中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Modeling of Heat Conduction in Thermoplastic Honeycomb Core/Face Sheet Fusion Bonding

文献类型:期刊论文

作者Fan XY ; Li YB ; Li J ; Yan C ; Li K
刊名Chinese Journal of Aeronautics
出版日期2009
期号22页码:685-690
关键词honeycomb structures heat conduction homogenization method welding
合作状况国内
中文摘要Honeycomb sandwich materials have been widely used in aerospace industry as secondary structural materials or interior panels.Recently the research of full thermoplastic honeycomb sandwich materials has been of interest due to their recyclability. In their production, they usually demand an adhesive-free process, namely fusion bonding, to connect thermoplastic honeycomb core and face sheets. It is a heat induced process where a parameter of temperature should be well controlled to guarantee the product quality. This article presents a mathematical model of heat conduction to analyze the transient temperature distribution from heating tools towards inner part of the core under fusion bonding conditions. In order to simplify the complexity of 3D honeycomb geometry, a homogenization method is used to obtain average thermal properties of the honeycomb along the major heat flux direction. The model is validated by comparing with the results of in-situ temperature measurement during fusion bonding. The presented model can also be applied to analyzing general out-of-plane heat conduction through honeycomb sandwich structures made from other materials.
收录类别SCI
语种英语
公开日期2010-01-18
源URL[http://ir.nimte.ac.cn/handle/174433/266]  
专题宁波材料技术与工程研究所_宁波所知识产出
推荐引用方式
GB/T 7714
Fan XY,Li YB,Li J,et al. Modeling of Heat Conduction in Thermoplastic Honeycomb Core/Face Sheet Fusion Bonding[J]. Chinese Journal of Aeronautics,2009(22):685-690.
APA Fan XY,Li YB,Li J,Yan C,&Li K.(2009).Modeling of Heat Conduction in Thermoplastic Honeycomb Core/Face Sheet Fusion Bonding.Chinese Journal of Aeronautics(22),685-690.
MLA Fan XY,et al."Modeling of Heat Conduction in Thermoplastic Honeycomb Core/Face Sheet Fusion Bonding".Chinese Journal of Aeronautics .22(2009):685-690.

入库方式: OAI收割

来源:宁波材料技术与工程研究所

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