| Citation: | YANG Keyu, JIA Linyuan, CHEN Yuchun, et al. Design method for mode transition control schedule of turboshaft-turbofan variable cycle engines[J]. Journal of Aerospace Power, 2025, 40（12）：20240697 doi: 10.13224/j.cnki.jasp.20240697
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The need for performance optimization during the mode transition process of a turboshaft-turbofan variable cycle engine was addressed. A mode transition control schedule design method focused on output power was proposed while considering the adjustment rate limits of variable geometry components. Based on the engine’s physical characteristics and component-level performance model, a direct solution method for the transition state of the turboshaft-turbofan variable cycle engine was developed using inverse algorithms and implicit calculation formats for transition state performance. Using this method, a control schedule design method was proposed, enabling to realize direct power control and set the operating point of compression components during mode transition. The results showed that under conditions of flight height
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