主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
微型涡喷发动机转速控制系统设计与验证
DOI:
作者:
作者单位:

南京航空航天大学

作者简介:

通讯作者:

中图分类号:

V235

基金项目:

直升机旋翼动力学国家级重点实验室基金资助项目(9140C400504130C4148)


Design and Validation of a Micro Turbine EngineSpeed Control System
Author:
Affiliation:

Nanjing University of Aeronautics and Astronautics

Fund Project:

National Key Laboratory of Rotorcraft Aeromechanics Fund Program of China (9140C400504130C4148)

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    微型涡喷发动机控制系统在发动机运行过程中起重要作用。从总体架构出发设计某微型涡喷发动机的系统控制结构,针对传统PID 控制效果不佳的问题,提出基于线性自抗扰控制(LADRC)技术的转速控制律设计方法;开展系统硬件实现和软件开发研究,运用STM32F103VET6 嵌入式微处理器研制发动机转速控制器硬件实物;针对半桥式油泵驱动电路存在桥臂直通隐患,设计可控制MOSFET 导通的延时电路,采用三层软件架构完成转速测量、闭环控制等程序设计、开发、调试;构建转速控制系统试验验证平台,测试、验证油泵驱动电路和延时电路以及转速控制系统。结果表明:驱动电路具有稳定可靠的通断特性,设计构建的控制系统能够实时监测发动机运行参数并控制发动机转速跟随目标转速,调节速度快、稳态误差小,满足微型涡喷发动机控制系统应用需求。

    Abstract:

    The control system of a micro turbine engine plays a crucial role during engine operation. This paper focuses on the design of a speed control system for a specific micro turbine engine. Starting from the overall architecture, the control structure of the system is designed. A speed control law design method based on Linear Active Disturbance Rejection Control (LADRC) technology is proposed. Subsequently, research is conducted on hardware implementation and software development using the STM32F103VET6 embedded microprocessor to develop the hardware controller for engine speed control. Addressing the potential issue of direct conduction in the half-bridge fuel pump drive circuit, a delay circuit is designed to control the conduction time of MOSFET. A three-layer software architecture is utilized for the design, development, and debugging of programs for speed measurement, closed-loop control, and other functions. Finally, a speed control system experimental verification platform is constructed to test and validate the fuel pump drive circuit, delay circuit, and speed control system. Experimental results demonstrate that the drive circuit exhibits stable and reliable on-off characteristics. The engine speed can rapidly follow the target speed, with a steady-state error of less than 1%, meeting the application requirements of the micro turbine engine control system.

    参考文献
    相似文献
    引证文献
引用本文
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2024-02-05
  • 最后修改日期:2024-04-08
  • 录用日期:2024-05-17
  • 在线发布日期: 2025-03-13
  • 出版日期: