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驻涡燃烧室前钝体燃料喷射性能数值分析
引用本文:徐 啸,潘伟宸,吴维维. 驻涡燃烧室前钝体燃料喷射性能数值分析[J]. 航空发动机, 2023, 49(4): 115-121
作者姓名:徐 啸  潘伟宸  吴维维
作者单位:江苏科技大学 能源与动力工程学院,江苏镇江 212000
基金项目:国家自然科学基金(51506079)资助
摘    要:为研究驻涡燃烧室在前钝体燃料喷射状况下的燃烧性能,采用3维数值仿真模拟方法,对驻涡燃烧室前钝体燃料喷射状况下的燃烧效率及燃烧室性能与无前钝体燃料喷射状况下的燃烧性能进行了对比分析,并对驻涡燃烧室的冷流以及燃烧状态下的燃烧室性能进行了系统研究。燃烧室温度分布表明:前钝体顶部燃料喷射在0.2~0.7的喷射系数范围内,缩短了燃烧室火焰长度,提高了燃烧室在相同轴向长度下的燃烧效率,使燃烧室更加紧凑;驻涡燃烧室前钝体顶部燃料喷射孔的孔径在一定范围内的变化对燃烧室的燃烧效率、出口温度分布系数以及总压损失影响较小。

关 键 词:驻涡燃烧室;前钝体燃料喷射;燃烧效率;出口温度分布;数值分析;航空发动机

Numerical Analysis of Trapped Vortex Combustor Performance Under Front Bluff Body Fuel Injection
XU Xiao PAN Wei-chen WU Wei-wei. Numerical Analysis of Trapped Vortex Combustor Performance Under Front Bluff Body Fuel Injection[J]. Aeroengine, 2023, 49(4): 115-121
Authors:XU Xiao PAN Wei-chen WU Wei-wei
Abstract:In order to study the combustion performance of a trapped vortex combustor (TVC) under the condition of front bluff body fu-el injection, comparative analyses were conducted on the combustion efficiency and the combustion performance of the TVC under condi-tions with and without front bluff body fuel injection using three-dimensional numerical simulation. The TVC performances under non-re-acting and reacting flow were systematically examined. The results of combustor temperature distribution show that the fuel injection fromthe top of the front bluff body with an injection coefficient in the range of 0.2-0.7 leads to a decreased flame length in the combustion cham-ber, improves the combustion efficiency at the same axial length of the combustion chamber and makes combustion chamber more compact.The variation of the diameter of the fuel injection orifice at the top of the front bluff body of the TVC within a certain range has little influ-ence on combustion efficiency, outlet temperature distribution coefficient, and total pressure loss of the combustion chamber.
Keywords:Trapped Vortex Combustor   front bluff body fuel injection   combustion efficiency   outlet temperature distribution   numerical analysis   aeroengine
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