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.
PITCH CONTROL ASSEMBLY
ENSEMBLE DE COMMANDE DE PAS
2018-09-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |