[1]纪占玲..高温载荷作用下金属蜂窝夹芯板结构的相变分析[J].郑州大学学报(工学版),2013,34(03):63-67.[doi:10.3969/j.issn.1671-6833.2013.03.016]
　JI Zhan-ling.Phase Change Analysis for Metal Honeycomb Sandwich PlateStructure Under High Temperature Load[J].Journal of Zhengzhou University (Engineering Science),2013,34(03):63-67.[doi:10.3969/j.issn.1671-6833.2013.03.016]
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高温载荷作用下金属蜂窝夹芯板结构的相变分析()
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《郑州大学学报(工学版)》[ISSN:1671-6833/CN:41-1339/T]

卷:
34卷
期数:
2013年03期
页码:
63-67
栏目:
出版日期:
2013-05-31

文章信息/Info

Title:
Phase Change Analysis for Metal Honeycomb Sandwich PlateStructure Under High Temperature Load
作者:
纪占玲.
华北水利水电学院机械学院,河南郑州450011;北京航空航天大学自动化科学与电气工程学院,北京100191
Author(s):
JI Zhan-ling1; 2
1.Sechool of Mechanical Engineering，North China University of Water Resourees and Electric Power, Zhengzhou 450011, Chi-na; 2.School of Automation Seience and Electrical Engineering，Beihang University，Beijing 100191，China
关键词:
蜂窝芯;  高温性能;  有限元分析;  热分析;  相变分析
Keywords:
honeycomb;  high-temperature property ;  finite element method ( FEM) ;  thermal analysis;  phasechange analysis
分类号:
TB333；TKl23
DOI:
10.3969/j.issn.1671-6833.2013.03.016
文献标志码:
A
摘要:
以含相变的多层板热传递理论为依据,采用有限单元法对金属蜂窝夹芯板进行了热分析,研究其在高温栽荷作用下的相变问题,计算结果表明,蜂窝夹芯板具有良好的隔热性能,内外表面间最大温差超过450℃；蜂窝芯温度场分布与其余四层不完全相同；各层板受内部设备的影响不同；外蒙皮在加栽18 s后开始产生固液相变,外胶层11s后开始产生固液相变,到14 s时已产生大面积气液相变,损伤面积和损伤程度不断增加,有限单元法较好地模拟了复杂结构在高温载荷作用下的温度场分布、相变失效过程及其演化规律.
Abstract:
Based on heat transfer theory with phase change of multilayer board，thermal analysis was imple-mented for metal honeycomb sandwich plate with finite element method ( FEM).The research of phase changeproblem undexr high temperafure load was carried out.The computing results show that honeycomb sandwichplate has good heat insulation performance， the maximum tcmperature difference was more than 450 ℃ bc-tween the inside and outside surface;temperature field distribution in the honeyeomb core layer is not com-pletely identical to the other four layers ; it is different that each layer is influenced by the internal devices ; theouter skin begins to form the solid-liquid phase change after loaded 18s，the outer glue starts to produce solidliquid phase change aiter loaded 11s , and has already large area of gas-liquid phase transition to 14s , damagearea and damage degree are increased continuously. It has been better simulated with FEM that temperatureficld distribution laws，phasc transition failure process and its cvolution of thc complcx strucetures under hightemperature load.

参考文献/References:

[1]FROSTIG Y，THOMSEN O T. Non-linear thermal re-sponse of sandwich panels with a flexible core and tem-perature dependent mechanical properties [ J]. Inter-national Journal of Solids and Structures，2011 , 48( 14/15): 2218 - 2237.

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更新日期/Last Update: 1900-01-01