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


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    Titel :

    An Integrated Motor Deceleration Drive System for Helicopter Tail


    Beteiligte:
    ZHEN SHENGCHAO (Autor:in) / PENG XIN (Autor:in) / LIU XIAOLI (Autor:in)

    Erscheinungsdatum :

    2020-09-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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