This utility model discloses an integrated three-phase drive and three-phase rectification
electronic control unit for aero-engines, comprising: a
digital signal controller U1, a three-phase full-bridge power circuit, a drive
chipset, a drive
resistor network, an anti-reverse device, a
capacitor C3, and a power supply S1; MOSFETs M1, M3, and M5 of the three-phase full-bridge power circuit form the upper bridge arm, and MOSFETs M2, M4, and M6 form the lower bridge arm, corresponding to the U-phase, V-phase, and W-phase, respectively; the
signal output from the
digital signal controller U1 is amplified by the drive
chipset and then drives the gates of MOSFETs M1 to M6 through the drive
resistor network; the positive and negative terminals of the power supply S1 are connected to the upper and lower bridge arms, respectively;
capacitor C3 is connected in parallel between the positive and negative terminals of the power supply S1; and the anti-reverse device is connected in series between the positive terminal of the power supply S1 and the upper bridge arm. This integrated three-phase drive and three-phase rectification
electronic control unit for aero-engines, through its
integrated design, reduces the need for additional batteries or external rectifiers, thus reducing the weight of the aircraft.