According to the invention, the assembly comprises a first inlet shaft (10a) configured to receive torque from a first engine (10), an outlet shaft (60a) configured to transmit torque to a torque receiver (60), a first transmission member (20) having at least two degrees of freedom and comprising first, second, and third movable portions, a first reversible electrical regulator machine (30), and a first reversible electrical balancing machine (40), wherein the inlet shaft (10a) is coupled to the first movable portion, the outlet shaft (60a) is coupled to the second movable portion, the first electrical regulator machine (30) is coupled to the third movable portion, and the first electrical balancing machine (40) is coupled in series with the inlet shaft or the outlet shaft (60a).
ENSEMBLE DE TRANSMISSION POUR AERONEF ET HELICOPTERE
TRANSMISSION ASSEMBLY FOR AN AIRCRAFT AND A HELICOPTER
GETRIEBEANORDNUNG FÜR EIN FLUGZEUG UND EINEN HUBSCHRAUBER
2018-01-10
Patent
Elektronische Ressource
Französisch
DISPOSITIF DE MANUTENTION POUR AERONEF, NOTAMMENT POUR HELICOPTERE
Europäisches Patentamt | 2021
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