A propeller transmission system for an aircraft powerplant includes a propeller shaft. One end of the propeller shaft is a power input end, and the other end of the propeller shaft is configured to connect a propeller. The power input end of the propeller shaft is provided with a driven gear, and the driven gear is in transmission connection with an input end of an overload clutch. The propeller transmission system further includes a torsional damper, an output end of the overload clutch is in axial transmission connection with the torsional damper by a flexible disc, and the torsional damper is in transmission connection with the propeller shaft.
Propeller transmission system for aircraft powerplant
2024-07-23
Patent
Electronic Resource
English