EXPERIMENTAL RESEARCH ON THE REPAIR OF THE DAMAGE IN HONEYCOMB-CORE T700/BMI COMPOSITE SANDWICH STRUCTURES

Abstract

Abstract: Honeycomb sandwich structures and three different aperture semi-penetrating damage parts were prepared in this paper. The damage is repaired by patching technology, including high temperature repair (homogeneous repair) and middle temperature repair (heterogeneous repair). The mechanical properties were tested at room temperature and high temperature. The results show that there is little difference on performance recovery of the damaged specimens between homogeneous repair and heterogeneous repair. And due to the poor manufacturability and high cure temperature (>177℃), damages tend to occur on other components. Heterogeneous repair, however, has better manufacturability and lower cure temperature, which can not only recover the properties of the damaged successfully but is suitable for rapid repair.

Key words: honeycomb sandwich structure, heterogeneous repair, mechanical property

CLC Number:

TB332

LI Cai-yan, XING Su-li, ZHU Bao-jun, XIAO Jia-yu. EXPERIMENTAL RESEARCH ON THE REPAIR OF THE DAMAGE IN HONEYCOMB-CORE T700/BMI COMPOSITE SANDWICH STRUCTURES[J]. COMPOSITES SCIENCE AND ENGINEERING, 2014, 0(11): 48-53.

References

[1] 董永琪. 夹芯结构的新进展[J]. 玻璃钢/复合材料,1997,(3):30-32.
[2] 马世勇,刘洪军. 玻璃钢夹芯材料的应用[J]. 玻璃钢/复合材料,2001,(4):53-55.
[3] F.E.Sezgin, M. Tanog Lu. Mechanical behavior of polypropylene-based honeycomb-core composite sandwich structures[J]. Journal of reinforced plastics and composites, 2010, 29(10): 121-125.
[4] Nicolas J. Lombardi, Judy Liu. Glass fiber-reinforced polymer/steel hybrid honeycomb sandwich concept for bridge deck applications[J]. Composite Structures, 2011, 93: 1275-1283.
[5] 冯消冰,王伟. 2MW风机复合材料叶片材料及工艺研究[J]. 玻璃钢/复合材料,2010,(7):84-88.
[6] Sokolinsky V S, Shen Hongbin, Lev V, et al. Experimental and analytical study of nonlinear bending response of sandwich beams[J].Composite Structure,2003,60:219-229.
[7] 李真,周化刚,薛元德. 剪切对泡沫夹层结构梁弯曲性能的影响[J]. 玻璃钢/复合材料,2011,(2):19-23.
[8] 季铁正, 蓝立文, 王宝山. 蜂窝夹心板的结构与应用[J]. 新型建筑材料, 1995,(2):31-33.
[9] 夏利娟,金咸定,汪庠宝. 卫星结构蜂窝夹层板的等效计算[J]. 上海交通大学学报,2003:999-1001.
[10] Ullmann T, Aoki R, Schmidt T. Lock-in thermography for process integrated non-destructive evaluation of carbon fibers reinforced aircraft structures[C]. 10th International Conference on QIRT, 2010.
[11] 赵祖虎. 蜂窝夹层结构的修补[J]. 航天返回与遥感,1994, 3(15): 63-67.
[12] 曲亚林,宁宁,詹绍正. 蜂窝夹芯结构的无损检测技术[J]. 航空制造技术, 2011, (20): 78-81.
[13] 翟光,杨小平. 多夹心层蜂窝板动力学特性分析与仿真[J]. 计算机仿真, 2006,8(23): 44-45.
[14] 朱翔. 复合材料蜂窝夹层结构总体稳定性分析的有限元法[J]. 洪都科技,2010: 17-22.
[15] 梁月华,韦娟芳. 蜂窝夹层结构镶嵌件拉伸承载力分析[J]. 空间电子技术, 2012: (1), 35-38.
[16] Avery J L, Sonkar B V. Compressive failure of sandwich beams with debonded face-sheets[J]. Journal of Composite Materials, 2000,34(14):1176-1199.
[17] 沃西源,夏英伟,涂彬. 蜂窝夹层结构复合材料特性及破坏模式分析[J]. 航天返回与遥感,2005,4(26):45-49.
[18] Tomblin J S, Salah L, Welch J M, et al. Bonded repair of aircraft composite sandwich structures, DOT/FAA/AR-03/74[R]. US Department of Transportation Federal Aviation Administration,2004.
[19] 许潮华,张小珍,宋桂枝. “Nomex”蜂窝芯材的研制和应用[J]. 玻璃钢/复合材料,1986,(2):22-24.
[20] 孙春芳,李文晓,薛元德,等. 高速列车用PMI泡沫力学性能研究[J]. 玻璃钢/复合材料,2006,(4):13-15.
[21] 汤超,乔玉炜. PMI泡沫夹层结构梁弯曲性能的影响[J]. 玻璃钢/复合材料,2011,(2):19-23.