周山,等.高分子泡沫材料.南京:南京大学出版社,1996.
  • 5[7]全国纤维增强材料标准化技术委员会秘书处.纤维增强塑料(玻璃钢)标准汇编.北京:中国标准出版社,1998.
  • 6K.R.Braziel,C.L.Cartwright.Commercial Aircraft Nose Radomes Using Rigid Foam Core Sandwich Construction[].Sandwich Constructions.
  • 7L.Herbeck,,Markus Kleineberg,C.Schopinger.FOAM CORES IN RTM STRUCTURES:MANUFACTURING AID OR HIGH-PERFOR-MANCE SANDWICH?[].SAMPE.
  • 8周祝林,徐玉珍,孙佩琼.复合材料平板及蜂窝芯综合性能测试与分析[J].纤维复合材料,2002,19(4):17-20. 被引量:11

共引文献92

同被引文献20

引证文献2

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