本项目以民用飞机主电源系统为研究对象，提出了一种整流感应式无刷电励磁同步发电机。与现有的无刷励磁电机相比，该种电机在继承了三级式无刷电励磁同步发电机优点的同时，有效减小了其结构复杂度，具有结构简单、调磁方便的优点。本项目探索了新电机的工作原理和结构方案，提炼了高度集成耦合磁路的分析方法，推导转子励磁电流的表达式，得到增大励磁效率的设计方法；分析了其航空应用的运行特性，开展了损耗和热场数值计算，为航空无刷交流电机技术的研究提供基础理论支撑，形成高性能无刷励磁技术。本项目具有多学科交叉的特色。不但可应用于航空领域，也可用于风力发电、燃气轮机发电、核能发电等领域。

The main power supply for the civil aircraft is taken as the research object. A Rectified and Induced Brushless Electrical Excitation Synchronous Generator (RIB-EESG) is proposed in this project. Compared with the current brushless excitation generators of the civil aircraft, the advantages of the three-stage brushless excitation synchronous generator are maintained. The RIB-EESG can overcome the complex structure of the three-stage brushless excitation synchronous generator. It also has the advantages, such as simple structure and convenience of magnetic flux adjustment. The operating principle and structure of IRB-EESG is analyzed. The method for the analysis of the machine with the coupled magnetic field is refined. The function of the rotor excitation current is deduced. The design strategy of the optimization of excitation efficiency is studied. The operational characteristics in the aero application is studied. The analysis of losses and thermal analysis are also carried out. The above-mentioned studies provide basic theory support to the aero brushless excitation ac machine. The theory and design method for the high-performance brushless excitation is also formed. This project is the multi-knowledge crossed research. It can be applied not only in the application of the aircraft, but also in the other field, such as wind power generation, gas turbine generation, nuclear power generation and so on.