Volume 32 Issue 1
Jan.  2017
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Quasistatic compression mechanical properties of EPDM material after pyrolysis.[J]. Journal of Aerospace Power, 2017, 32(1): 114-119. doi: 10.13224/j.cnki.jasp.2017.01.016
Citation: Quasistatic compression mechanical properties of EPDM material after pyrolysis.[J]. Journal of Aerospace Power, 2017, 32(1): 114-119. doi: 10.13224/j.cnki.jasp.2017.01.016

Quasistatic compression mechanical properties of EPDM material after pyrolysis.

doi: 10.13224/j.cnki.jasp.2017.01.016
  • Received Date: 2015-05-18
  • Publish Date: 2017-01-28
  • In order to study the pyrolysis process of ethylene propylene diene monomer (EPDM) insulation material and its compression mechanical behavior under high strain rate, the thermal stability of EPDM was analyzed by thermogravimetric analysis (TGA). Based on the TGA curve and the thermal degradation temperature, the resistance furnace was set at different temperatures to complete the pyrolysis test. And then quasistatic compression tests were conducted by the universal testing machine. Results showed that, the mechanical properties of EPDM can be divided into three stages, the stressstrain curves first decreased, then rose and last reduced with the increase of pyrolysis temperature. Phased models were used to give a good description of mechanical properties of EPDM material under different degrees of pyrolysis. The second order Polynomial hyperelastic model including temperature related items was built to predict the mechanical response of EPDM material after different pyrolysis temperatures. Compared with the test results, the compression models can be used to effectively describe the mechanical behaviors of EPDM material with good accuracy.

     

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  • [1]
    杨飒,何国强,李江,等.炭化层疏松/致密结构的三元乙丙烧蚀模型[J].航空动力学报,2012,27(5):1172-1178. YANG Sa,HE Guoqiang,LI Jiang,et al.EPDM ablation model considering of porous/compact structure of charring layer[J].Journal of Aerospace Power,2012,27(5):1172-1178.(in Chinese)
    [2]
    Song B,Chen W.Onedimensional dynamic compressive behavior of EPDM rubber[J].Journal of Engineering Materials and Technology,2003,125(3):294-301.
    [3]
    Jiang Y,Zhang X,He J,et al.Effect of polyphenylsilsesquioxane on the ablative and flameretardation properties of ethylene propylene diene monomer (EPDM) composite[J].Polymer Degradation and Stability,2011,96(5):949-954.
    [4]
    Dubey R,Chawla M,Siril P F,et al.Bimetallic nanocomposites of Mn with very high catalytic activity for burning rate enhancement of composite solid propellants[J].Thermochimica Acta,2013,572(43):30-38.
    [5]
    张涛,孙冰.固体火箭发动机绝热层温度场的有限元计算方法[J].航空动力学报,2009,24(6):1407-1412. ZHANG Tao,SUN Bing.Numerical computation of solid rocket motor insulation layer temperature by finite element method[J].Journal of Aerospace Power,2009,24(6):1407-1412.(in Chinese)
    [6]
    Kokan T S,Olds J R,Seitzman J M,et al.Characterizing highenergydensity propellants for space propulsion applications[J].Acta Astronautica,2009,65(7):967-986.
    [7]
    Natali M,Rallini M,Puglia D,et al.EPDM based heat shielding materials for solid rocket motors:a comparative study of different fibrous reinforcements[J].Polymer Degradation and Stability,2013,98(11):2131-2139.
    [8]
    刘洋,李江,何国强,等.颗粒冲刷条件下三元乙丙绝热材料烧蚀特性实验[J].推进技术,2010,31(5):612-617. LIU Yang,LI Jiang,HE Guoqiang,et al.Experiment on ablation characteristic of EPDM insulator under particles erosion condition[J].Journal of Propulsion Technology,2010,31(5):612-617.(in Chinese)
    [9]
    Jovanovi V,Samar ijaJovanovi S,BudinskiSimendi J,et al.Composites based on carbon black reinforced NBR/EPDM rubber blends[J].Composites:Part B Engineering,2013,45(1):333-340.
    [10]
    朱艳峰,刘锋,黄小清,等.橡胶材料的本构模型[J].橡胶工业,2006,53(2):119-125. ZHU Yanfeng,LIU Feng,HUANG Xiaoqing,et al.The constitutive model of rubber material[J].China Rubber Industry,2006,53(2):119-125.(in Chinese)
    [11]
    杨性坤,胡付欣.氯丁橡胶接枝甲基丙烯酸丁酯的热降解动力学[J].合成橡胶工业,2008,30(5):343-347. YANG Xingkun,HU Fuxin.Thermal degradation kinetics of chloroprene rubber grafting butyl methacrylate[J].China Synthetic Rubber Industry,2008,30(5):343-347.(in Chinese)
    [12]
    卢子兴,严寒冰,王建华.聚氨酯复合泡沫塑料的准静态压缩力学性能[J].中国塑料,2004,18(3):31-34. LU Zixing,YAN Hanbing,WANG Jianhua.Mechanical properties of polyurethane syntactic foams under quasistatic compression[J].China Plastics,2004,18(3):31-34.(in Chinese)
    [13]
    庞宝君,杨震琦,王立闻,等.橡胶材料的动态压缩性能及其应变率相关的本构模型[J].高压物理学报,2011,25(5):407-415. PANG Baojun,YANG Zhenqi,WANG Liwen,et al.Dynamic compression properties and constitutive model with strain rate effect of rubber material[J].Chinese Journal of High Pressure Physics,2011,25(5):407-415.(in Chinese)
    [14]
    蒋晶,许进升,陈雄,等.WJ9发动机涡轮转子叶片包容性研究[C]∥中国航空学会(直升机)第3届动力与传动学术讨论会论文集.北京:中国航空学会,2000:76-81.
    [15]
    李晓芳,杨晓翔.橡胶材料的超弹性本构模型[J].弹性体,2005,15(1):50-58. LI Xiaofang,YANG Xiaoxiang.A review of elastic constitutive model for rubber materials[J].China Elastomerics,2005,15(1):50-58.(in Chinese)
    [16]
    龚科家,危银涛,叶进雄.填充橡胶超弹性本构参数试验与应用[J].工程力学,2009,26(6):193-198. GONG Kejia,WEI Yintao,YE Jinxiong.Constitutive parametric experiment of tire rubber hyperelastic laws with application[J].Engineering Mechanics,2009,26(6):193-198.(in Chinese)
    [17]
    Wang X,Huang C,Zou B,et al.Dynamic behavior and a modified JohnsonCook constitutive model of inconel 718 at high strain rate and elevated temperature[J].Materials Science and Engineering:A,2013,580(37):385-390.
    [18]
    梁兴文,叶艳霞.混凝土结构非线性分析[M].北京:中国建筑工业出版社,2007.
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