Pitch control assembly and propeller blade assembly having a spider hub comprising a hub and a set of arms spaced circumferentially about the hub and projecting radially from the hub, wherein the set of arms are configured to receive a set of blades such that a blade root of a blade is rotationally mountable into an arm included in the set of arms, a crosshead located within the hub and axially moveable relative to the hub, a torque tube located in the arm and extending into the hub, wherein a pitch angle of the blade can be adjusted by axially moving the crosshead to rotate the torque tube to effect a corresponding rotation of the blade.
PITCH CONTROL ASSEMBLY AND PROPELLER ASSEMBLY AND METHOD OF ADJUSTING PITCH
DISPOSITIF DE COMMANDE DE PAS ET DISPOSITIF D'HELICE ET METHODE DE REGLAGE DE PAS
2017-01-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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