发明名称 AIRCRAFT MOTOR DRIVE CONTROL APPARATUS AND AIRCRAFT MOTOR DRIVE CONTROL SYSTEM
摘要 The command signal processing unit outputs, when a first PWM frequency command signal is received, a high-PWM frequency command signal such that an asynchronous PWM control is performed at a PWM frequency of a predetermined constant frequency. The command signal processing unit outputs, when a second PWM frequency command signal is received, a low-PWM frequency command signal such that an asynchronous or synchronous PWM control is performed at a frequency lower than the above-described frequency. The PWM frequency control unit controls the PWM frequency such that an asynchronous PWM control is performed if a motor has a rotational speed less than a predetermined rotational speed and that a synchronous PWM control is performed if the motor has a rotational speed greater than or equal to the predetermined rotational speed, when a low-PWM frequency command signal is input.
申请公布号 US2012187892(A1) 申请公布日期 2012.07.26
申请号 US201213344219 申请日期 2012.01.05
申请人 TSUNEMATSU TOKUJI;NAKAJIMA KAZUSHIGE;KITAZWA HIROYUKI;YOKOGAWA TOMOYUKI;NABTESCO CORPORATION 发明人 TSUNEMATSU TOKUJI;NAKAJIMA KAZUSHIGE;KITAZWA HIROYUKI;YOKOGAWA TOMOYUKI
分类号 H02P6/20 主分类号 H02P6/20
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