采用红外隐身技术的涡扇发动机优化设计

M. Chen, H. Chen, H. Zhang, J. Luo
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引用次数: 0

摘要

为了获得红外隐身技术对涡扇发动机性能的最优解,建立了带后向红外辐射强度计算模块的涡扇发动机数学模型。分析了红外抑制措施对涡扇发动机性能的影响。基于多目标粒子群优化(MOPSO)算法,得到了改装红外辐射抑制模块的参考发动机巡航状态下性能的最优解;进一步,通过多设计点(mdp)概念,对涡扇发动机进行了热循环优化设计。结果表明,采用气膜冷却的整体式全屏蔽导杆具有理想的红外抑制效果。与改装了红外辐射抑制模块的参考发动机相比,经过循环优化设计的发动机可以获得更好的红外隐身性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Optimisation design of turbofan engine using infrared stealth technology
To obtain the optimal solution for the performance of the turbofan engine using infrared stealth technology, an engine mathematical model with a backward infrared radiation intensity calculation module was established. The effects of infrared suppression measures on the performance of turbofan engines were analysed. Based on the multi-objective particle swarm optimisation (MOPSO) algorithm, the optimal solution for the performance in the cruise state of the reference engine refitted with the infrared radiation suppression module was obtained; Further, through the multiple design points (MDPs) concept, the thermal cycle optimisation design of the turbofan engine was carried out. The results show that the integrated fully shielded guiding strut (IFSGS) with air film cooling had the ideal infrared suppression effect. Compared with the reference engine refitted with infrared radiation suppression module, the engine after cycle optimisation design could obtain better infrared stealth performance.
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