The invention belongs to the technical field of scramjet engine control, and particularly discloses a regenerative cooling ramjet engine overtemperature protection method based on flight-engine integrated control, and the overtemperature protection method comprises flight-engine integrated control of an engine overtemperature state and a self-optimization control method of the temperature of the engine. According to the overtemperature protection method, the overtemperature problem of the regenerative cooling ramjet engine can be effectively solved from the angle of flight-engine integrated control, and technical guarantee is provided for normal work of the regenerative cooling ramjet engine.
本发明属于超燃冲压发动机控制技术领域,具体公开了一种基于飞发一体化控制的再生冷却冲压发动机超温保护方法,该超温保护方法包含发动机超温状态的飞发一体化控制以及发动机自身温度的自寻优控制方法,该超温保护方法从飞发一体化控制的角度出发,可有效地解决再生冷却冲压发动机超温的问题,为再生冷却冲压发动机的正常工作提供了技术保障。
Overtemperature protection method for regenerative cooling ramjet engine based on flight-engine integrated control
基于飞发一体化控制的再生冷却冲压发动机超温保护方法
2025-02-21
Patent
Electronic Resource
Chinese
Cooling System for Ramjet Engine
NTIS | 1979
|Cooling System for Ramjet Engine
NTIS | 1979
|