张小波1 ,白文涛 1 ,周文俊 2 ,任童2 ,彭孝天 3 ,冯诗愚 2.结构对耗氧型惰化系统中反应器性能的影响[J].航空发动机,2024,50(4):75-81
结构对耗氧型惰化系统中反应器性能的影响
Effect of Structure on the Performance of Reactor in Oxygen Consuming Inerting System
  
DOI:
中文关键词:  反应器  催化惰化  RP-3燃油  转化率  耗氧速率
英文关键词:reactor  catalytic inerting  RP-3 fuel  conversion rate  oxygen consumption rate
基金项目:国家自然科学基金委员会-中国民用航空局民航联合研究基金(U1933121)资助
作者单位
张小波1 ,白文涛 1 ,周文俊 2 ,任童2 ,彭孝天 3 ,冯诗愚 2 1.航空工业金城南京机电液压工程研究中心2.南京航空航天大学 航空学院:南京 210016 3.南京工业大学 机械与动力工程学院南京 211816 
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中文摘要:
      针对新型低温催化惰化系统中反应器存在的易飞温和转化率低的问题,基于FLUENT多孔介质模型,以用户自定义标 量(UDS)添加固相能量方程,以用户自定义函数(UDF)形式加入化学反应,建立了圆柱体、圆锥体及反圆锥体3种结构的反应器仿 真模型,并通过自建试验台对模型的正确性进行了验证。定义了转化率和耗氧速率2个性能指标,研究了反应器进口气体温度、 进口流量和RP-3燃油蒸气体积浓度对反应器性能的影响,分析了反应器的操作范围,并从流动速度的角度出发,比较了3种结构 反应器的性能差异。结果表明:进口气体的温度及RP-3燃油体积浓度的提高以及进口流量的减小可以促进反应的发生;反应器 的起燃温度为470 K;在相同条件下,3种结构反应器的转化率从高到低依次为圆锥体、圆柱体、反圆锥体,可操作温度范围差值为 8~10 K。
英文摘要:
      To solve the problems of thermal runaway and low conversion rate in the reactor of the novel low-temperature catalytic inerting system, based on the FLUENT porous media model, the solid-phase energy equation was added by UDS, and the chemical reaction was added by UDF, simulation models were developed for cylindrical, conical, and reverse conical reactor structures and their accuracy verified using a self-built experimental platform. Two performance indicators, the conversion rate and oxygen consumption rate were defined. The effects of the inlet gas temperature, inlet flow, and RP-3 fuel vapor concentration on the performance of the reactor were studied, the operating range of the reactor was analyzed, and the performance differences of the three structures were compared in terms of flow velocity. The results show that an increase in the temperature of the inlet gas and the volume concentration of RP-3 fuel, along with a decrease in the inlet flow rate, can promote the occurrence of the reaction. The ignition temperature of the reactor is 470 K. Under identical conditions, the conversion rates of the three types of reactors follow a descending order: conical, cylindrical, and anti-conical, with a differ? ence in operating temperature range of 8-10 K.
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