Calculation of thermodynamical equilibrium composition of combustion gases

燃燒氣體의 熱力學的 平衡組成計算에 관한 硏究

A compute program based on the minimization of total Gibbs' free energy and enthalpy balance was developed to calculate the chemical equilibrium composition and adiabatic flame temperature, especially stressed on NO and CO concentration of Heavy oil. Twenty four components of combustion gases which would be produced from the combustion of Heavy oil were chosen and utilized for the products composition analysis of competing combustion reaction. As the results, following conclusions were turned out; (1) Maximum adiabatic flame temperature was found around to be 2900K, when the stoichiometric air ratio was 0.8. (2) Maximum NO quantity in adiabatic process was occurred when supplied air quantity was around 120% of theoretical air requirement. (3) NO and CO quantities were increased with combustion gas temperature at constant stoichiometric air ratio. (4) At constant temperature of combustion gas, NO quantity was increased and Co quantity was decreased with supplied air quantity.

본 논문에서는 연소기체의 열력학적 평형조성 계산을 위한 수식을 Gibbs의 자 유에너지 최소화법에 의하여 유도하고 이를 컴퓨터 프로그램화하여, Table 1의 특성을 지닌 연료에 대하여 ⅰ) 연소공기량에 따른 평형조성 및 단열불꽃온도, ⅱ) 연소온도 변화에 따른 평형조성의 변화를 계산함으로써 연소기체의 생성기구를 열력학적으로 해 석하였다.