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2. Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing 100095, China
3. Key Laboratory of Aeronautical Materials Testing and Evaluation Aero Engine Corporation of China, Beijing 100095, China, fund=null, authors=ZHANG Qin1,2,3 , WANG Yana1 , YANG Yang1,2,3 , HE Yuhuai1,2,3 , CHEN Xinwen1,2,3 , authorsList=ZHANG Qin, WANG Yana, YANG Yang, HE Yuhuai, CHEN Xinwen), CN=ArticleExt(id=1242140453391381257, articleId=1242140450962879225, tenantId=1146029695717560320, journalId=1146031591421210625, language=CN, title=采用不同金属材料铆接修补碳纤维复合材料板的性能对比, columnId=1242140444671423178, journalTitle=科技导报, columnName=专题:航空复合材料技术, runingTitle=null, highlight=null, articleAbstract=随着复合材料在主承力结构上的应用,复合材料修理技术已经成为复合材料服役周期内的重要一环,其中利用金属的铆接修补方法在快速修补技术中具有重要应用。采用中心挖跑道形孔法模拟碳纤维复合材料损伤,分别使用不锈钢板与钛合金板对复合材料损伤件进行铆钉修补,对损伤件和两种修补件进行轴向拉伸试验,并采用应变计监测复合材料孔边及金属板中心应变。试验结果表明:采用不锈钢和钛合金与复合材料损伤件以铆接方式得到的修补件可承受的最大载荷相同,与未修补的相比提升了65.2%,说明对复合材料损伤板使用金属材料铆接修补具有一定补强效果,并且与使用不锈钢和钛合金材料进行修补的效果相当;在修补件拉伸过程中,碳纤维复合材料先于修补用金属材料失效;2种金属铆接修补件的破坏应变比无修补的损伤件的破坏应变略有增加但影响不大。, correspAuthors=null, authorNote=张琴,助理工程师,研究方向为复合材料力学性能,电子信箱:zhangqin621@126.com, correspAuthorsNote=null, copyrightStatement=null, copyrightOwner=null, extLink=null, articleAbsUrl=null, sourceXml=null, magXml=null, pdfUrl=null, pdf=8UeMOriHRuRKnc3X8Rb+iA==, pdfFileSize=2592295, pdfExtLink=null, richHtmlUrl=null, mobilePdfUrl=null, reviewReport=null, pdfFirstPage=null, abstractGraph=null, abstractGraphContent=null, abstractVideo=null, citation=null, cebUrl=null, magXmlContent=null, mapNumber=null, authorCompany=1. 中国航发北京航空材料研究院检测研究中心,北京 100095
2. 航空材料检测与评价北京市重点实验室,北京 100095
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科技导报
| 专题:航空复合材料技术 2023, 41(9): 67-74
采用不同金属材料铆接修补碳纤维复合材料板的性能对比
全屏
张琴1,2,3 ,王雅娜1 ,杨洋1,2,3 ,何玉怀1,2,3 ,陈新文1,2,3
作者信息
1. 中国航发北京航空材料研究院检测研究中心,北京 100095
2. 航空材料检测与评价北京市重点实验室,北京 100095
3. 中国航空发动机集团材料检测与评价重点实验室,北京 100095
Tensile performance of carbon fiber reinforced composite repaired with different metal plate using riveted joints
Affiliations
出版时间: 2023-05-13
doi: 10.3981/j.issn.1000-7857.2023.09.008
文章导航
随着复合材料在主承力结构上的应用,复合材料修理技术已经成为复合材料服役周期内的重要一环,其中利用金属的铆接修补方法在快速修补技术中具有重要应用。采用中心挖跑道形孔法模拟碳纤维复合材料损伤,分别使用不锈钢板与钛合金板对复合材料损伤件进行铆钉修补,对损伤件和两种修补件进行轴向拉伸试验,并采用应变计监测复合材料孔边及金属板中心应变。试验结果表明:采用不锈钢和钛合金与复合材料损伤件以铆接方式得到的修补件可承受的最大载荷相同,与未修补的相比提升了65.2%,说明对复合材料损伤板使用金属材料铆接修补具有一定补强效果,并且与使用不锈钢和钛合金材料进行修补的效果相当;在修补件拉伸过程中,碳纤维复合材料先于修补用金属材料失效;2种金属铆接修补件的破坏应变比无修补的损伤件的破坏应变略有增加但影响不大。
复合材料
/
铆接修补
/
不锈钢
/
钛合金
/
拉伸
With the application of composites in the main load-bearing structure, composite repair technology has become an important part of the service life of composites. The riveting repair method has an important application in rapid repair technology. In this study damage of carbon fiber composite materials was simulated by the central digging runway-shaped hole method, then the stainless steel plate and titanium alloy plate were used to rivet the damaged parts of the composites. The axial tensile tests of the damaged specimen and the two repair parts were carried out, in which a strain gauge was used to monitor the strains of the hole edge and the metal plate center. The test results show that the maximum loads of the repaired parts obtained by riveting the damaged parts of stainless steel, titanium alloy, and composite are the same, which are increased by 65.2% the unrepaired specimen, indicating that the use of metal materials riveting repair has a certain enhancement effect on the bearing capacity of the damaged composite plates and that the repair effects of stainless steel and titanium alloy materials are comparable. In the tensiling process of the repair specimen, the carbon fiber reinforced composite fails before the metal material; the failure strains of the two metal riveted repair parts are only slightly increased as compared to those of the unrepaired ones.
composites
/
riveting repair
/
stainless steel
/
titanium alloy
/
tensile
张琴,王雅娜,杨洋,何玉怀,陈新文.
采用不同金属材料铆接修补碳纤维复合材料板的性能对比.
科技导报,
2023
, 41
(9)
: 67
-74
.
DOI: 10.3981/j.issn.1000-7857.2023.09.008
ZHANG Qin, WANG Yana, YANG Yang, HE Yuhuai, CHEN Xinwen.
Tensile performance of carbon fiber reinforced composite repaired with different metal plate using riveted joints[J].
Science & Technology Review ,
2023
, 41
(9)
: 67
-74
.
DOI: 10.3981/j.issn.1000-7857.2023.09.008
2023年第41卷第9期
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文章信息
doi: 10.3981/j.issn.1000-7857.2023.09.008
接收时间:2023-01-13
首发时间:2023-06-01
出版时间:2023-05-13
收稿日期:2023-01-13
修回日期:2023-04-13
https://castjournals.cast.org.cn/joweb/kjdb/CN/10.3981/j.issn.1000-7857.2023.09.008
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2种不同金属材料的力学参数
科 Family 属数 Number of genus 种数 Number of species 占总种数比例 Percentage of total species (%) 属 Genus 种数 Number of species 占总种数比例 Percentage of total species (%) 鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78 小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39 多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39 红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87 小菇属 Mycena 11 5.26 光柄菇属 Pluteus 5 2.39 红菇属 Russula 17 8.13 栓菌属 Trametes 5 2.39
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