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涡轮基变循环组合动力控制技术发展分析
李凌蔚1,吴宋伟2,张天宏1,嵇润民1
1.南京航空航天大学 能源与动力学院,江苏 南京 210016;2.中国航发控制系统研究所,江苏 无锡 214063
摘要:
基于现有文献梳理分析涡轮基变循环组合发动机控制技术的发展现状。介绍了涡轮基变循环组合发动机的发展历史和结构特点,提炼出其控制系统设计的关键技术;分别围绕飞/推一体化综合建模技术、模态切换控制技术以及飞/推一体化协同控制技术三个关键技术问题进行文献分析;基于国内空天动力需求及研究现状,提出对涡轮基变循环组合发动机控制技术的未来发展思考。
关键词:  空天飞行器  涡轮基变循环组合发动机  控制技术  飞/推一体化  模态切换  综述
DOI:10.13675/j.cnki.tjjs.2203092
分类号:V236
基金项目:江苏省科研与实践创新计划(KYCX21_0229)。
Development Analysis of Turbine-Based Variable Cycle Combined Power Control Technology
LI Ling-wei1, WU Song-wei2, ZHANG Tian-hong1, JI Run-min1
1.College of Energy and Power,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;2.AECC Aero Engine Control System Institute,Wuxi 214063,China
Abstract:
Based on the analysis of the existing literature, this paper summarizes the research status of turbine-based variable cycle combined (TBVCC) engine control technology. Firstly, the development history and structural characteristics of TBVCC engine are introduced, and the key technologies of control system design are extracted. Then, the three key problems of aircraft/propulsion integration modeling technology, mode switching control technology and aircraft/propulsion integration cooperative control technology are analyzed respectively. Finally, based on the domestic aerospace power demand and research status, the future investigation of control technology for TBVCC engine is put forward.
Key words:  Space vehicle  Turbine-based variable cycle combined engine  Control technology  Aircraft/propulsion integration  Mode switching  Review