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A new design method for mode transition control law of variable cycle engine

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

14 引用 (Scopus)

摘要

Both the polar moment of inertia and volume dynamics of variable cycle engine were considered, the transition-state numerical simulation system for VCE is established. A new mode transition method with a ladder-type variation of thrust is proposed. The ladder-type mode transition method isolates the thrust variation from the traditional mode transition process The VCE thrust is kept constant during mode transition, making it easy to get smooth mode transition. Differential evolution algorithm is used to design the mode transition control law. Based on the designed mode transition control law, the transient simulation of mode transition performance is conducted. The result shows that the designed control law basically realizes the ladder-type mode transition. The parameters change smoothly throughout the entire mode transition process. Thrust changes dramatically with minor change in specific fuel consumption. The inlet mass flow ratio changes slightly which means that the control law can enable what is known as flow holding.

源语言英语
主期刊名2018 Joint Propulsion Conference
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105708
DOI
出版状态已出版 - 2018
活动54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 - Cincinnati, 美国
期限: 9 7月 201811 7月 2018

出版系列

姓名2018 Joint Propulsion Conference

会议

会议54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
国家/地区美国
Cincinnati
时期9/07/1811/07/18

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