期刊文献+

高温载荷作用下金属蜂窝夹芯板结构的相变分析

Phase Change Analysis for Metal Honeycomb Sandwich Plate Structure Under High Temperature Load
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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,研究其在高温载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;外蒙皮在加载18 s后开始产生固液相变,外胶层11 s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. Based on heat transfer theory with phase change of muhilayer board, thermal analysis was imple- mented for metal honeycomb sandwich plate with finite element method ( FEM). The research of phase change problem under high temperature load was carried out. The computing results show that honeycomb sandwich plate has good heat insulation performance, the maximum temperature difference was more than 450 % be- tween the inside and outside surface; temperature field distribution in the honeycomb core layer is not com- pletely identical to the other four layers; it is different that each layer is influenced by the internal devices; the outer skin begins to form the solid-liquid phase change after loaded 18s, the outer glue starts to produce solid- liquid phase change after loaded 11 s, and has already large area of gas-liquid phase transition to 14s, damage area and damage degree are increased continuously. It has been better simulated with FEM that temperature field distribution laws, phase transition failure process temperature load. and its evolution of the complex structures under high
作者 纪占玲
出处 《郑州大学学报(工学版)》 CAS 北大核心 2013年第3期63-67,共5页 Journal of Zhengzhou University(Engineering Science)
基金 航空科学基金资助项目(2008ZC51028)
关键词 蜂窝芯 高温性能 有限元分析 热分析 相变分析 honeycomb high-temperature property finite element method (FEM) thermal analysis phasechange analysis
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参考文献8

  • 1FROSTIG 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.
  • 2Fan Xinyu,Li Yubin,Li Juan,Yan Chun,Li Ke.Modeling of Heat Conduction in Thermoplastic Honeycomb Core/Face Sheet Fusion Bonding[J].Chinese Journal of Aeronautics,2009,22(6):685-690. 被引量:3
  • 3FELI S, Namdari Pour M H. An analytical model forcomposite sandwich panels with honeycomb core sub- jected to high-velocity impact [ J]. Composites: Part B, 2012, 43(5) : 2439 -2447.
  • 4CRUMP D A, DULIEU-BARTON J M. Assessment of non-adiabatic behaviour in thermoelastic stress analysis of composite sandwich panels [ J]. Experimental Me- chanics, 2012, 52 (2): 829-842.
  • 5吴大方,郑力铭,潘兵,王岳武,孙冰,牟朦.非线性热环境下高温合金蜂窝板隔热性能研究[J].力学学报,2012,44(2):297-307. 被引量:18
  • 6张秋慧,冯国英,韩敬华,贾俊,杨李茗,朱启华,谢旭东.多脉冲激光对K9玻璃的表面损伤实验研究[J].强激光与粒子束,2008,20(1):62-66. 被引量:8
  • 7HASSE C, GRENET M, BONTEMPSC Andre, et al. Realization, test and modeling of honeycomb wall- boards containing a phase change material [ J]. Ener- gy and Buildings, 2011, 43(1) : 232 -238.
  • 8AGYENIM F, HEWITT N, EAMES P, et al. A re- view of materials, heat transfer and phase change prob- lem formulation for latent heat thermal energy storage systems (LHTESS) [ J ]. Renewable and Sustainable Energy Reviews, 2010,14 (2): 615-628.

二级参考文献46

  • 1郭少锋,陆启生,邓少永,黎全,汪晓波.ns脉冲激光对K9玻璃的破坏实验[J].强激光与粒子束,2004,16(7):817-820. 被引量:11
  • 2王涛,赵元安,黄建兵,贺洪波,劭建达,范正修.重复率激光作用下光学薄膜损伤的累积效应[J].强激光与粒子束,2005,17(B04):171-174. 被引量:11
  • 3解维华,张博明,杜善义.金属蜂窝结构有效热导率的预报与实验研究[J].哈尔滨工业大学学报,2007,39(5):787-789. 被引量:11
  • 4Trende A, Astrom B T, Woginger A, et al. Modelling of heat transfer in thermoplastic composites manufacturing: double-belt press lamination. Composites Part A 1999; 30(8): 935-943.
  • 5Trende A, Astrom B T. Heat transfer in compression molding of thermoplastic composite laminates and sandwich panels. Journal of Thermoplastic Composite Materials 2002; 15(1): 43-63.
  • 6Akermo M, Astrom B T. Modeling compression molding of all-thermoplastic honeycomb core sandwich components. Part A: model development. Polymer Composites 2000; 21(2): 245-256.
  • 7Akermo M, Astrom B T. Modeling compression molding of all-thermoplastic honeycomb core sandwich components. Part B: model verification. Polymer Composites 2000; 21 (2): 257-267.
  • 8Suratno B R, Ye L, Mai Y W. Simulation of temperature and curing profiles in pultruded composite rods. Composites Science and Technology 1998; 58(2): 191- 197.
  • 9Joshi S C, Lain Y C. Three-dimensional finite-element/ nodal-control-volume simulation of the pultrusion process with temperature-dependent material properties including resin shrinkage. Composites Science and Technology 2001; 61(11): 1539-1547.
  • 10Joshi S C, Lam Y C, Win T U. Improved cure optimization in pultrusion with pre-heating and die-cooler temperature. Composites Part A 2003; 34(12): 1151- 1159.

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