The invention relates to a propulsion system (20) for a non-rotary-wing aircraft (3), the system comprising an alternating-current generator (24), at least one wingtip propulsion unit (22) comprising an alternating-current motor, and at least one lift-increase propulsion unit (23a-23d) comprising an alternating-current motor. The generator is connected to the lift-increase propulsion unit via a AC/DC converter (261), an intermediate DC distribution stage (260) provided with electric batteries (262) and a DC/AC converter (263a-263d). On the other hand, the generator is connected to the wingtip propulsion unit in such a way as to supply this propulsion unit with alternating current, without intermediate conversion of this alternating current into direct current.The invention also relates to an aircraft provided with such a propulsion system.
SYSTÈME DE PROPULSION POUR AÉRONEF À VOILURE FIXE, ET AÉRONEF ASSOCIÉ
PROPULSION SYSTEM FOR FIXED WING AIRCRAFT AND AIRCRAFT EQUIPPED WITH SAID SYSTEM
ANTRIEBSSYSTEM FÜR STARRFLÜGELFLUGZEUG UND DAMIT AUSGESTATTETES FLUGZEUG
2024-04-24
Patent
Electronic Resource
French
SYSTÈME DE PROPULSION POUR AÉRONEF À VOILURE FIXE, ET AÉRONEF ASSOCIÉ
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