超燃冲压发动机燃油供给系统方案设计

Du Yuhuan, Z. Xiaodong
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引用次数: 0

摘要

超燃冲压发动机是未来高超声速飞行器的基础,而供油系统是超燃冲压发动机发展的重要组成部分。考虑燃油主动冷却,分析设计了一种通过阀控的燃油供给系统方案,并针对该方案提出了相应的控制程序。在对系统进行简化后,建立了单点燃油喷射系统各部分的数学模型。最后,采用齐格勒-尼科尔斯整定法设计了PID控制器;仿真结果表明,该控制器能够满足系统的性能要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of scramjet engine fuel feed system scheme
Scramjet is the basis for future hypersonic vehicles, and fuel supply system is an important part in scramjet engine development. Considering of the fuel active cooling, a fuel feed system scheme through valve control was analyzed and designed, and then the control program was put forward for this corresponding scheme. After simplifying the system, each part's mathematical model of the single-point fuel injection system was built. Finally, a PID controller was designed by using Ziegler-Nichols tuning method; simulation results show that the controller can meet the system performance requirements.
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