Zhang Qingyu, Zhang Xinming, Hu Jing, Li Guowei
College of Mechanical and Electrical Engineering, Changchun University of Science and Technology, Changchun, 130022, China.
College of Control Science and Engineering, Bohai University, Jinzhou, 121013, China.
Sci Rep. 2025 Aug 20;15(1):30574. doi: 10.1038/s41598-025-15621-5.
This article focuses on optimizing the evaporation and atomization performance of the evaporator tube in the combustion chamber of a microturbine engine, and examines its impact on engine thrust. Given that the evaporator tube design is crucial for enhancing combustion efficiency as a key component of the combustion chamber, this study introduces an innovative evaporator tube structure that incorporates biomimetic design principles through theoretical exploration. The proposed structure adds specifically sized grooves to the inner wall of traditional evaporation tubes to improve the evaporation and atomization processes of fuel droplets. The effectiveness of this design is demonstrated by comparing and analyzing the differences in evaporation and atomization characteristics between traditional and biomimetic evaporation tubes. As the incoming air temperature increases, the diameter of fuel droplets decreases, while the evaporation rate significantly rises. Moreover, when the biomimetic tube's inner wall grooves are precisely designed with a width of 0.5 mm, a depth of 0.6 mm, and a length of 1.5 mm, the atomization effect of fuel droplets reaches its optimal state, significantly improving the evaporation rate compared to traditional evaporation tubes.
本文着重于优化微型涡轮发动机燃烧室中蒸发管的蒸发和雾化性能,并研究其对发动机推力的影响。鉴于蒸发管设计作为燃烧室的关键部件对提高燃烧效率至关重要,本研究通过理论探索引入了一种融合仿生设计原理的创新型蒸发管结构。所提出的结构在传统蒸发管的内壁添加特定尺寸的凹槽,以改善燃料液滴的蒸发和雾化过程。通过比较和分析传统蒸发管与仿生蒸发管在蒸发和雾化特性上的差异,证明了该设计的有效性。随着进气温度升高,燃料液滴直径减小,而蒸发速率显著提高。此外,当仿生管内壁凹槽精确设计为宽度0.5毫米、深度0.6毫米、长度1.5毫米时,燃料液滴的雾化效果达到最佳状态,与传统蒸发管相比,蒸发速率显著提高。