A pitch control assembly (110) for adjusting the pitch of a propeller blade, including a pitch control unit comprising a housing(104), with a plurality of control valves(106) and corresponding hydraulic lines(108) located within the housing, a blade angle unit (110), a transfer bearing (120) mounted to the housing and having a plurality of hydraulic lines(122) fluidly coupled to the hydraulic lines of the pitch control unit, a transfer tube (140) axially receiving and axially moveable relative to at least a portion of the transfer bearing, a magnetic core sleeve(150) carried by the transfer tube and located within the blade angle unit.


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    Titel :

    PITCH CONTROL ASSEMBLY


    Weitere Titelangaben:

    ENSEMBLE DE COMMANDE DE PAS


    Beteiligte:

    Erscheinungsdatum :

    2018-09-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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