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HYBRID PROPULSION SYSTEM FOR MULTI-ROTOR ROTARY-WING AIRCRAFT, COMPRISING IMPROVED DC/AC CONVERSION MEANS
HYBRID PROPULSION SYSTEM FOR MULTI-ROTOR ROTARY-WING AIRCRAFT, COMPRISING IMPROVED DC/AC CONVERSION MEANS
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机译：多转子旋转翼飞机的混合动力推进系统，包括改进的DC / AC转换装置
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摘要
In order to reduce the weight of a hybrid propulsion system (30) for a multi-rotor rotary-wing aircraft, the system comprises at least one inverter (36) configured to supply power in parallel to multiple electric motors (46A, 46B) intended to drive the corresponding propellers of the system.
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