| 摘要 |
A torque-dividing transmission (20), particularly for aircraft, having a single input pinion (21) and a single output gear (26), both rotating about respective fixed axes (14); at least two gear assemblies (30), both interposed between the pinion (21) and the output gear (26), and each for transferring a respective portion of the torque from the pinion (21) to the output gear (26); and a torque-dividing device (44) for dividing the input torque equally between the two gear assemblies (30); the torque-dividing device (44) having, for each gear assembly (30), a number of elongated elements (52) elastically bendable in use. <IMAGE> |
