CAJ | 학술논문

根据燃油箱气相空间中各气体组分混合特性，采用数值积分方法，在综合考虑油箱载油率、环境温度、燃油中气体溶解度、燃油蒸汽及富氮气体浓度等因素的条件下，建立油箱惰化数学模型，并通过相关文献中的实验数据验证了该模型的正确性。在此基础上，分别对飞机滑行－爬升和俯冲－下降阶段的惰化流量需求开展研究，并分析了载油率、富氮气体浓度、温度等因素对惰化流量需求的影响。本文的研究成果可为飞机油箱惰化系统设计提供理论支持。
근거연유상기상공간중각기체조분혼합특성，채용수치적분방법，재종합고필유상재유솔、배경온도、연유중기체용해도、연유증기급부담기체농도등인소적조건하，건립유상타화수학모형，병통과상관문헌중적실험수거험증료해모형적정학성。재차기출상，분별대비궤활행－파승화부충－하강계단적타화류량수구개전연구，병분석료재유솔、부담기체농도、온도등인소대타화류량수구적영향。본문적연구성과가위비궤유상타화계통설계제공이론지지。
According to the characteristics of gas-component mixing in fuel tank vapor space, and considering the influences of several factors such as fuel loading rate, environment temperature, gas solu-bility in fuel, fuel vapor and nitrogen-enriched gas concentration, a mathematical model of fuel tank iner-ting is established by using the numerical integration method.The correctness of the model is verified by the experimental data published in related literatures.On this basis, This paper researches on inerting flow requirements for aircraft taxiing -climb and subducting-descent stages, and analyzes the impact of fuel loading rate, nitrogen-enriched gas concentration, temperature and other factors on the inerting flow re-quirements.The study can provide theoretical support for design of the aircraft fuel tank inerting system.