玻璃纤维增强型复合材料圆筒高温高压动态冲击断口形貌分析

王加刚; 余永刚; 周良梁; 曹韩学; 刘溪

doi:10.11883/1001-1455(2017)06-1107-06

玻璃纤维增强型复合材料圆筒高温高压动态冲击断口形貌分析

doi: 10.11883/1001-1455(2017)06-1107-06

王加刚^{1, 2},
余永刚^1, ,,
周良梁¹,
曹韩学³,
刘溪³

1.
南京理工大学能源与动力工程学院，江苏南京 210094
2.
重庆望江工业有限公司，重庆 400071
3.
重庆大学材料科学与工程学院，重庆 400044

详细信息

作者简介:
王加刚(1979—)，男，博士研究生

通讯作者:
余永刚, yyg801@njust.edu.cn

中图分类号: O346.1
计量
- 文章访问数: 4231
- HTML全文浏览量: 1267
- PDF下载量: 379
- 被引次数: 0
出版历程
- 收稿日期: 2016-08-11
- 修回日期: 2017-01-22
- 刊出日期: 2017-11-25

Fracture analysis of glass fiber reinforced composite material under high temperature and pressure

1.
School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China
2.
Chongqing Wangjiang Industry Co Ltd, Chongqing 400071, China
3.
College of Materials Science and Engineering, Chongqing University, Chongqing 400044, China

摘要

摘要: 为了探究埋头弹火炮所用的玻璃纤维增强型(GFR)复合材料药筒在高温高压瞬态冲击条件下的结构强度，分别开展了圆筒静态整体拉伸和动态高温高压冲击实验，从拉伸/瞬态超高压破坏试样断口部分截取断口样品，在扫描电子显微镜下观察断口形貌，得到GFR复合材料在两种不同受力情况下的失效模式。结果表明：室温整体单轴拉伸断裂时，GFR复合材料的断面与轴线夹角接近45°, 失效模式为环氧树脂基体破坏和纤维拔出；在高压瞬态冲击作用下，试样主要失效模式为纤维的脆性断裂，同时由于火药燃烧产生的高温燃气使部分环氧树脂基体碳化，纤维与基体界面结合力降低，少数纤维熔融或软化附着在断口上，部分软化的纤维因瞬态超高压被拉细。
- 玻璃纤维 /
- 复合材料 /
- 非金属药筒 /
- 瞬态冲击 /
- 断口形貌
Abstract: In this study we carried out an static overall tensile experiment at room temperature and a transient blast experiment under ultra high pressure to investigate the structural strength of glass fiber reinforced (GFR) composite cartridge of CTA gun with transient impulse under high temperature and pressure. The fracture surfaces of the specimens were cut from the tensile/transient ultra high pressure failure samples, and the fracture morphology was observed under the scanning electron micro scope. The results show that the main failure modes of GFR composites are matrix failure and fiber pulling-out when the uniaxial overall tensile fracture occurs at room temperature with the intersection between the GFR composites section and the axis close to 45°; the main failure mode of the specimen under transient ultra high pressure is the brittle fracture of the fiber and, due to the a portion of substrate's carbonization resulting from the high temperature heat produced by the ignited gun powder, the fiber matrix interface's binding force is reduced and a few fibers either melt or soften, becoming attached to the fractured surface, thereby attenuating part of the softened fibers due to the transient super high pressure.
- glass fiber /
- composite material /
- nonmetallic cartridge /
- transient blast experiment /
- fracture morphology

HTML全文

图 1 室温整体拉伸实验

Figure 1. Overall tensile experiment at ambient temperature

下载: 全尺寸图片幻灯片

图 2 高温高压瞬态冲击试样

Figure 2. Sample of transient ultrahigh pressure experiment

下载: 全尺寸图片幻灯片

图 3 高温高压瞬态冲击压力曲线

Figure 3. Pressure curve in thin-walled cylinder

下载: 全尺寸图片幻灯片

图 4 玻璃纤维增强型复合材料轴向拉伸断口

Figure 4. Fracture appearance of GFR composite material specime in overall tensile experiment

下载: 全尺寸图片幻灯片

图 5 室温单轴拉伸断口形貌

Figure 5. Uniaxial tensile fracture morphology at room temperature

下载: 全尺寸图片幻灯片

图 6 玻璃纤维增强型复合材料高压瞬态冲击断口

Figure 6. Fracture appearance of GFR composite material specimen in transient blast experiment

下载: 全尺寸图片幻灯片

图 7 高温高压瞬态冲击条件下的典型断口形貌

Figure 7. Observation of typical fracture surface morphology by SEM

下载: 全尺寸图片幻灯片

参考文献(19)

