| 摘要 |
A transmission assembly for an aircraft and a helicopter comprising such an assembly for independently adjusting the speed of rotation of an engine and a torque receiver. According to the invention, the assembly comprises a first input shaft (10a), configured to receive mechanical torque from a first engine (10), an output shaft (60a), configured to transmit mechanical torque to a torque receiver (60), a first transmission member (20) having at least two degrees of mobility comprising first, second and third movable parts, a first regulating reversible electric machine (30), and a first balancing reversible electric machine (40), in which the input shaft (10a) is coupled to the first movable part, the output shaft (60a) is coupled to the second movable part, the first regulating electric machine (30) is coupled to the third movable part, and the first balancing electric machine (40) is coupled in series to the input shaft or the output shaft (60a). |
