To provide a power supply system of a vertical take-off and landing aircraft including VTOL rotors.SOLUTION: A controller (a control unit 64) of a power supply system 30 of a vertical take-off and landing aircraft is configured to: after lift is generated by wings (a front wing and a rear wing), perform stop control of controlling electric power supplied to a motor 40 so that rotation of a VTOL rotor 20 continues to stop; temporarily cancel the stop control in response to a temperature of any one switching element detected by a temperature detection unit (a temperature sensor 58) becoming equal to or higher than a temperature threshold during the stop control; and resume the stop control after the stop control has been temporarily canceled.SELECTED DRAWING: Figure 2

    【課題】VTOLロータを備える垂直離着陸航空機の電力供給システムに関する。【解決手段】垂直離着陸航空機の電力供給システム30のコントローラ(制御部64)は、翼(前翼、後翼)による揚力が発生した後に、VTOLロータ20の回転が停止し続けるようにモータ40に供給する電力を制御する停止制御を行い、停止制御中に、温度検出部(温度センサ58)によって検出されるいずれか1つのスイッチング素子の温度が温度閾値以上になることに応じて、停止制御を一時解除し、停止制御の一時解除後に停止制御を再開する。【選択図】図2


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    Titel :

    POWER SUPPLY SYSTEM OF VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    Weitere Titelangaben:

    垂直離着陸航空機の電力供給システム


    Beteiligte:
    YOSHIMURA KAISAKU (Autor:in) / AIZAWA BON (Autor:in) / UCHIDA KENTA (Autor:in) / KATO MASASHI (Autor:in) / TSUKAMOTO MUNENORI (Autor:in)

    Erscheinungsdatum :

    15.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern