采用整机试验的方法,对某型涡轮喷气式发动机从低转速到高转速状态下的燃烧室出口温度进行了测量.结果表明:该折流燃烧室在发动机低转速下性能较差,但各项性能参数随着发动机转速的增加而上升.在发动机设计点状态下,该折流燃烧室各项指标基本符合设计要求,其出口温度分布系数小于0.31,燃烧效率可达98.1%. The whole engine test was used to measure the outlet temperature of a certain type of turbojet engine from low speed to high speed.The results show that the baffled combustion chamber has poor performance at low engine speed, The performance parameters of the bifurcated combustor increase with the increase of the engine speed.At the engine design point, the indexes of the baffling combustion chamber basically meet the design requirements, the outlet temperature distribution coefficient is less than 0.31 and the combustion efficiency can reach 98.1%.