大推力氢氧补燃发动机调节阀液流压力闭环控制方法与应用
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1.北京航天动力研究所;2.天津理工大学

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Control method and application of closed-loop of hydraulic pressure of High-thrust LOX/LH2 staged combustion cycle engines control valve
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    摘要:

    大推力氢氧发动机为了使得运载能力达到最优,飞行过程中大范围调节推力,采用了伺服作动系统实现变推力调节;基于机电伺服控制的发动机推力调节方案,调节阀闭环控制流量调节技术是发动机变推力调节的核心技术,调节阀流量控制是采用伺服作动系统调节阀门的横截面积来控制调节阀入口压力;根据分析液流试验台与伺服作动系统的非线性因素,通过试验数据方法获取控制系统等价模型的基础上,进行了控制器算法设计;在仿真测试中增加扰动验证控制器算法设计的有效性,同时在调节阀液流试验中进行了应用。

    Abstract:

    The High-thrust LOX/LH2 staged combustion cycle engines adopts variable thrust adjustment which can achieve the best thrust control and optimize the best carrying capacity. Based on the electromechanical servo-controlled engine thrust adjustment scheme, the closed-loop control flow regulation technology of the regulating valve is the core technology of the variable thrust regulation of the engine. The flow control of the regulating valve is to use the servo actuation system to adjust the cross-sectional area of the valve to control the entrance pressure of the regulating valve. According to the analysis of the nonlinear factors of the liquid flow test bench and the servo actuation system, the controller algorithm is designed on the basis of the obtaining the equivalent model of the control system through the experimental data method. The effectiveness of the closed-loop control method is verified by the hardware-in-the-loop simulation platform. Meanwhile, it is used in the closed-loop test of regulating value liquid flow pressure.

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李宁宁,徐志强,胡慧,许亮.大推力氢氧补燃发动机调节阀液流压力闭环控制方法与应用计算机测量与控制[J].,2025,33(10):97-102.

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  • 收稿日期:2024-06-18
  • 最后修改日期:2024-08-16
  • 录用日期:2024-08-16
  • 在线发布日期: 2025-10-27
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