In one embodiment, an electrical propulsion system includes an electrical motor configured to drive one or more propellers of the aircraft, a capacitor configured to stabilize a direct current (DC) bus voltage, a first inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to alternate current (AC) voltages to drive a first set of stator windings of the electrical motor, in response to a first pulse width modulation (PWM) vector, and a second inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to AC voltages to drive a second set of stator windings of the electrical motor, in response to a second PWM vector. The first PWM vector and the second PWM vector are substantially equal and opposite vectors.
SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
SYSTEME UND VERFAHREN FÜR KIPPPROPELLER MIT KIPPAKTUATORGETRIEBE UND INTEGRIERTEM WECHSELRICHTER
SYSTÈMES ET PROCÉDÉS POUR HÉLICES BASCULANTES AVEC BOÎTE DE VITESSES À ACTIONNEUR D'INCLINAISON ET ONDULEUR INTÉGRÉ
2025-08-13
Patent
Electronic Resource
English
SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
European Patent Office | 2025
|SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
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|SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
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|SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER
European Patent Office | 2024
|Review of V/STOL aircraft with tilt-propellers and tilt-rotors
Engineering Index Backfile | 1968
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