航空学报2025，Vol.46Issue(16)：152-169,18.DOI:10.7527/S1000-6893.2024.31624
考虑环境指标的变循环发动机控制规律设计
Control law design for variable cycle engine considering environmental indicators
摘要
Abstract
Due to its prominent advantages in long-distance and long-endurance transportation,supersonic civil air-craft has become an important development direction for future civil aircraft.The concept of"green aviation"makes energy saving,emission reduction and noise reduction important optimization design objectives of civil aircraft,which naturally imposes corresponding requirements for its power plant.The traditional configuration power fails to realize the combination of low noise at takeoff,high thrust per unit for super-cruise,low fuel consumption rate and low emission index.Taking the dual-containment Variable Cycle Engine(VCE)configuration with Core Driven Fan Stage(CDFS)as the research object,this study examines the design method of steady state adjustable geometry control law consider-ing key optimization design objectives such as the engine performance,jet noise,and NOx emission.The research shows that the improvement in the first-containment variable cycle engine is the best way to improve the engine perfor-mance,and increase in the first culvert split ratio helps to reduce NOx emission,while increase in the inner and second culvert split ratios facilites jet noise reduction.The design results are applied to the power unit re-optimization design of the first generation supersonic airliner Concorde.Compared with the baseline scheme,the supersonic cruise fuel con-sumption rate and the takeoff jet speed are reduced by 20.19%and 44.47%,respectively,enabling the takeoff noise in-dex to meet the airworthiness requirements,under the premise of fulfilling the performance requirements of the aircraft.关键词
喷流噪声/NOx排放/变循环发动机/可调几何调节/控制规律优化设计Key words
jet noise/NOx emission/variable cycle engine/adjustable geometry regulation/control law optimiza-tion design分类
航空航天引用本文复制引用
李富霖,陈敏,唐海龙,张纪元,周越,马静..考虑环境指标的变循环发动机控制规律设计[J].航空学报,2025,46(16):152-169,18.基金项目
国家自然科学基金(52406006) （52406006）
航空发动机气动热力国家级重点实验室基金(2024-CXPT-GF-JJ-88-0001,12700002024146001) National Natural Science Foundation of China(52406006) （2024-CXPT-GF-JJ-88-0001,12700002024146001）
Foundation of National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics(2024-CXPT-GF-JJ-88-0001,12700002024146001) （2024-CXPT-GF-JJ-88-0001,12700002024146001）
