航空发动机性能退化缓解控制技术

李业波; 李秋红; 黄向华; 赵永平

航空发动机性能退化缓解控制技术

1.
南京航空航天大学能源与动力学院, 南京 210016
2.
南京理工大学机械工程学院, 南京 210094

基金项目: 国家自然科学基金(51006052); 航空科学基金(20110652003); 中央高校基本科研业务费专项基金(NZ2012104)

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出版历程
- 收稿日期: 2011-05-29
- 修回日期: 2012-02-07
- 刊出日期: 2012-04-28

Performance deterioration mitigation control of aero-engine

1.
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2.
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China

摘要

摘要: 开展了航空发动机性能退化缓解控制技术的相关研究.性能退化缓解控制通过内环控制转速,外环控制推力,实现了对航空发动机的控制.该控制方式既有传统控制方式的优点,又能像直接推力控制那样实现对推力的直接控制,达到提高发动机控制自主性的目的.为了验证性能退化缓解控制的有效性,以某型双轴混排涡扇发动机为对象进行了控制系统设计及仿真验证.仿真结果表明了性能退化缓解控制技术的有效性和可行性.
- 航空发动机 /
- 性能退化缓解控制 /
- 外环控制 /
- 内环控制 /
- 推力估计
Abstract: The research on PDMC(performance deterioration mitigation control) of intelligent engine was performed.The PDMC consists of both loops,for example,the inner loop controls the rotor speed and the outer loop controls the thrust.As a result,it not only inherits the advantage of traditional control system,but also can realize the direct control of thrust as the direct thrust control.Meanwhile,it enhances the autonomous control of aero-engine.To verify the effectiveness of PDMC,simulations on a two-spool-mixed-flow-turbofan engine were performed.The simulation results show the efficacy and feasibility of PDMC technology.
- aero-engine /
- performance deterioration mitigation control /
- outer loop control /
- inner loop control /
- thrust estimation

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参考文献(14)

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