胶接与钎焊铝蜂窝板力学性能研究

doi:10.11896/cldb.21070282

材料导报

2022, Vol. 36

Issue (23): 21070282-6 https://doi.org/10.11896/cldb.21070282

金属与金属基复合材料

胶接与钎焊铝蜂窝板力学性能研究

王文权¹, 王苏煜¹, 徐宇欣¹, 张新戈^1,*, 毕英超¹, 石磊²

1 吉林大学材料科学与工程学院,长春 130025
2 浙江亚通焊材有限公司,杭州 310030

Mechanical Properties of Glued and Brazed Aluminum Honeycomb Panel

WANG Wenquan¹, WANG Suyu¹, XU Yuxin¹, ZHANG Xinge^1,*, BI Yingchao¹, SHI Lei²

1 School of Materials Science and Engineering,Jilin University,Changchun 130025,China
2 Zhejiang Asia General Soldering & Brazing Material Co., Ltd.,Hangzhou 310030,China

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摘要蜂窝板是一种起源于天然蜂巢的仿生复合材料,其中,铝蜂窝板作为一种优异的轻质高强结构,广泛应用于轨道交通与航空航天领域,如舱壁、机翼与卫星整流罩等。铝蜂窝板由铝合金面板与蜂窝芯层复合而成,因此研究面板与芯层的高效连接工艺势在必行。胶接铝蜂窝板在使用过程中易产生空鼓、起包、胶接面失效等缺陷,且蜂窝板各项性能均受到了胶黏剂性能的限制。使用钎焊铝蜂窝板替代胶接铝蜂窝饭可以更好地发挥蜂窝结构的性能优势。本研究对比了相同尺寸规格下胶接与钎焊铝蜂窝板的平压、剪切和滚筒剥离性能及失效形式的差异,为不同工况条件下铝蜂窝板复合结构的连接工艺与失效研究提供了理论指导。

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关键词: 铝蜂窝板胶接钎焊力学性能失效形式

Abstract: Honeycomb panel is a kind of bionic composite material originated from natural honeycomb nests. As an excellent light-weight and high-strength structure, aluminum honeycomb panel has been widely used in transportation and aerospace applications,such as bulkheads, wings and satellite fairings, etc. Aluminum honeycomb panels consist of aluminum alloy skins and honeycomb core, which are bonded together to form sandwich structures, and the efficient bonding technique has become key issue. The glued aluminum honeycomb panel is prone to failure of the glued surface during engineering operation, resulting in defects such as hollowing and bagging, and mechanical properties of the honeycomb panel are limited to the performance of the adhesive. Adopting brazed aluminum honeycomb panels instead of glued aluminum honeycomb is a way to better play the superiority of honeycomb structure. This study compared the mechanical properties of axial compression, shear and roller peeling as well as the failure modes of glued and brazed aluminum honeycomb panel specimens at the same size. This research can provide a theoretical guidance for the bonding technique and failure analysis of aluminum honeycomb composite structures under different working conditions.

Key words: aluminum honeycomb panel glued brazed mechanical properties failure mechanism

发布日期: 2022-12-09

ZTFLH:	TG454
	TG495
	TB331

基金资助: 吉林省科技发展计划项目( 20200401034GX);吉林省发改委产业技术研究与开发专项(2020C029-1)

通讯作者: ^*zhangxinge@jlu.edu.cn

作者简介: 王文权,1994年获得吉林工业大学学士学位,2001年获得吉林大学硕士学位,2005年获得吉林大学工学博士学位,现任吉林大学材料科学与工程学院教授、博士研究生导师。长期从事材料连接和材料表面改性领域的教学和科研工作。2010—2012年在长春轨道客车股份有限公司博士后工作站工作,2009 年在德国亚琛大学表面工程研究所任访问学者,2007年在韩国釜山国立大学材料连接实验室任访问学者。发表了SCI/EI检索论文50余篇,负责完成科研项目20余项,授权发明专利10余项。
张新戈,2004年获得吉林大学学士学位,2006年获得哈尔滨工业大学硕士学位,2011年获得哈尔滨工业大学博士学位,现任吉林大学材料科学与工程学院副教授、博士研究生导师,长期从事新材料连接和增材制造领域的教学和科研工作。发表了SCI/EI检索论文30余篇,授权发明专利5项。

引用本文:

王文权, 王苏煜, 徐宇欣, 张新戈, 毕英超, 石磊. 胶接与钎焊铝蜂窝板力学性能研究[J]. 材料导报, 2022, 36(23): 21070282-6.
WANG Wenquan, WANG Suyu, XU Yuxin, ZHANG Xinge, BI Yingchao, SHI Lei. Mechanical Properties of Glued and Brazed Aluminum Honeycomb Panel. Materials Reports, 2022, 36(23): 21070282-6.

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http://www.mater-rep.com/CN/10.11896/cldb.21070282 或 http://www.mater-rep.com/CN/Y2022/V36/I23/21070282

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