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纳米CuO的批量制备及其对高氯酸铵热分解性能的影响研究
郝嘎子1,刘 杰1,高 寒1,肖 磊1,姜 炜1,李凤生2,赵凤起2,高红旭2
(1. 南京理工大学 化工学院/国家特种超细粉体工程技术研究中心,江苏 南京 210094;2. 西安近代化学研究所 燃烧与爆炸技术重点实验室,陕西 西安 710065)
摘要:
采用HLG-5型纳米化粉碎机批量制备了纳米CuO。通过X射线衍射仪(XRD)、扫描电子显微镜(SEM)、透射电子显微镜(TEM)对CuO颗粒的结构、大小及形貌进行了表征,并采用差示扫描量热仪(DSC)分别研究了纳米CuO的含量为1%,1.5%,2%,2.5%,4%对不同粒度AP的热分解性能的影响。结果表明,制备的CuO颗粒大小约为17nm,为单斜晶系,呈类球形。2%含量的纳米CuO对AP具有更好的催化性能,可使64μm,6μm,1μm AP的高温分解峰分别降低83.0℃,81℃,55.4℃;表观分解热分别增加880J/g,617J/g,391J/g;反应速度常数提高数倍。
关键词:  纳米CuO  热分解  催化效果  固体火箭推进剂
DOI:
分类号:
基金项目:基础产品创新技术火炸药科研专项,国家自然科学基金(51206081)。
Batch Production of Nano-Sized CuO and Its Catalytic Effects on Thermal Decomposition of Ammonium Perchlorate
HAO Ga-zi1,LIU Jie1,GAO Han1,XIAO Lei1,JIANG Wei1,LI Feng-sheng2,ZHAO Feng-qi2,GAO Hong-xu2
(1. National Special Superfine Powder Engineering Research Center of China/School of Chemical Engineering,Nanjing University of Science and Technology,Nanjing 210094,China;2. Science and Technology on Combustion and Explosion Laboratory,Xi’an Modern Chemistry Research Institude,Xi’an 710065,China)
Abstract:
Nano-CuO have been successfully prepared in large-scale using the HLG-5 grinder. The microstructure,size and morphology of CuO particles were characterized by X-ray diffraction (XRD),scanning electron microscopy (SEM) and transmission electron microscopy (TEM). The catalytic effects of nano-CuO with mass fraction of 1%,1.5%,2%,2.5% and 4%,respectively,on thermal decomposition of AP with different size were investigated by DSC. The results show that nano-CuO could be indexed as pure monoclinic and have a semi-spherical morphology with a fairly uniform size of 17nm. Furthermore,the nano-CuO have the optimal catalytic effect at a mass fraction of 2%,and the peak values of high temperature decomposition of 64μm,6μm,and 1μm AP decreased by 83.0℃,81℃ and 55.4℃,respectively. The apparent thermal decomposition of 64μm,6μm,and 1μm AP increased by 880J/g,617J/g and 391J/g,respectively,and the reaction rate constant of AP also increased by several times.
Key words:  Nano-CuO  Thermal decomposition  Catalytic effects  Solid rocket propellants