低温共固化高阻尼复合材料

doi:10.7527/S1000-6893.2018.22721

材料工程与机械制造

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低温共固化高阻尼复合材料

郑长升¹, 梁森¹, 陈静², 梁恒亮²

1. 青岛理工大学机械与汽车工程学院, 青岛 266520;
2. 中航复合材料有限责任公司, 北京 101300

收稿日期:2018-10-10 修回日期:2018-11-09 出版日期:2019-08-15 发布日期:2019-01-11
通讯作者: 梁森 E-mail:liangsen888111@163.com
基金资助:
国家自然科学基金（51375248）

Low-temperature co-cured high damping composites

ZHENG Changsheng¹, LIANG Sen¹, CHEN Jing², LIANG Hengliang²

1. School of Mechanical and Automotive Engineering, Qingdao University of Technology, Qingdao 266520, China;
2. AVIC Composite Corporation Ltd., Beijing 101300, China

Received:2018-10-10 Revised:2018-11-09 Online:2019-08-15 Published:2019-01-11
Supported by:
National Natural Science Foundation of China (51375248)

摘要/Abstract

摘要： 在低温下实现了嵌入式阻尼复合材料的共固化，且共固化层合板具有良好的层间结合性能。通过正交试验研制出一种能够与玻璃纤维/酚醛树脂预浸料在80℃时共固化且力学性能优良的黏弹性材料组分。探索使用强极性的四氢呋喃作为溶剂将黏弹性阻尼材料溶解为阻尼胶浆，然后用刷涂工艺制作带阻尼薄膜的预浸料，最终按照预定的铺层经过共固化工艺制备出嵌入式低温共固化复合材料试件。自由衰减试验及层间剪切试验获得了阻尼性能及剪切性能随阻尼层厚度的变化规律曲线，实验数据表明：随着阻尼层厚度增大，复合材料结构的阻尼系数变大，层间剪切应力逐渐减小。

关键词: 低温共固化, 阻尼复合材料, 刷涂工艺, 阻尼薄膜, 阻尼性能, 剪切性能

Abstract: The co-curing of embedded damping composites is achieved at low temperatures, and the co-cured laminates possessed superior interlayer bonding property. An orthogonal test is implemented to develop a viscoelastic material ingredient capable of co-curing with fiberglass/phenolic resin prepreg at 80℃, obtaining excellent mechanical properties. The strong polar tetrahydrofuran is employed as a solvent to dissolve the viscoelastic damping material into damping paste, then the prepreg with damping film is manufactured using the brushing coating process. Finally, based on the scheduled layup sequence, the embedded low-temperature co-cured composite specimens are prepared through the co-curing process. The curves of the damping and shear properties with respect to damping layer thickness were obtained through free decay test and interlaminar shear test. The experimental data indicated that the thicker the damping film, the larger the composite structure damping coefficient, and the lower the interlaminar shear stress.

Key words: low-temperature co-cured, damping composites, brushing process, damping film, damping property, shear property

中图分类号:

V258
TB332

郑长升, 梁森, 陈静, 梁恒亮. 低温共固化高阻尼复合材料[J]. 航空学报, 2019, 40(8): 422721-422721.

ZHENG Changsheng, LIANG Sen, CHEN Jing, LIANG Hengliang. Low-temperature co-cured high damping composites[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(8): 422721-422721.

