变循环发动机模式切换控制计划优化方法

By employing C-Bézier curves and multi-objective optimization methods in a variable cycle engine, the open-loop control plan of the adjustable geometry mechanism was optimized, solving the problems of thrust fluctuation and time non-optimization during the mode switching process of the variable cycle engine, and achieving safe, smooth and fast mode switching control.

CN117742158BActive Publication Date: 2026-07-17NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
Filing Date
2024-01-25
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In existing variable cycle engine mode switching control, the mode switching process suffers from large thrust fluctuations, unoptimized switching time, and difficulty in coordinating multiple variables. Furthermore, traditional methods have failed to effectively balance mode switching time and stability.

Method used

An open-loop control plan for the adjustable geometry mechanism using C-Bézier curve mapping is adopted. Through multi-objective optimization, the position and time of the adjustable geometry mechanism during the mode switching process are optimized. Based on the NSGA-II algorithm, the optimal mode switching control plan is formulated to ensure safe, smooth and rapid engine switching.

Benefits of technology

It achieves the shortest mode switching time and the smallest thrust fluctuation, ensuring the smooth operation of the variable cycle engine within the safety boundary and improving the performance of mode switching control.

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Abstract

本发明公开了一种变循环发动机模式切换控制计划优化方法。首先将各可调几何机构在模式切换过程中的开环控制计划分别映射为C‑Bézier曲线,C‑Bézier曲线的横坐标为模式切换过程中所经历的时间在模式切换时间中的占比,纵坐标为可调几何机构期望位置;然后以各条C‑Bézier曲线除起点、终点以外的其他控制点纵坐标、各条C‑Bézier曲线参数α及模式切换时间作为待优化变量,以模式切换时间最短、推力波动最小为目标,使用多目标优化方法对模式切换过程进行优化,得到最优的模式切换时间以及相对应的开环控制计划。本发明还公开了一种变循环发动机模式切换控制方法。本发明能够同时兼顾模式切换时间和模式切换的平稳性,全面提升发动机模式切换控制性能。
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