Treatise and Report
QIAN Juan, CHEN Qian-hong
Advanced Technology of Electrical Engineering and Energy.
2013, 32(4):
49-54.
Nowadays, more-electric-aircraft (MEA) technology has become a mainstream method of airplane power supply. Because of its high reliability, light in weight and energy saving, 270V high voltage DC power system has become the main development direction for airplane power supply. In the situation of high-power DC-DC converter in aeronautics, full bridge LLC resonant converter can be a relatively better topology. Traditional analog control method has some weakness such as: the control method is relatively single, the hardware of the system is complex, and hard to improve efficiency and to reduce the costs. For these reasons, this paper proposes a solution of digital control. This solution can effectively decrease the size of the power, reduce the costs and improve the efficiency. At last, this paper developed a model machine with the input of 270(1 ±10)% VDC, and the output of 28V/500W DC. The result of the experiments verified the theoretical analysis and the feasibility of the digital control.