[1]	李晓琴, 张巨伟.纤维缠绕复合材料管道的应力分析[J].中国化工装备, 2008, 10(2):106-108. http://d.old.wanfangdata.com.cn/Periodical/syhgyy200804031 Li Xiaoqin, Zhang Juwei.Stress analysis of fiber reinforced polymer pipes[J].China Chemical Industry Equipment, 2008, 10(2):106-108. http://d.old.wanfangdata.com.cn/Periodical/syhgyy200804031
[2]	Guynn E G, Ochoa O O, Bradley W L.Aparametric study of variable that affect fiber microbuckling initiation in composite laminates:Analyses[J].Journal of Composite Materials, 1992, 26(11):1594-1616. doi: 10.1177/002199839202601103
[3]	Jumahat A, Soutis C, Jones F R, et al.Fracture mechanisms and failure analysis of carbon fiber/toughened epoxy composites subjected to compressive loading[J].Composite Structures, 2010, 92(2):295-305. doi: 10.1016/j.compstruct.2009.08.010
[4]	Miller A G, Wingert A L.Fracture surface characterization of commercial graphite/epoxy systems[M].Philadelphia PA:American Society for Testing and Materials, 1979:223-296.
[5]	Grove R A, Smith B W.Compendium of post-failure analysis techniques for composite materials[R].Seattle, WA: Boeing Military Aircraft Co, 1986.
[6]	Gary G, Zhao H.Dynamic testing of fibre polymer matrix composite plates under in-plane compression[J].Composites:A, 2000, 31(8):835-840. doi: 10.1016/S1359-835X(00)00026-9
[7]	王越, 张凤玲.玻璃纤维增强尼龙66拉伸/冲击断口分析[J].测控技术, 2011, 30(增刊):375-377. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=7595978 Wang Yue, Zhang Fengling.Fracture analysis of glass fiber reinforced nylon 66 under tensile impact test[J].Measurement & Control Technology, 2011, 30(suppl):375-377. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=7595978
[8]	牟善彬, 宋显辉, 苏小萍.玻璃纤维处理后复合材料强度的变化及微观特征[J].北京科技大学学报, 2001, 23(增刊):23-24. http://d.old.wanfangdata.com.cn/Conference/3207252 Mou Shanbin, Song Xianhui, Su Xiaoping.Strength variation and micro-characteristics of composites after the treatment of glass fibers[J].Journal of University of Science and Technology Beijing, 2001, 23(suppl):23-24. http://d.old.wanfangdata.com.cn/Conference/3207252
[9]	陈煊, 程礼, 陈卫, 等.二维C/SiC复合材料准静态和动态拉伸力学性能[J].复合材料学报, 2016, 33(12):2846-2853. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=fhclxb201612020 Chen Xuan, Cheng Li, Chen Wei, et al.Quasi-static and dynamic tensile mechanical properties of two dimensional C/SiC composites[J].Acta Materiae Compositae Sinica, 2016, 33(12):2846-2853. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=fhclxb201612020
[10]	严世成, 梁克瑞.玻璃钢/复合材料的发展、应用与展望[J].广东化工, 2014, 41(24):72-73. doi: 10.3969/j.issn.1007-1865.2014.24.038 Yan Shicheng, Liang Kerui.Development, application and Prospect of FRP/composite[J].Guangdong Chemical Industry, 2014, 41(24):72-73. doi: 10.3969/j.issn.1007-1865.2014.24.038
[11]	吴如艳, 陈凤舞.玻璃钢材料发展现状综述[J].河南科技, 2013(2):120, 127. http://d.old.wanfangdata.com.cn/Periodical/hnkj201304106
[12]	Chamis C C, Minnetyan L.Defect/damage tolerance of pressurized fiber composite shells[J].Composite Structure, 2001, 51(2):159-168. doi: 10.1016/S0263-8223(00)00141-0
[13]	Verijenko V E, Adalis L, Tabakov P Y.Stress distribution in continuously heterogeneous thick laminated pressure vessels[J].Composite Structures, 2001, 54(2):371-377. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CC0210302721
[14]	陈鹏万, 黄风雷.含能材料损伤理论及应用[M].北京:北京理工大学出版社, 2006:1-2.
[15]	刘政, 刘小梅.短纤维增强铝硅合金复合材料的组织与断口形貌分析[J].兵器材料科学与工程, 2002, 25(3):22-25. doi: 10.3969/j.issn.1004-244X.2002.03.008 Liu Zheng, Liu Xiaomei.Analysis on structure and fracture morphology of short fiber reinforced aluminum-silicon alloy composites[J].Ordnance Material Science and Engineering, 2002, 25(3):22-25. doi: 10.3969/j.issn.1004-244X.2002.03.008
[16]	张厚江, 陈五一, 陈鼎昌.碳纤维复合材料(CFRP)孔壁的微观形态[J].复合材料学报, 2000, 17(2):98-101. doi: 10.3321/j.issn:1000-3851.2000.02.022 Zhang Houjiang, Chen Wuyi, Chen Dingchang.Microstructure of the hole surface of CFRP[J].Acta Materiae Compositae Sinica, 2000, 17(2):98-101. doi: 10.3321/j.issn:1000-3851.2000.02.022
[17]	刘芳, 杨柳.纤维增强复合材料的冲击拉伸力学性能[J].纤维复合材料, 2004, 21(4):41-42. doi: 10.3969/j.issn.1003-6423.2004.04.012 Liu Fang, Yang Liu.The researches on fiber-reformed composites impact tensile performance[J].Fiber Composites, 2004, 21(4):41-42. doi: 10.3969/j.issn.1003-6423.2004.04.012
[18]	夏源明, 杨报昌, 贾德新, 等.摆锤式杆杆型冲击拉伸装置和低温动态测试技术[J].实验力学, 1989, 4(1):57-66. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CAS201303040000253173 Xia Yuanming, Yang Baochang, Jia Dexin, et al.Rod-type impact tensile test device of the pendulum bar and low temperature dynamic testing technology[J].Journal of Experimental Mechanics, 1989, 4(1):57-66. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=CAS201303040000253173
[19]	易法军, 梁军, 孟松鹤, 等.防热复合材料的烧蚀机理与模型研究[J].固体火箭技术, 2000, 23(4):48-56. http://d.old.wanfangdata.com.cn/Periodical/gthjjs200004012 Yi Fajun, Liang Jun, Meng Songhe, et al.Study on ablation mechanism and models of heatshield composites[J].Journal of Solid Rocket Technology, 2000, 23(4):48-56. http://d.old.wanfangdata.com.cn/Periodical/gthjjs200004012