参考文献 22

[1]	沈观林, 胡更开. 复合材料力学[M]. 北京:清华大学出版社, 2006:1-8. SHEN G L, HU G K. Mechanics of composite materials[M]. Beijing:Tsinghua University Press, 2006:1-8(in Chinese).
[2]	梁森, 梁磊,米鹏. 嵌入式共固化复合材料阻尼结构的新进展[J]. 应用力学学报, 2010, 27(4):767-772. LIANG S, LIANG L, MI P. New development of damping structure of embedded co-cured composites[J]. Journal of Applied Mechanics, 2010, 27(4):767-772(in Chinese).
[3]	邓安仲, 李丰恺. 夹芯复合材料阻尼性能的研究进展[J]. 材料导报,2017,31(9):165-171. DENG A Z, LI F K. Research progress on damping property of sandwich composites[J]. Materials Review,2017,31(9):165-171(in Chinese).
[4]	GIBSON R F. A review of recent research on mechanics of multifunctional composite materials and structures[J].Composite Structures,2010,92(12):2793-2810.
[5]	AGNESE F, SCARPA F. Macro-composites with star-shaped inclusions for vibration damping in wind turbine blades[J]. Composite Structures, 2014, 108(1):978-986.
[6]	杜善义. 先进复合材料与航空航天[J]. 复合材料学报,2007, 24(1):1-12. DU S Y. Advanced composite materials and aerospace engineering[J]. Acta Materiae Compositae Sinica, 2007, 24(1):1-12(in Chinese).
[7]	赵云峰, 游少雄. 结构/阻尼一体化复合材料技术及其应用研究进展[J].材料工程,2012(11):86-91. ZHAO Y F,YOU S X. Review on the structure/damping cocured composite materials and their applications[J]. Journal of Materials Engineering, 2012(11):86-91(in Chinese).
[8]	PAN L J,ZHANG B M. Damping and mechanical properties of cocured composite laminates with embedded perforate viscoelastic layer[J]. Journal of Materials science and Technology,2009,25(4):543-546.
[9]	NI N N,WEN Y F, HE D L,et al.High damping and high stiffness CFRP composites with aramid non-woven fabric interlayers[J]. Composites Science & Technology, 2015, 117:92-99.
[10]	潘利剑. 粘弹阻尼层共固化复合材料的性能研究与优化设计[D].哈尔滨:哈尔滨工业大学,2009:55-70. PAN L J. Study of performance and optimum design of cocured composite laminates with embedded viscoelastic layer[D]. Harbin:Harbin Institute of Technology,2009:55-70(in Chinese).
[11]	FOTSING E R, MIRON F, EURY Y,et al.Bonding analysis of carbon/epoxy composites with viscoelastic acrylic adhesive[J]. Composites Part B:Engineering, 2012,43(5):2087-2093.
[12]	倪楠楠. 结构阻尼树脂基复合材料的结构与性能研究[D]. 杭州:浙江大学,2015:67-82. NI N N. Study of structures and properties of structural damping polymer matrix composites[D]. Hangzhou:Zhejiang University,2015:67-82(in Chinese).
[13]	林国兴, 丁亮,张明霞. 碳纤复合约束阻尼结构共固化成型及其性能研究[J]. 材料开发与应用,2017, 32(6):110-115. LIN G X,DING L,ZHANG M X. Study on co-cure processing and performance for carbon fibre composite constrained damping structure[J]. Development and Application of Materials,2017,32(6):110-115(in Chinese).
[14]	BIGGERSTAFF J M,KOSMATKA J B.Damping performance of co-cured graphite/epoxy composite laminates with embedded damping materials[J].Journal of Composites Materials,1999,33(15):1457-1469.
[15]	LIANG S,ZHANG Z S,MI P. Sound insulation characteristics of the embedded and co-cured composite damping structures[J]. Advanced Materials Research,2012, 487:598-602.
[16]	ZHANG S H, CHEN H L.A study on the damping characteristics of laminated composites with integral viscoelastic layers[J]. Composite Structures,2006,74(1):63-69.
[17]	SUZUKI K, KAGEYAMA K, KIMPARA I, et a1.Vibration and damping prediction of laminates with constrained viscoelastic layers-numerical analysis by a multilayer higher-order-deformable finite element and experimental observations[J]. Mechanics of Advanced Materials and Structures, 2003, 10(3):43-75.
[18]	张乾, 梁森,梁天锡. 嵌入式共固化耐高温阻尼复合材料制备及老化前后力学性能[J]. 航空学报,2015,36(7):2468-2474. ZHANG Q, LIANG S, LIANG T X. Manufacturing process and mechanical performance before and after aging treatment of embedded co-cured high-temperature-resistance damping composite[J]. Acta Aeronautica et Astronautica Sinica,2015, 36(7):2468-2474(in Chinese).
[19]	LIANG S,LIANG K Y,LUO L. Study on low-velocity impact of embedded and co-cured composite damping panels with numerical simulation method[J]. Composite Structures,2014, 107(1):1-10.
[20]	化学工业部沈阳橡胶研究设计院. 硫化橡胶或热塑性橡胶拉伸应力应变性能的测定:GB/T 528-2009[S]. 北京:中国标准出版社, 2009:12-14. Shenyang Rubber Research and Design Institute of Ministry of Chemical Industry. Rubber, vulcanized or thermoplastic determination of tensile stress-strain properties:GB/T 528-2009[S]. Beijing:Standard Press of China, 2009:12-14(in Chinese).
[21]	桦林佳通轮胎有限公司. 硫化橡胶或热塑性橡胶撕裂强度的测定(裤形、直角形和新月形试样):GB/T 529-2008[S]. 北京:中国标准出版社, 2008:23-25. Giti Hualin Tire Co. Ltd. Vulcanized or thermoplastic-determination of tear strength (Trouser, angle and crescent test pieces):GB/T 529-2008[S]. Beijing:Standard Press of China, 2008:23-25(in Chinese).
[22]	航空航天工业部七零三研究所. 黏弹性阻尼材料强迫非共振型动态测试方法:GJB 981-1990[S]. 北京:中国标准出版社,1990:14-17. Research Institute of Ministry of Aeronautics and Astronautics. Forced nonresonant dynamic testing method for viscoelastic damping materials:GJB 981-1990[S].Beijing:Standard Press of China,1990:14-17(in Chinese).

E-mail：hkxb@buaa.edu.cn

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低温共固化高阻尼复合材料

Low-temperature co-cured high damping composites

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