Three-Phase PWM Voltage-Source-Inverter Weight Optimization for Aircraft Application Using Deterministic Algorithm

In this paper, a design by optimization process is used to size a 10-kW three-phase pulse width modulation (PWM) inverter for aeronautic application. The objective function is the converter weight, which has to be minimized. Sizing constraints are the efficiency, alternating current (AC) and direct...

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Published inElectronics (Basel) Vol. 9; no. 9; p. 1393
Main Authors Voldoire, Adrien, Schanen, Jean-Luc, Ferrieux, Jean-Paul, Derbey, Alexis, Gautier, Cyrille
Format Journal Article
LanguageEnglish
Published Basel MDPI AG 01.09.2020
Subjects
Aircraft
Algorithms
Alternating current
Design
Design optimization
Direct current
Electric converters
Inverters
Methods
Optimization
Power
Pulse duration modulation
Seats
Simulation
Variables
Weight
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ISSN2079-9292
2079-9292
DOI10.3390/electronics9091393

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Abstract In this paper, a design by optimization process is used to size a 10-kW three-phase pulse width modulation (PWM) inverter for aeronautic application. The objective function is the converter weight, which has to be minimized. Sizing constraints are the efficiency, alternating current (AC) and direct current (DC) harmonics, and thermal constraints on all devices. A deterministic algorithm is chosen since it allows obtaining quick results and dealing with a large number of variables. All equations are analytical, in order to comply with this gradient-based optimization strategy, which imposes the derivability of the models. Several optimization results using different AC inductor solutions (iron powder and ferrite) are compared. The optimized converters were built and tested experimentally to verify their performances. Semiconductor and inductor losses were measured accurately using calorimetric test benches. The optimality of the solutions was carefully verified by changing parameters.
AbstractList In this paper, a design by optimization process is used to size a 10-kW three-phase pulse width modulation (PWM) inverter for aeronautic application. The objective function is the converter weight, which has to be minimized. Sizing constraints are the efficiency, alternating current (AC) and direct current (DC) harmonics, and thermal constraints on all devices. A deterministic algorithm is chosen since it allows obtaining quick results and dealing with a large number of variables. All equations are analytical, in order to comply with this gradient-based optimization strategy, which imposes the derivability of the models. Several optimization results using different AC inductor solutions (iron powder and ferrite) are compared. The optimized converters were built and tested experimentally to verify their performances. Semiconductor and inductor losses were measured accurately using calorimetric test benches. The optimality of the solutions was carefully verified by changing parameters.
Author Ferrieux, Jean-Paul
Gautier, Cyrille
Schanen, Jean-Luc
Derbey, Alexis
Voldoire, Adrien
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  surname: Derbey
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SubjectTerms Aircraft
Algorithms
Alternating current
Design
Design optimization
Direct current
Electric converters
Inverters
Methods
Optimization
Power
Pulse duration modulation
Seats
Simulation
Variables
Weight
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Title Three-Phase PWM Voltage-Source-Inverter Weight Optimization for Aircraft Application Using Deterministic Algorithm
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