发明名称 AIRCRAFT MOTOR DRIVE CONTROL APPARATUS AND AIRCRAFT ACTUATOR HYDRAULIC SYSTEM
摘要 A controller that performs pulse width modulation control of a three-phase inverter circuit includes a three-phase modulation voltage command value generation unit, a two-phase modulation voltage command value generation unit, a voltage command switching unit, and a PWM signal output unit. The voltage command switching unit switches a voltage command value to a two-phase modulation voltage command value when a determination value becomes larger than or equal to a first threshold value, and switches the voltage command value to a three-phase modulation voltage command value when the determination value becomes smaller than a second threshold value, which is smaller than the first threshold value.
申请公布号 US2013330207(A1) 申请公布日期 2013.12.12
申请号 US201313908790 申请日期 2013.06.03
申请人 NABTESCO CORPORATION 发明人 NAKAJIMA KAZUSHIGE;TSUNEMATSU TOKUJI;NAKAGAWA SHINGO
分类号 F04B17/03;H02P6/24;H02P23/00 主分类号 F04B17/03
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