The invention provides a synchronous turnover mechanism applied to an aerocar, which consists of a motor, a motor straight gear, a main transmission shaft, a main straight gear, a main shaft front bevel gear, a main shaft rear bevel gear, a front driving shaft, a rear driving shaft, a front driving bevel gear, a left front driving bevel gear, a right front driving bevel gear, a left front driven shaft, a left front driven bevel gear, a right front driven shaft, a right front driven bevel gear, a rear driving bevel gear, a left rear driving bevel gear, a right rear driving bevel gear, a left rear driven shaft, a left rear driven bevel gear, a right rear driven shaft, a right rear driven bevel gear and wheel type propellers. The synchronous turnover mechanism applied to the aerocar can realize synchronous turnover of four wheel type propellers, and has the advantages of convenience in control, rapidness, high precision, easiness in operation, low manufacturing cost and the like.
Synchronous turnover mechanism applied to aerocar
2015-12-30
Patent
Elektronische Ressource
Englisch
IPC: | B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen |