| 飞机专用电源系统的设计与仿真 |
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| 引用本文： | 周增福,严仰光.飞机专用电源系统的设计与仿真[J].微特电机,2006,34(6):27-29. |
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| 作者姓名： | 周增福 严仰光 |
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| 作者单位： | 南京航空航天大学,江苏南京,210016 |
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| 摘 要： | 介绍了一种适用于未来先进飞机的新型飞机专用电源系统的设计方案，由永磁同步发电机和宽电压输入范围的变换／调节装置组成。该方案具有系统结构简单、可靠性高和转速范围宽等优点，并对专用电源系统进行了仿真，仿真结果与理论分析一致。
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| 关 键 词： | 飞机飞行控制系统 高可靠性 专用电源系统 设计与仿真 |
| 文章编号： | 1004-7018(2006)06-0027-03 |
| 收稿时间： | 2004-01-08 |
| 修稿时间： | 2004-03-09 |
Design and Simulation for Special Electrical Power Supply System of Aircraft |
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| ZHOU Zeng-fu,YAN Yang-guang.Design and Simulation for Special Electrical Power Supply System of Aircraft[J].Small & Special Electrical Machines,2006,34(6):27-29. |
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| Authors: | ZHOU Zeng-fu YAN Yang-guang |
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| Affiliation: | Nanjing University of Aeronautics and Astronautics,Nanjing 210016 ,China |
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| Abstract: | A novel design project for the special electrical power supply system of the advanced aircraft to the special electrical power supply system. The system consists of a permanent magnet synchronous generator and a converter/regulator with a wide range of the input voltage. The project has many advantages such as the simple confignration of system, the high reliability and the wide range of revolution speed. The conclusions of simulating of the parameters are presented. The results of simulation are consistent with the theory analysis. |
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| Keywords: | flight control system of aircraft high reliability special electrical power supply system design and simulation |
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