东北大学学报(自然科学版) ›› 2025, Vol. 46 ›› Issue (4): 71-77.DOI: 10.12068/j.issn.1005-3026.2025.20239049

• 机械工程 • 上一篇    下一篇

航空发动机燃油泵调节器计量活门特性分析

蔡惠坤1, 李朝阳1, 周毅博1,2, 徐晨1   

  1. 1.厦门大学 萨本栋微米纳米科学技术研究院,福建 厦门 361102
    2.中国航发控制系统研究所,江苏 无锡 214063
  • 收稿日期:2023-09-14 出版日期:2025-04-15 发布日期:2025-07-01
  • 作者简介:蔡惠坤(1984—),男,福建漳州人,厦门大学副教授,博士生导师.
  • 基金资助:
    国家自然科学基金资助项目(52076183);福建省科技厅STS计划项目(2023T3009)

Characteristic Analysis on Metering Valves of Fuel Pump Regulators in Aero Engines

Hui-kun CAI1, Zhao-yang LI1, Yi-bo ZHOU1,2, Chen XU1   

  1. 1.Pen -Tung Sah Institute of Micro-Nano Science and Technology,Xiamen University,Xiamen 361102,China
    2.China Aviation Development Control System Research Institute,Wuxi 214063,China. Corresponding author: CAI Hui-kun,E-mail: caihuikun@xmu. edu. cn
  • Received:2023-09-14 Online:2025-04-15 Published:2025-07-01

摘要:

为提高航空发动机燃油泵调节器系统的控制精度和品质,构建了基于AMESim的航空发动机计量活门仿真模型和实验测试平台,解析了发动机出口流量与活门开度之间的线性变化关系.活门前后压力先缓慢增加,在活门开度达到60%后迅速增大,但二者的压力差基本维持在0.5 MPa.仿真与实验结果的变化趋势一致,稳态误差控制在5%以内,动态误差控制在10%以内.同时研究了系统转速和出口负载对计量活门工作特性的影响,发现系统转速对计量活门前后压力影响较大,易引发压力超调和液压冲击现象;而出口负载对计量活门前后压力影响较小,虽无超调,但有轻微的滞后现象.

关键词: 航空发动机, 燃油泵调节器, 计量活门, 稳态特性, 动态特性

Abstract:

In order to improve the control accuracy and performance quality of fuel pump regulators for an aero engine, a simulation model and an experimental bench of the metering valve were built based on AMESim, and the linear relationship between the engine outlet flow and the valve’s opening degree was analyzed. It was found that the engine outlet flow changes linearly with valve opening, but both the inlet and outlet pressures change slowly initially and then increase greatly when the valve’s opening reaches 60%. Meanwhile, the pressure difference of the inlet and outlet is almost at 0.5 MPa. The simulation results agree well with the experimental results, and the differences of the steady and dynamic states are below 5% and 10%, respectively. Furthermore, the effects of the system’s rotating speed and outlet load on the metering valve performance were also studied, and it was found that the system’s rotating speed plays a large role on the metering valve performance as there can be some pressure overshoot and hydraulic impact when it changes, whereas the outlet load plays a small role on the metering valve performance as there is no pressure overshoot but there is a little lagging.

Key words: aero engine, fuel pump regulator, metering valve, steady characteristics, dynamic characteristics

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