厘米级微型涡轮喷气发动机关键控制技术研究

刘源; 黄向华; 张天宏

厘米级微型涡轮喷气发动机关键控制技术研究

1.
中国航空动力控制系统研究所, 无锡 214063
2.
南京航空航天大学能源与动力学院, 南京 210016)

基金项目: 国防科研基金重大项目

计量
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- 被引次数: 0
出版历程
- 收稿日期: 2006-03-20
- 修回日期: 2006-11-03
- 刊出日期: 2007-03-28

Research on key control technology of micro turbine engine in centimeter size

1.
China Aviation Motor Control Institute, Wuxi 214063, China
2.
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

摘要

摘要: 结合厘米级微型涡喷发动机自身特点, 从工程角度研究其关键控制技术.首先运用相似理论, 将参考发动机的起动控制时序变换适用于目标发动机的起动控制, 为了解决微型发动机起动困难问题还首次提出起动供油自校正技术.慢车以上状态采用系统辨识法建模, 通过仿真结合试验的方法设计了带可自动调整前馈的闭环PI调节器.试车试验表明, 研究的控制规律能控制发动机正常可靠运转, 满足各项性能指标要求.
- 航空、航天推进系统 /
- 微型涡喷发动机 /
- 相似理论 /
- 供油自校正 /
- 系统辨识
Abstract: Key control technology of micro turbine energy(MTE) in centimeter size was studied for engineering applications,based on MTE's characteristics.The starting control was firstly transformed for the targeted engine with reference to the starting control time sequence of MTE.The self-revised fuel supply technology was proposed for the first time in order to solve the startup problem of MTE.After the idle state,MTE's model was established by means of system identification,and a closed-loop PI with self-adjust feedforward was designed through simulation and experiments.The test run of MTE demonstrates that the control rules can ensure normal and reliable operation of MTE while meeting the requirements of performance indicators.
- aerospace propulsion system /
- micro turbine energy /
- similarity theory /
- self-revised fuel supply /
- system identification

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参考文献(10)

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