TY - GEN
T1 - Design and Control of Microturbine Generator Rectifier for Hybrid Electric Propulsion UAV
AU - Wei, Xiaocheng
AU - Yan, Liang
AU - Zhou, Yuchen
AU - Jin, Zijian
AU - Quan, Xiao
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - Compared to traditional electric drones, hybrid electric propulsion drones using turbine power generation have significantly improved endurance and payload capacity. The high-frequency AC power output from the turbine power generation system needs to be rectified before it can be used for propulsion and other onboard equipment. This article proposes a high-performance Microturbine Generator (MTG) rectifier based on a combination of diode rectifier bridge and boost/boost DCDC. This rectifier can achieve precise, efficient, and reliable control of MTG system output voltage, current, and power. Based on this rectifier, the MTG system can achieve generator speed control and engine generator joint control, which will greatly improves the operational stability and reliability of the system and significantly increasing fuel efficiency. The effectiveness of the proposed rectifier in the MTG system was verified through simulation.
AB - Compared to traditional electric drones, hybrid electric propulsion drones using turbine power generation have significantly improved endurance and payload capacity. The high-frequency AC power output from the turbine power generation system needs to be rectified before it can be used for propulsion and other onboard equipment. This article proposes a high-performance Microturbine Generator (MTG) rectifier based on a combination of diode rectifier bridge and boost/boost DCDC. This rectifier can achieve precise, efficient, and reliable control of MTG system output voltage, current, and power. Based on this rectifier, the MTG system can achieve generator speed control and engine generator joint control, which will greatly improves the operational stability and reliability of the system and significantly increasing fuel efficiency. The effectiveness of the proposed rectifier in the MTG system was verified through simulation.
KW - DCDC Converter
KW - Hybrid Eclectic Propulsion
KW - Microturbine
KW - UAV
UR - https://www.scopus.com/pages/publications/85205674154
U2 - 10.1109/ICIEA61579.2024.10665215
DO - 10.1109/ICIEA61579.2024.10665215
M3 - 会议稿件
AN - SCOPUS:85205674154
T3 - 2024 IEEE 19th Conference on Industrial Electronics and Applications, ICIEA 2024
BT - 2024 IEEE 19th Conference on Industrial Electronics and Applications, ICIEA 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 19th IEEE Conference on Industrial Electronics and Applications, ICIEA 2024
Y2 - 5 August 2024 through 8 August 2024
ER -