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.


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    Title :

    SYSTEMS AND METHODS FOR TILT PROPELLERS WITH TILT ACTUATOR GEARBOX AND INTEGRATED INVERTER


    Additional title:

    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



    Publication date :

    2025-08-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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