A landing gear drive system clutch assembly and method of operation 300 comprising a drive gear 320, a driven transmission 350 with an intermediate gear 340 for receiving driving torque from the drive gear and transmitting driving torque to the driven transmission. The drive gear being engageable with the intermediate gear which is engageable with the driven transmission. There is also disclosed an aircraft landing gear comprising a strut with a lever arm (130, Fig 1b) and a drive system with a drive shaft (240, fig 1b) located within an axel and a drive shaft (230, fig 1b) located in the lever arm. There is further disclosed a drive system and method of operation comprising a drive shaft located in a landing gear axel, a clutch assembly comprising a drive gear and a driven transmission, wherein the drive gear is engageable with the driven transmission. There is further disclosed a landing gear drive clutch assembly and method of operation comprising a drive gear assembly and a driven transmission, the drive gear comprising two pinion gears 323, 324 mounted either side of a rotational axis of the driven transmission which can individually engage the driven transmission via movement of a lever.


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    Titel :

    A landing gear drive system clutch assembly


    Beteiligte:

    Erscheinungsdatum :

    18.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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