FIELD: electricity.
SUBSTANCE: invention is referred to a voltage generation method implemented by a generator module (20) of an airborne vehicle mains (1), at that the above mains (1) comprises a power supply line (3) supplied by the above generator module (20), a direct-current bus (4) supplied by the above power supply line (3) through a rectifier (5) and at least one electric drive (9) supplied by alternating current from the direct-current bus (4) through an inverter (8); thereat the generation method comprises the stage at which alternating-current voltage (VAC) is supplied as the function of the set voltage and the voltage measured in the airborne mains (1). In order to obtain the technical result the generation method comprises the stage whereat the above set voltage value is defined as the function of the operating parameter (v9) of the above drive (9).
EFFECT: limiting losses in the inverter and reducing its dimensions.
7 cl, 5 dwg
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Authors
Dates
2015-09-27—Published
2012-03-07—Filed