摘要
可调喷管是影响军用发动机推力性能和飞行器总体性能的关键部件。以介绍航空燃气涡轮发动机为主兼顾火箭发动机以及组合循环发动机,对几何可调喷管的结构特点、工作原理以及发展状况进行了归纳总结,指出几何可调喷管结构设计的关键技术。
Variable nozzle is the key component that affects the thrust performance of military propulsion system and the overall performance of aircraft. Focused on the aviation gas turbine engine,both the rocket propulsion and the combined cycle engine were taken into account. The structure characteristics,working principle and the development of variable nozzles were summarized and concluded. The critical technologies for variable nozzles structure design were proposed.
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