吸气式斜爆轰发动机燃料掺混与燃烧组织技术研究进展  

Research Progress of Fuel Mixing and Combustion Organization Technology in Air-Breathing Oblique Detonation Engine

作　　者：尚甲豪 曹军伟[1,2,3] Shang Jiahao;Cao Junwei(China Airborne Missile Academy,Luoyang 471009,China;Collaborative Innovation Center for Future Airborne Weapon Technology,AVIC,Beijing 100029,China;Chinese Aeronautical Establishment,Beijing 100029,China)

机构地区：[1]中国空空导弹研究院,河南洛阳471009 [2]航空工业未来机载武器技术协同创新中心,北京100029 [3]中国航空研究院,北京100029

出　　处：《航空兵器》2025年第1期40-50,共11页Aero Weaponry

摘　　要：吸气式斜爆轰发动机采用驻定斜爆轰波组织燃烧,实现高马赫数来流中稳定燃烧与高效快速能量转化,具有作为高超声速吸气式动力的应用潜力与价值。本文梳理了近年来斜爆轰发动机燃料掺混与燃烧组织技术的研究进展,包括燃烧室流动控制、燃料敏化、燃料喷注技术等方面,并对斜爆轰发动机地面试验技术进行了补充介绍。最后,基于当前斜爆轰发动机燃料掺混与燃烧组织技术及其地面试验技术的研究现状,对未来技术发展方向进行了展望。The air-breathing oblique detonation engine(ODE)utilizing standing oblique detonation waves achieves stabilized combustion and highly efficient and rapid energy conversion in high Mach number flows.It holds significant potential and value as a propulsion system for hypersonic air-breathing applications.This paper reviews the recent advancements in the research of fuel mixing and combustion organization technology in ODE,including combustion chamber flow control,fuel sensitization,and fuel injection technologies.Additionally,it provides supplementary insights into the ground testing technology for ODE.Finally,based on the current status of fuel mixing and combustion organization technology and ground testing technology,this paper looks ahead to the future directions for technological development.

关 键 词：斜爆轰发动机 爆轰燃烧 超声速燃烧室 高超声速推进 燃料掺混 燃烧组织 

分 类 号：TJ760[兵器科学与技术—武器系统与运用工程] V231[航空宇航科学与技术—航空宇航推进理论与工程]