A transmission system for an aircraft powerplant includes a transmission shaft, where an input end of the transmission shaft is sleeved with a driven gear. One end of the driven gear is axially limited, and the other end of the transmission shaft is configured to connect a rotating member. Furthermore, the other end of the driven gear is in transmission connection with a stop hub, and the stop hub is in transmission connection with an overload clutch. The overload clutch is in transmission connection with the transmission shaft. A disc spring member is interposed between one end of the overload clutch and the stop hub, and the other end of the overload clutch is axially limited. A limit distance is formed between the overload clutch and the stop hub, and a force value of the overload clutch varies with a pressure applied.


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    Titel :

    Transmission system for aircraft powerplant


    Beteiligte:
    ZHOU DAN (Autor:in) / XIONG YINCHAO (Autor:in) / PI LIPING (Autor:in) / TANG ZHONG (Autor:in)

    Erscheinungsdatum :

    23.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / F16H Getriebe , GEARING / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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