发明名称 航空機搭載用モータ駆動制御装置
摘要 An inverter and a control unit that has a command signal processing unit and a PWM frequency control unit and performs pulse width modulation control are provided. If the command signal processing unit has received a first PWM frequency command signal, it outputs a low PWM frequency command signal so that synchronous or asynchronous PWM control is performed at a PWM frequency in a predetermined frequency range. The command signal processing unit outputs a high PWM frequency command signal so that synchronous or asynchronous PWM control is performed at a higher frequency than the above-mentioned frequency if the command signal processing unit has received a second PWM frequency command signal and until a predetermined time period elapses. The command signal processing unit outputs a low PWM frequency command signal if it has received the second PWM frequency command signal and after the predetermined time period elapsed.
申请公布号 JP5844164(B2) 申请公布日期 2016.01.13
申请号 JP20120008607 申请日期 2012.01.19
申请人 ナブテスコ株式会社 发明人 中川 伸吾;森 淳
分类号 B64C13/50;H02M7/48;H02P6/08;H02P27/08 主分类号 B64C13/50
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