用于西锐SR20复合材料胶接维修的国产中温固化胶膜性能研究

玻璃钢/复合材料 ›› 2018, Vol. 0 ›› Issue (6): 44-47.

用于西锐SR20复合材料胶接维修的国产中温固化胶膜性能研究

徐艺, 贺强

中国民用航空飞行学院民航安全工程学院,广汉618307

收稿日期:2017-11-24 出版日期:2018-06-28 发布日期:2018-06-28
作者简介:徐艺(1985-),女,博士,讲师,主要从事复合材料方面的研究,xuyi99@yeah.net。
基金资助:
中国民用航空飞行学院博士科研启动基金(BJ2016-01);中国民用航空飞行学院青年基金(Q2018-43);中央高校教育教学改革专项项目(E20170207)

STUDY ON THE PERFORMANCE OF THE MID-TEMPERATURE CURED ADHESIVE FILM USEDFOR BONDING REPAIRING OF CIRRUS SR20 COMPOSITES

XU Yi, HE Qiang

Civil Aviation Safety Engineering Institute, Civil Aviation Flight University of China,Guanghan 618307, China

Received:2017-11-24 Online:2018-06-28 Published:2018-06-28

摘要/Abstract

摘要： 研究了自制中温胶膜J-12和西锐SR20复合材料维修手册提供的AF-163-2M中温胶膜的固化工艺、力学性能及使用温度差异。结果显示:两胶膜在120 ℃~130 ℃时具有较好的固化速率,均能在150 ℃长期使用,满足SR20复合材粘接维修需要;室温下J-12胶膜固化物AF-163-2M胶膜单搭接拉伸剪切强度分别为30.1 MPa、27.4 MPa,J-12胶膜固化物的剪切强度优于AF-163-2M胶膜固化物。综上所述,国产J-12胶膜性能与AF-163-2M胶膜性能相当,可作为替代性产品应用于西锐SR20复合材料粘接维修。

关键词: 中温固化胶膜, 拉伸剪切, 固化工艺, 耐热性

Abstract: The differences between the curing process, mechanical properties and temperature of J-12 medium-temperature adhesive film were compared with those of AF-163-2M which was suggested to use in bonding repair of Cirrus SR20 composites. It was found that those two adhesive films have good curing rate between 120 ℃ and 130 ℃, and both of them could maintain good mechanical properties at 150 ℃ and meet the maintenance needs of Cirrus SR20 composites. The single lap shear tensile strength of cured J-12 adhesive film and AF-163-2M film were 30.1 MPa and 27.4 MPa at room temperature, respectively. The shear strength of cured J-12 film is better than that of cured AF-163-2M film. To sum up, the comprehensive performances of J-12 adhesive film are similar to those of AF-163-2M adhesive film, which could be used as an alternative product used in the Cirrus SR20 composites bonding repairing.

Key words: mid-temperature cured adhesive film, tensile shearing, curing process, heat resistance

中图分类号:

TB332

徐艺, 贺强. 用于西锐SR20复合材料胶接维修的国产中温固化胶膜性能研究[J]. 玻璃钢/复合材料, 2018, 0(6): 44-47.

XU Yi, HE Qiang. STUDY ON THE PERFORMANCE OF THE MID-TEMPERATURE CURED ADHESIVE FILM USEDFOR BONDING REPAIRING OF CIRRUS SR20 COMPOSITES[J]. Fiber Reinforced Plastics/Composites, 2018, 0(6): 44-47.

参考文献

[1] 王跃全. 飞机复合材料结构修理设计渐进损伤分析[D]. 南京:南京航空航天大学, 2010.
[2] 沈军, 谢怀勤. 航空用复合材料的研究与应用进展[J]. 玻璃钢/复合材料, 2006(5): 48-54.
[3] Katnam K, Silva D, Young T. Bonded repair of composite aircraft structures: A review of scientific challenges and opportunities[J]. Progress in Aerospace Sciences, 2013(61): 26-42.
[4] 西锐SR20:230万的全复合材料安全教练机[J]. 玻璃钢/复合材料, 2014(2): 90.
[5] 徐绯, 刘斌, 李文英, 等. 复合材料修理技术研究进展[J]. 玻璃钢/复合材料, 2014(8): 105-112.
[6] 汤洪涛. 航空复合材料维修[J]. 航空制造技术, 2007(10): 62-64.
[7] 张翠芳. 特种胶粘剂的研究进展及应用[J]. 广东化工, 2014, 41 (11): 163-164.
[8] 韩凤志, 李东临. 耐高温环氧树脂胶黏剂的研究进展[J]. 广东化工, 2014, 41(8):94-95.
[9] Hawyes V, Curtis P, Soutis C. Effect of impact damage on the compressive response of composite laminates[J]. Composites Part A: Applied Science and Manufacturing, 2001, 32(9):1263-1270.
[10] Jones R, Chiu W K,Smith R. Airworthiness of composite repairs:failure mechanisms[J]. Engineering Failure Analysis, 1995, 2(2): 117-128.
[11] 张明. 通用航空环氧树脂的固化和相行为研究[D]. 北京: 北京航空材料研究院, 2006.
[12] 杜善义, 关志东. 我国大型客机先进复合材料技术应对策略思考[J]. 复合材料学报, 2008, 25(1):1-10.
[13] 乔海涛, 邹贤武. 复合材料胶接技术的研究进展[J]. 宇航材料工艺, 2010(2): 11-14.
[14] 赵渠森. 先进复合材料手册[M]. 北京: 机械工业出版, 2003.
[15] 程小全, 彭霄婧, 胡仁伟, 等. 碳纤维复合材料结构修理用胶黏剂应用研究[J]. 高科技纤维与应用, 2015, 40(5): 12-20.
[16] Armstrong K B. The selection of adhesives for aircraft repairs based on fundamental mechanical properties of the resins themselves (Phase Ⅱ)[M]. In Adhesion 13, Springer Netherlands: Dordrecht, 1989: 237-277.
[17] Ubin A M, Perl D R. Composite structures repair development for the F/A-18E/F aircraft[C]//In: 40^th international SAMPE symposium, 1995: 154-167.
[18] Chabot K A, Bonk R B. Evaluation of adhesives and primers systems for adhering carbon/epoxy composites and metals[C]//In:25^th international SAMPE technical conference, 1993: 338-352.
[19] Bill Nickolson. Development of a 180°F hot/wet service temperature paste adhesive for composite fabrication[C]//In:34^th international SAMPE symposium, 1989: 631-642.
[20] Tillman M S, Hayes B S,Seferis J C. Influence of substrate-adhesive resin compatibility on the fracture of composite bonds[C]//In: 46^th international SAMPE symposium, 2001: 8-19.
[21] 李岩, 刘泊天, 张静静, 等. MD-130胶黏剂固化工艺及空间适用性研究[J]. 宇航材料工艺, 2015, 45(1): 40-42.
[22] 赵汉清, 于昕, 付刚, 等. J-133B(AE)室温固化结构胶黏剂体系[J]. 化学与黏合, 2008, 30(4): 23-26.
[23] 曲春艳, 王德志, 冯浩. J-18双马来酰亚胺基复合材料胶接用结构胶膜[J]. 材料工程, 2007(s1): 15-19.
[24] 邹贤武, 乔海涛, 齐楠. SY-D15表面处理剂的性能研究[J]. 粘接, 2007(2): 10-12.