The invention provides an aircraft. An aircraft (10) is provided with a rotor (18) and a rotor (20) driven by an electric motor (48), a PCU (42), an inverter (50), a DC wiring, and an AC wiring. The PCU is used for converting alternating current power output from a generator (40) into direct current power; an inverter that converts DC power supplied from the PCU (42) into AC power and outputs the AC power to the electric motor (48); the DC wiring is connected with the PCU (42) and the inverter (50); and an AC wiring connecting the inverter (50) and the electric motor (48), the AC wiring being disposed in a direction orthogonal to the direction in which the rotating shafts of the generator (40) and the gas turbine (38) extend. Therefore, the thrust can be ensured.

    本发明提供一种航空器。航空器(10)具有旋翼(18)及旋翼(20)、PCU(42)、逆变器(50)、直流配线和交流配线,其中,所述旋翼(18)及所述旋翼(20)由电动马达(48)驱动;所述PCU将从发电机(40)输出的交流电功率转换为直流电功率;所述逆变器将从PCU(42)供给的直流电功率转换为交流电功率,并将其向电动马达(48)输出;所述直流配线连接PCU(42)和逆变器(50);所述交流配线连接逆变器(50)和电动马达(48),在与发电机(40)和燃气涡轮(38)的旋转轴延伸的方向正交的方向上配置交流配线。据此,能够确保推力。


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    Titel :

    Aircraft


    Weitere Titelangaben:

    航空器


    Beteiligte:
    MITANI MANABU (Autor:in) / FUKAZU TOMOHIRO (Autor:in) / FUKUCHI YUICHI (Autor:in) / ETO MASASHI (Autor:in)

    Erscheinungsdatum :

    2023-10-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern



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