期刊文献+

中温固化阻燃结构胶膜流变特性与蜂窝粘接性能 被引量:7

Rheology and Honeycomb Adhesion Property of the Flame-retardant Structural Adhesive Film Cured at Moderate Temperature
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摘要 研究了用于蜂窝夹层结构粘接的阻燃结构胶膜的化学流变特性与蜂窝粘接性能。通过流变仪研究了胶膜固化过程中化学黏度的变化,考察了固化反应(温度、时间)、阻燃剂、增韧剂对体系化学流变特性的影响。分析了流变特性和胶瘤形成在蜂窝夹层结构粘接过程中的作用,并测试了蜂窝夹层结构的剥离和平面拉伸性能。结果表明:阻燃剂的加入使得体系100℃前的黏度有所升高,固化活性略有降低,最低黏度温度从112℃推迟到120℃;加入增韧剂后的胶黏剂的黏度显著提高,制备的阻燃胶膜最低黏度在50Pa.s左右,固化过程中具有适宜的流动性和胶瘤形状,固化后具有较高的滚筒剥离强度和平面拉伸强度。 The ehemorheology and honeycomb adhesion properties of an epoxy structural adhesive film with flame retardancy used in honeycomb sandwich structure bonding was studied. The chemical viscosity was measured by a rheometer during the curing process of adhesive film, the influences of curing temperature and time, flame retardants and toughening agents on the chemorheology of the adhesive film were investigated. The role of ehemorheology and formation of symmetric fillet during the adhesion proeess was discussed and the peel and flatwise tensile strength was determined. The presence of the flame retardants slightly increased the viscosity under 100℃, decelerated the progression of the curing reaction, and shifts the minimum viscosity temperature from 112℃ to 120 ℃. The addition of the toughening agent increased the viscosity dramatically and thus the prepared flame-retardant adhesive film exhibited a lowest viscosity of 50Pa.s, the proper chemorheology and symmetric fillet during the curing process. The adhesive film showed an excellent roller peel strength and flatwise tensile strength.
出处 《化学与粘合》 CAS 2012年第5期17-21,共5页 Chemistry and Adhesion
关键词 阻燃胶膜 化学流变 胶瘤 蜂窝夹层结构 Flame-retardant adhesive film chemorheology adhesive fillet honeycomb sandwich structure
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参考文献8

  • 1GRIMES G C. The adhesive-honeycomb relationship[j]. AppliedPolymer Symposia, 1996(3): 157-190.
  • 2OKADA U, KOKTSCHOT M T. The role of the resin fillet in thedelamination of honeycomb sandwich structures [j]. CompositesScience and Technology, 2002,62(14): 1811-1819.
  • 3原崇新,李敏,顾轶卓,张佐光.蜂窝夹层结构真空袋共固化工艺过程实验研究[J].复合材料学报,2008,25(2):57-62. 被引量:31
  • 4CHEN L,WANG Y Z. A review on flame retardant technology inChina[j].Part I: development of flame retardants[ J].Polymers forAdvanced Technologies ,2010,21(1): 1-26.
  • 5ROLLER M B. Rheology of curing thermosets: A review[j].Poly-mer Engineering & Science, 1986,26(6): 432-440.
  • 6HALLEY P J, MACKAY M E. Chemorheology of thermosets-anoverview [j].Polymer Engineering & Science, 1996,36 (5): 593 -609.
  • 7BUTUKURI R H, BHEEMREDDY V P. Evaluation of skin-coreadhesion bond of out -of-autoclave honeycomb sandwich struc-tures[j]. Journal of Reinforced Plastics and Composites,2012,31(5): 331 -339.
  • 8HION J,LETEHRIEH Y. Prediction of the adhesive fillet size forskin to honeycomb core bonding in ultra-light sandwich struc-tures [J ].Composites Part A: Applied Science and Manufacturing,2008,39(9): 1547-1555.

二级参考文献10

  • 1赵卫娟,张佐光,王景明.树脂流动对气泡运动特性的影响[J].复合材料学报,2006,23(2):25-29. 被引量:8
  • 2Ryo O, Kortschol M T. The role of the resin fillet in the delamination of honeycomb sandwich structures [J]. Composites Science and Technology, 2002, 62(14) :1811-1819.
  • 3Kishi H, Nishimura A, Odagiri N. " TORAYCA" T700 fabric/3680 self-adhesive type honeycomb cocure prepreg [J]. SAMPE Journal, 2001, 37(2): 89-92.
  • 4Vadakke V, Carlsson L A. Experimental investigation of compression failure of sandwich specimens with face/core debond [J]. Composites Part B, 2004, 35(6/8): 583-590.
  • 5Young Wenbin. Resin flow analysis in the consolidation of multi - directional laminated composites [J]. Polymer Composites, 1995, 16(3):250-257.
  • 6Grove S M, Popham E, Miles M E. An investigation of the skin/core bond in honeycomb sandwich structures using statistical experimentation techniques [J]. Composites Part A, 2006, 37(5): 804-812.
  • 7Nam J D, Sefferis J C. Gas permeation and viscoelastic deformation of prepregs in composite manufacturing processes [J]. Polymer Composites, 1995, 16(5):370-377.
  • 8Wood J R. Bader M G. Void control for polymer- matrix composites Ⅰ:Theoretical and experimental methods for determining the growth and collapse of gas bubbles [J]. Composites Manufacturing, 1994, 5(3): 139-147.
  • 9Campbell F C, Mallow A R. Porosity in carbon fiber composites an overview of causes [J].Journal of Advanced Materials, 1995, 26(4) : 18-33.
  • 10张广成,赵景利.蜂窝夹层结构复合材料的力学性能研究[J].机械科学与技术,2003,22(2):280-282. 被引量:34

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