Volume 49 Issue 8
Aug.  2023
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YU Z L,GE H J,WANG Y S,et al. Dual-input dual-Buck aviation static inverter with four-quadrant operation and circulation-free[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(8):2176-2186 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0625
Citation: YU Z L,GE H J,WANG Y S,et al. Dual-input dual-Buck aviation static inverter with four-quadrant operation and circulation-free[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(8):2176-2186 (in Chinese) doi: 10.13700/j.bh.1001-5965.2021.0625

Dual-input dual-Buck aviation static inverter with four-quadrant operation and circulation-free

doi: 10.13700/j.bh.1001-5965.2021.0625
Funds:

National Natural Science Foundation of China (U1933115,U2133203) 

More Information
  • Corresponding author: E-mail:allenge@nuaa.edu.cn
  • Received Date: 22 Oct 2021
  • Accepted Date: 13 Feb 2022
  • Available Online: 22 Sep 2023
  • Publish Date: 10 Mar 2022
  • The aviation static inverter (ASI) is a key part of the airborne power system, and inorder to further improve the efficiency and reliability of the ASI, an efficient and Ihighly reliable circulation-free ASI topology is proposed on the basis of thedual-input dual-Buck inverter technology. The topology not only can operate in four quadrants and transmit part of the power at a single stage, but also achieves circulation-free operation of the bridge arm in all working modes. In this paper, the four quadrant operation mode and the equivalent mathematical model of the topology are analyzed in detail. The driving mode of the main power transistor of the circulation-free ASI based on the mono-polar cascade double carrier modulation is studied. The parameter optimization of the regulator is studied, and the stability margin of the converter closed-loop control system is expanded. Experimental research on the switching loss and efficiency of this topology and full bridge inverter is carried out. The results show that the topology and its control method are correct and feasible, and part of the power can be transmitted in a single stage with high efficiency. And it has the advantages of no bridge arm through risk and no body diode freewheeling. It lays a foundation for high efficiency and high-reliability aviation static converter technology.

     

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