Abstract This invention relates to an integrated motor deceleration drive system for helicopter tail comprises a disc motor and a two-speed transmission mechanism; the disc motor comprises a stator (4), a rotor (5), a roller bearing (7) and a bearing bracket (9), wherein the roller bearing (7) is sleeved on the bearing bracket (9) and is coaxially positioned on the motor shell (3) with the rotor (5); the two-speed transmission mechanism comprises a gearbox body (1), an output shaft (28), a first-speed driving gear (17), a first-speed driven gear (34), a second-speed driving gear (22), a second-speed driven gear (33), an intermediate shaft (32) and a synchronizer (19). -1/7 Figure 1
An Integrated Motor Deceleration Drive System for Helicopter Tail
2020-09-17
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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