航空发动机控制系统及关键技术现状与展望  

Research Status and Prospect of Aeroengine Control Systems and Key Technologies

作　　者：高亚辉 倪烨斌 姜成平 王欢 卢俊杰 GAO Yahui;NI Yebin;JIANG Chengping;WANG Huan;LU Junjie(AECC Aero Engine Control System Institute,Wuxi 214000,China)

机构地区：[1]中国航发控制系统研究所,无锡214000

出　　处：《南京航空航天大学学报》2024年第4期577-596,共20页Journal of Nanjing University of Aeronautics & Astronautics

摘　　要：航空发动机控制系统是航空发动机的安全关键系统,对发动机在飞行全包线范围内安全可靠产生推力或功率至关重要。本文阐述了航空发动机控制系统的演进历程,对架构设计、控制律设计、故障诊断与状态监视设计三大系统级关键核心技术以及仿真使能技术的发展情况进行总结分析,并对工程可应用性进行探讨,最后对未来的发展方向和重点研究内容进行展望,为新一代航空发动机控制系统设计提供一定参考。The aeroengine control system is a safety-critical system for aeroengine,crucial for generating reliable thrust or power within the entire flight envelope of the engine.This paper presents the evolution of the aeroengine control system,summarizes and analyzes the development of three key system-level technologies,including architecture design,control law design,and fault diagnosis and condition monitoring design,as well as simulation enabling technologies.The discussion on the applicability of these technologies in engineering is then conducted.The prospects for future development directions and key research areas are finally explored,providing a valuable reference for the design of next generation aeroengine control systems.

关 键 词：航空发动机 控制系统 架构设计 控制律 故障诊断 状态监视 仿真 

分 类 号：V233.7[航空宇航科学与技术—航空宇航推进理论与工程]