高活性铝粉的改性及在化学推进剂中燃烧团聚研究进展
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摘要
通过添加金属粉来提高化学火箭推进剂的能量性能已成为一种通用方法,但在实际应用中存在一系列利弊的两方面问题。研究了不同类型铝粉的活化和活性铝粉(包括球形μAl、包覆n Al、化学活化和机械活化铝粉)的特性,考察了其对推进剂燃烧性能的改善和聚集/团聚机理,并提出了提高铝粉燃烧效能的方法途径。结果表明,纳米铝粉不仅可显著提高推进剂的燃速,还可使推进剂的凝相燃烧产物(CCP)明显减少,从而减少两相流损失;活化Al尽管会降低Is,但其活性Al含量所产生的理论Is比n Al的高,尤其是机械活化铝粉。由于不同活化铝粉具有各自的优缺点,建议同时搭配使用两种不同类型的活化铝粉,以弥补单一铝粉的缺点。
Addition of metal,which acts as one of the most important energetic fuels,to the chemical rocket propellant can increase the energetic performance,while there are several advantages and disadvantages during the application in the solid and hybrid propulsion.The activation of aluminum powder and the characteristics of active aluminum(such as spherical μAl,coat n Al,mechanical and chemical active aluminum) were investigated.The improvement on the combustion performances of propellant and the aggregation/agglomeration mechanism of aluminum were conducted,new high-energy fuel with great prospects is also forecasted.The results shown that n Al can not only significantly increase the burning rate,but also significantly reduce the condensed combustion products(CCP) of propellants and reduce the two-phase flow loss.Although the activated Al decreases Is,the theoretical Is produced by its active Al content is higher than that of n Al,especially for mechanical activated aluminum powder.Moreover,the application of dual metal fuels mixture was introduced to the propellant formulation,which can cover the shortages of each type of Al fuel.
Addition of metal,which acts as one of the most important energetic fuels,to the chemical rocket propellant can increase the energetic performance,while there are several advantages and disadvantages during the application in the solid and hybrid propulsion.The activation of aluminum powder and the characteristics of active aluminum(such as spherical μAl,coat n Al,mechanical and chemical active aluminum) were investigated.The improvement on the combustion performances of propellant and the aggregation/agglomeration mechanism of aluminum were conducted,new high-energy fuel with great prospects is also forecasted.The results shown that n Al can not only significantly increase the burning rate,but also significantly reduce the condensed combustion products(CCP) of propellants and reduce the two-phase flow loss.Although the activated Al decreases Is,the theoretical Is produced by its active Al content is higher than that of n Al,especially for mechanical activated aluminum powder.Moreover,the application of dual metal fuels mixture was introduced to the propellant formulation,which can cover the shortages of each type of Al fuel.
引文
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