An electric vertical take-off and landing machine (100, 100a-100d) including a plurality of electric drive systems (10, 10a-10d) having a drive motor (12) for driving and rotating a rotary wing (30) and a drive unit (11) for driving the drive motor includes: a drive information detection unit (55) for detecting drive information for each of the plurality of electric drive systems; the drive information includes at least one of motor information constituting an index of a deterioration state of the drive motor and drive unit information constituting an index of a deterioration state of the drive unit; and a maintenance necessity detection unit (57) that detects, on the basis of the detected drive information, whether maintenance is to be performed on each of the plurality of electric drive systems.

    包括具有驱动旋转翼(30)而使其旋转的驱动用马达(12)及使驱动用马达驱动的驱动部(11)的多个电驱动系统(10、10a~10d)的电动垂直起降机(100、100a~100d)包括:驱动信息检测部(55),其针对多个电驱动系统的每一个检测驱动信息,该驱动信息包括构成驱动用马达的劣化状态的指标的马达信息和构成驱动部的劣化状态的指标的驱动部信息中的至少一方;以及是否要保养检测部(57),其基于检测到的驱动信息,对是否要针对多个电驱动系统的每一个的保养进行检测。


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    Title :

    Electric aircraft and control device for electric aircraft


    Additional title:

    电动航空器及电动航空器的控制装置


    Contributors:

    Publication date :

    2024-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES



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