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空天防御  2025, Vol. 8 Issue (4): 27-37    
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连续旋转爆震发动机发展现状及使用前景
陈铮1, 李晓龙2, 徐广川3, 赵文文1, 杜溢华1, 殷玮1, 马虎3
1. 上海机电工程研究所,上海 201109; 2. 上海航天技术研究院,上海 201109; 3. 南京理工大学 机械工程学院 特种动力技术教育部重点实验室,江苏 南京 210094
Development Status and Application Prospect of Continuous Rotating Detonation Engine
CHEN Zheng1, LI Xiaolong2, XU Guangchuan3, ZHAO Wenwen1,DU Yihua1, YIN Wei1, MA Hu3
1. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China; 2. Shanghai Academy of Spaceflight Technology, Shanghai 201109, China; 3. School of Mechanical Engineering, Key Laboratory of Special Engine Technology, Ministry of Education, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China
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摘要 连续旋转爆震燃烧技术以其高效、安全、环保单次起爆即可持续燃烧等优点逐渐受到世界各国的关注,被视为具有变革性的航空航天推进技术;首先,从旋转爆震发动机的动力技术优势、爆震机理及应用方向进行简要梳理;其次,对使用连续爆轰模式的冲压发动机、火箭发动机及燃气涡轮发动机近年来的关键研究进展进行综述;最后,总结连续爆轰燃烧发动机工程应用面临的关键问题,并对旋转爆震发动机未来发展方向作出展望。
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关键词 爆震燃烧燃烧效率巡航导弹传播模态燃料比冲    
Abstract:Continuous rotating detonation combustion, which is characterized by high efficiency, safety, and environmental friendliness, and is capable of sustaining combustion with a single ignition, has gradually attracted the attention worldwide and is considered a revolutionary aerospace propulsion technology. In this paper, firstly, the power technology advantages, detonation mechanism, and application directions of rotating detonation engines were systematically reviewed. Then, the key research progress in recent years on ramjet engines, rocket engines, and gas turbine engines that use continuous detonation mode was summarized. Finally, the key issues faced in the engineering application of continuous detonation combustion engines were studied, and the future development trend was projected.
Key wordsdetonation combustion    combustion efficiency    cruise missile    propagation mode    specific impulse of fuel
收稿日期: 2025-05-15      出版日期: 2025-09-09
ZTFLH:  V 23  
基金资助:国家自然科学基金项目(12072163, 52106161, 12302434);国防科技重点实验室基金项目(2023LB013003)
作者简介: 陈铮(1983—),男,硕士,高级工程师。
引用本文:   
陈铮, 李晓龙, 徐广川, 赵文文, 杜溢华, 殷玮, 马虎. 连续旋转爆震发动机发展现状及使用前景[J]. 空天防御, 2025, 8(4): 27-37.
CHEN Zheng, LI Xiaolong, XU Guangchuan, ZHAO Wenwen, DU Yihua, YIN Wei, MA Hu. Development Status and Application Prospect of Continuous Rotating Detonation Engine. Air & Space Defense, 2025, 8(4): 27-37.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2025/V8/I4/27

参考文献
[1] 刘杰, 陈海燕, 高璞, 梁壮. 美英法空袭叙利亚作战特点分析及防空装备发展启示[J]. 空天防御, 2018, 1(4): 78-84.
[2] 李晓龙, 张顺家, 李勇, 毕鹏, 尹航. 巡航导弹高度跟踪制导律研究[J]. 空天防御, 2018, 1(4): 29-36.
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