Invention Grant
- Patent Title: Aircraft motor drive control apparatus and aircraft actuator hydraulic system
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Application No.: US13908790Application Date: 2013-06-03
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Publication No.: US09670917B2Publication Date: 2017-06-06
- Inventor: Kazushige Nakajima , Tokuji Tsunematsu , Shingo Nakagawa
- Applicant: NABTESCO CORPORATION
- Applicant Address: JP Tokyo
- Assignee: NABTESCO CORPORATION
- Current Assignee: NABTESCO CORPORATION
- Current Assignee Address: JP Tokyo
- Agency: Studebaker & Brackett PC
- Priority: JP2012-130442 20120608
- Main IPC: H02P27/00
- IPC: H02P27/00 ; F04B17/03 ; H02P23/00 ; H02P6/24 ; F04B49/00 ; H02P23/20

Abstract:
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.
Public/Granted literature
- US20130330207A1 AIRCRAFT MOTOR DRIVE CONTROL APPARATUS AND AIRCRAFT ACTUATOR HYDRAULIC SYSTEM Public/Granted day:2013-12-12
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