HYBRID PROPULSION SYSTEM FOR MULTI-ROTOR ROTARY WING AIRCRAFT, COMPRISING IMPROVED DC/AC CONVERSION MEANS

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United States of America Patent

APP PUB NO 20200115062A1
SERIAL NO

16336537

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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In order to reduce the weight of a hybrid propulsion system for a multi-rotor rotary-wing aircraft, the system comprises at least one inverter configured to supply power in parallel to multiple electric motors intended to drive the corresponding propellers of the system.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN HELICOPTER ENGINESBORDEAUX BORDEAUX GIRONDE

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
KLONOWSKI, Thomas Moissy-Cramayel, FR 31 125
MEZIERE, Ludovic Moissy-Cramayel, FR 4 13
PLISSONNEAU, Bernard Moissy-Cramayel, FR 4 157

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