超燃冲压发动机控制问题研究  

Research of Scramjet Engine Control Problems

作　　者：杜宪 段楠 马松[2] 王珂[1] DU Xian DUAN Nan MA Song WANG Ke(School of Control Science and Engineering, Dalian University of Technology, Dalian 116024, China Shenyang Aircraft Design ＆ Research Institute, Shenyang 110035, China)

机构地区：[1]大连理工大学控制工程与科学学院,辽宁大连116024 [2]沈阳飞机设计研究所,辽宁沈阳110035

出　　处：《飞机设计》2017年第3期14-18,共5页Aircraft Design

摘　　要：介绍了超燃冲压发动机及其发展现状,重点总结了其现阶段在控制方面存在的一些问题。对超燃冲压发动机在模态转换控制、进气道控制以及燃油冷却系统控制3个方面的关键问题进行了分析。最后,根据其工作要求及工作环境,指出了其控制系统研究方向及研究重点。The scramjet engine and its development status are introduced, as well as key issues about scramjet engine control. Three aspects about scramjet engine control are analyzed in detail, including modal conversion control, inlet control and fuel cooling system control. Finally, according to work environment and requirements of scramjet engine, research direction and research priorities about scramjet engine control system are presented.

关 键 词：超燃冲压发动机 模态转换控制 进气道控制 燃油冷却系统控制 

分 类 号：V231[航空宇航科学与技术—航空宇航推进理论与工程] V228.7